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A318/A319/A320/A321FLIGHT CREW TRAINING MANUAL

PRELIMINARY PAGESTABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET PLP-TOC. P 1/2FCTM 09 JAN 09

PLP. PRELIMINARY PAGESTABLE OF CONTENTS........................................................................................................................................... 1/2LIST OF EFFECTIVE SECTIONS/SUBSECTIONS.................................................................................................1/2LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETINS........................................................................1/2LIST OF EFFECTIVE FLIGHT CREW TRAINING BULLETINS..............................................................................1/2AIRCRAFT ALLOCATION TABLE........................................................................................................................ 1/136LIST OF MODIFICATIONS.................................................................................................................................... 1/32

�

IN. Introduction

OP. Operational Philosophy

NO. Normal Operations

AO. Abnormal Operations

SI. Supplementary Information

PIR. Preventing Identified Risks


PRELIMINARY PAGESTABLE OF CONTENTS


ENV A318/A319/A320/A321 FLEET PLP-TOC. P 2/2FCTM 09 JAN 09


PRELIMINARY PAGESLIST OF EFFECTIVE SECTIONS/SUBSECTIONS

ENV A318/A319/A320/A321 FLEET PLP-LESS. P 1/2FCTM 09 JAN 09

M(1) Localization Subsection Title Pages Rev. DateR IN-010 GENERAL INTRODUCTION 1/2 to 2/2 09 JAN 09

OP-010 INTRODUCTION 1/2 to 2/2 08 JUL 08R OP-020 FLIGHT CONTROLS 1/20 to 20/20 09 JAN 09R OP-030 AP / FD / ATHR 1/24 to 24/24 09 JAN 09

OP-040 ECAM 1/10 to 10/10 08 JUL 08NO-010 GENERAL 1/4 to 4/4 08 JUL 08

R NO-020 PRE START 1/22 to 22/22 08 JUL 08R NO-030 START 1/12 to 12/12 09 JAN 09R NO-040 TAXI 1/20 to 20/20 09 JAN 09R NO-050 TAKEOFF 1/18 to 18/18 08 JUL 08R NO-060 CLIMB 1/8 to 8/8 08 JUL 08R NO-070 CRUISE 1/24 to 24/24 08 JUL 08R NO-080 DESCENT 1/10 to 10/10 09 JAN 09

NO-090 HOLDING 1/2 to 2/2 08 JUL 08R NO-100 APPROACH GENERAL 1/22 to 22/22 08 JUL 08R NO-110 ILS APPROACH 1/6 to 6/6 08 JUL 08R NO-120 NON PRECISION APPROACH 1/14 to 14/14 09 JAN 09

NO-130 CIRCLING APPROACH 1/4 to 4/4 09 JAN 09R NO-140 VISUAL APPROACH 1/4 to 4/4 08 JUL 08

NO-150 PRECISION APPROACH 1/8 to 8/8 08 JUL 08R NO-160 LANDING 1/18 to 18/18 09 JAN 09R NO-170 GO AROUND 1/8 to 8/8 08 JUL 08R NO-180 TAXI IN 1/6 to 6/6 08 JUL 08

AO-010 GENERAL 1/6 to 6/6 09 JAN 09R AO-020 OPERATING TECHNIQUES 1/20 to 20/20 09 JAN 09

AO-022 AUTOFLIGHT 1/2 to 2/2 08 JUL 08R AO-024 ELECTRICAL 1/6 to 6/6 08 JUL 08R AO-026 FIRE PROTECTION 1/8 to 8/8 09 JAN 09

AO-027 FLIGHT CONTROLS 1/2 to 2/2 08 JUL 08AO-028 FUEL 1/2 to 2/2 08 JUL 08

R AO-029 HYDRAULIC 1/6 to 6/6 08 JUL 08R AO-032 LANDING GEAR 1/2 to 2/2 09 JAN 09R AO-034 NAVIGATION 1/14 to 14/14 09 JAN 09

AO-070 POWER PLANT 1/2 to 2/2 08 JUL 08R AO-090 MISCELLANEOUS 1/10 to 10/10 08 JUL 08

SI-010 ADVERSE WEATHER 1/16 to 16/16 08 JUL 08R SI-020 FLYING REFERENCE 1/6 to 6/6 08 JUL 08

SI-030 NAVIGATION ACCURACY 1/8 to 8/8 08 JUL 08R SI-040 ZFW - ZFCG ENTRY ERRORSZFW - ZFCG

ENTRY ERRORS1/8 to 8/8 08 JUL 08


PRELIMINARY PAGESLIST OF EFFECTIVE SECTIONS/SUBSECTIONS

ENV A318/A319/A320/A321 FLEET PLP-LESS. P 2/2FCTM 09 JAN 09

M(1) Localization Subsection Title Pages Rev. DateSI-060 TCAS 1/4 to 4/4 08 JUL 08

R SI-070 USE OF RADAR 1/10 to 10/10 09 JAN 09PIR-010 PREVENTING IDENTIFIED RISKS 1/4 to 4/4 08 JUL 08

(1) Evolution code


PRELIMINARY PAGESLIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN

ENV A318/A319/A320/A321 FLEET PLP-LEOEB. P 1/2FCTM 09 JAN 09

M(1) Identification T(2) E(3) Rev. Date Title

No Operations Engineering Bulletin

(1) Evolution code(2) Ecam Importance Type(3) Documentary Unit Impacted by Ecam


PRELIMINARY PAGESLIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN


ENV A318/A319/A320/A321 FLEET PLP-LEOEB. P 2/2FCTM 09 JAN 09


PRELIMINARY PAGESLIST OF EFFECTIVE FLIGHT CREW TRAINING BULLETIN

ENV A318/A319/A320/A321 FLEET PLP-LEFCTB. P 1/2FCTM 09 JAN 09

M(1) Identification Rev. Date Title

No Flight Crew Training Bulletin

(1) Evolution code


PRELIMINARY PAGESLIST OF EFFECTIVE FLIGHT CREW TRAINING BULLETIN


ENV A318/A319/A320/A321 FLEET PLP-LEFCTB. P 2/2FCTM 09 JAN 09


PRELIMINARY PAGESAIRCRAFT ALLOCATION TABLE

ENV A318/A319/A320/A321 FLEET PLP-AAT. P 1/136FCTM 09 JAN 09

This table gives, for each delivered aircraft, the cross reference between:

- The Manufacturing Serial Number (MSN).- The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S.- The registration number of the aircraft as known by AIRBUS S.A.S.- The aircraft model.

M(1) MSN FSN Registration Number Model

0002 AIB 0008 F-GFKQ 320-111

0003 AIB 0401 F-GGEG 320-111

N 0005 AIB 0001 F-GFKA 320-111

0007 AIB 0002 F-GFKB 320-111

0010 AIB 0011 F-GGEA 320-111

0012 AIB 0012 F-GGEB 320-111

0013 AIB 0013 F-GGEC 320-111

0014 AIB 0004 F-GFKD 320-111

0016 AIB 0015 F-GGEE 320-111

0019 AIB 0005 F-GFKE 320-111

0020 AIB 0006 F-GFKF 320-111

0021 AIB 0007 F-GFKG 320-111

0029 AIB 0007 SX-BLX 320-211

0031 AIB 0301 N301US 320-211

0033 AIB 0001 F-GHQA 320-211

0034 AIB 0303 N303US 320-211

0035 AIB 0002 5B-DAU 320-231

0037 AIB 0003 5B-DAV 320-231

0038 AIB 0004 5B-DAW 320-231

0039 AIB 0006 G-BUSG 320-211

0040 AIB 0304 N304US 320-211

0041 AIB 0305 N305US 320-211

0042 AIB 0007 G-BUSH 320-211

0043 AIB 0001 S5-AAA 320-231





0044 AIB 0068 F-GHQC 320-211

0045 AIB 0001 VT-EPB 320-231

0046 AIB 0002 VT-EPC 320-231

0047 AIB 0003 VT-EPD 320-231

0048 AIB 0004 VT-EPE 320-231

0049 AIB 0005 VT-EPF 320-231

0050 AIB 0006 VT-EPG 320-231

0051 AIB 0007 VT-EPH 320-231

0052 AIB 0620 N620AW 320-231

0053 AIB 0621 N621AW 320-231

0054 AIB 0622 N622AW 320-231

0055 AIB 0624 N624AW 320-231

0056 AIB 0008 VT-EPI 320-231

0057 AIB 0009 VT-EPJ 320-231

0058 AIB 0010 VT-EPK 320-231

0059 AIB 0201 C-FDQQ 320-211

0061 AIB 0031 F-GFKH 320-211

0062 AIB 0032 F-GFKI 320-211

0063 AIB 0033 F-GFKJ 320-211

0064 AIB 0625 N625AW 320-231

0065 AIB 0626 N626AW 320-231

0066 AIB 0627 N627AW 320-231

0067 AIB 0628 N628AW 320-231

0068 AIB 0202 C-FDQV 320-211

0069 AIB 0001 D-AIPA 320-211

0070 AIB 0002 D-AIPB 320-211

0071 AIB 0003 D-AIPC 320-211

0072 AIB 0004 D-AIPD 320-211

0073 AIB 0203 C-FDRH 320-211





0074 AIB 0011 VT-EPL 320-231

0075 AIB 0012 VT-EPM 320-231

0076 AIB 0629 N629AW 320-231

0077 AIB 0631 N631AW 320-231

0078 AIB 0005 D-AIPE 320-211

0080 AIB 0014 VT-EPO 320-231

0081 AIB 0632 N632AW 320-231

0082 AIB 0633 N633AW 320-231

0083 AIB 0006 D-AIPF 320-211

0084 AIB 0204 C-FDRK 320-211

0085 AIB 0052 UR-DAA 320-211

0086 AIB 0007 D-AIPH 320-211

0087 AIB 0001 SX-BVL 320-212

R 0088 AIB 0002 SX-BVK 320-212

0089 AIB 0015 VT-EPP 320-231

0090 AIB 0016 VT-EPQ 320-231

0091 AIB 0634 N634AW 320-231

0093 AIB 0008 D-AIPK 320-211

0094 AIB 0009 D-AIPL 320-211

0095 AIB 0017 VT-EPR 320-231

0096 AIB 0018 VT-EPS 320-231

0097 AIB 0019 VT-EPT 320-231

0098 AIB 0636 N636AW 320-231

0099 AIB 0637 N637AW 320-231

0100 AIB 0034 F-GFKK 320-211

0101 AIB 0035 F-GFKL 320-211

0102 AIB 0036 F-GFKM 320-211

0103 AIB 0008 G-BUSI 320-211

0104 AIB 0010 D-AIPM 320-211





0108 AIB 0071 F-GHQD 320-211

0109 AIB 0009 G-BUSJ 320-211

0110 AIB 0012 D-AIPP 320-211

0111 AIB 0013 D-AIPR 320-211

0112 AIB 0503 TS-INK 320-211

0113 AIB 0002 S5-AAB 320-231

0114 AIB 0003 S5-AAC 320-231

0115 AIB 0072 F-GHQE 320-211

0116 AIB 0014 D-AIPS 320-211

0117 AIB 0015 D-AIPT 320-211

0118 AIB 0309 N309US 320-211

0119 AIB 0001 TS-IMB 320-211

0120 AIB 0010 G-BUSK 320-211

0121 AIB 0310 N310NW 320-211

0122 AIB 0205 C-FDRP 320-211

0123 AIB 0007 TS-IME 320-211

0124 AIB 0002 TS-IMC 320-211

0125 AIB 0311 N311US 320-211

0126 AIB 0206 C-FDSN 320-211

0127 AIB 0207 C-FDST 320-211

0128 AIB 0037 F-GFKN 320-211

0129 AIB 0038 F-GFKO 320-211

0130 AIB 0073 F-GHQF 320-211

0131 AIB 0226 F-GLGM 320-212

0132 AIB 0002 TC-FBE 320-212

0133 AIB 0039 F-GFKP 320-211

0134 AIB 0001 EC-GRE 320-211

0135 AIB 0016 D-AIPU 320-211

0136 AIB 0002 EC-GRF 320-211





0137 AIB 0017 D-AIPW 320-211

0138 AIB 0001 TC-SKJ 320-211

0139 AIB 0002 B-MAY 320-211

0140 AIB 0009 VP-BQY 320-211

0141 AIB 0208 C-FDSU 320-211

0142 AIB 0010 SX-BVD 320-211

0143 AIB 0003 EC-GRG 320-211

0144 AIB 0201 F-GJVA 320-211

0145 AIB 0202 F-GJVB 320-211

0146 AIB 0004 EC-GRH 320-211

0147 AIB 0018 D-AIPX 320-211

0148 AIB 0003 TC-SKK 320-211

0149 AIB 0209 C-FFWI 320-211

0150 AIB 0210 C-FFWJ 320-211

0151 AIB 0004 JA8384 320-211

0152 AIB 0312 N312US 320-211

0153 AIB 0313 N313US 320-211

0154 AIB 0211 C-FFWM 320-211

0155 AIB 0074 F-GHQG 320-211

0156 AIB 0075 F-GHQH 320-211

0157 AIB 0011 VP-BQZ 320-211

0158 AIB 0005 EC-FCB 320-211

0159 AIB 0212 C-FFWN 320-211

0160 AIB 0314 N314US 320-211

0161 AIB 0019 D-AIPY 320-211

0162 AIB 0020 D-AIPZ 320-211

0163 AIB 0001 I-LINH 320-231

0164 AIB 0005 4R-ABF 320-231

0165 AIB 0001 SU-GBA 320-231





0166 AIB 0002 SU-GBB 320-231

0167 AIB 0005 JA8385 320-211

0168 AIB 0003 VT-EYD 320-231

0169 AIB 0006 4R-ABE 320-231

0170 AIB 0006 JA8386 320-211

0171 AIB 0315 N315US 320-211

0172 AIB 0021 D-AIQA 320-211

0173 AIB 0006 EC-FDB 320-211

0174 AIB 0401 C-GPWG 320-211

0175 AIB 0402 C-FPWE 320-211

0176 AIB 0007 EC-FDA 320-211

0177 AIB 0008 EC-GRI 320-211

0178 AIB 0003 SU-GBC 320-231

0179 AIB 0005 VT-EYE 320-231

0180 AIB 0005 5B-DBA 320-231

0181 AIB 0001 9K-AKA 320-212

0182 AIB 0002 9K-AKB 320-212

0183 AIB 0213 C-FTJO 320-211

0184 AIB 0076 F-GHQI 320-211

0185 AIB 0051 CS-TNA 320-211

0186 AIB 0040 F-GFKR 320-212

0187 AIB 0041 F-GFKS 320-212

0188 AIB 0042 F-GFKT 320-211

0189 AIB 0003 F-OHFR 320-212

0190 AIB 0004 F-OHFU 320-212

0191 AIB 0052 CS-TNB 320-211

0192 AIB 0316 N316US 320-211

0193 AIB 0006 G-VCED 320-231

0194 AIB 0004 SU-GBD 320-231





0195 AIB 0003 9K-AKC 320-212

0196 AIB 0007 JA8387 320-211

0197 AIB 0317 N317US 320-211

0198 AIB 0005 SU-GBE 320-231

0199 AIB 0009 EC-ICQ 320-211

0200 AIB 0022 D-AIQB 320-211

0201 AIB 0023 D-AIQC 320-211

0202 AIB 0024 D-AIQD 320-211

0203 AIB 0251 F-GLGG 320-211

0204 AIB 0001 F-GJVC 320-211

0205 AIB 0003 TS-IMD 320-211

0206 AIB 0318 N318US 320-211

0207 AIB 0010 EC-FGV 320-211

0208 AIB 0319 N319US 320-211

0209 AIB 0025 D-AIQE 320-211

0210 AIB 0403 C-GQCA 320-211

0211 AIB 0002 HB-IJZ 320-211

0212 AIB 0008 JA8388 320-211

0213 AIB 0320 N320US 320-211

0214 AIB 0077 F-GHQJ 320-211

0215 AIB 0004 EI-DOE 320-211

0216 AIB 0026 D-AIQF 320-211

0217 AIB 0027 D-AIQH 320-211

0218 AIB 0028 D-AIQK 320-211

0219 AIB 0009 JA8389 320-211

0220 AIB 0252 F-GLGH 320-211

0221 AIB 0053 LZ-BHD 320-211

0222 AIB 0054 TS-INE 320-211

0223 AIB 0011 EC-FGH 320-211





0224 AIB 0012 EC-FGR 320-211

0225 AIB 0501 VT-EYF 320-231

0226 AIB 0043 F-GFKU 320-211

0227 AIB 0044 F-GFKV 320-211

0228 AIB 0045 F-GFKX 320-211

0229 AIB 0012 EK 32008 320-211

0230 AIB 0502 UR-DAB 320-231

0231 AIB 0404 C-FPWD 320-211

0232 AIB 0405 C-FDCA 320-211

0233 AIB 0214 C-FTJP 320-211

0234 AIB 0101 CS-TNO 320-211

0235 AIB 0227 F-GKXB 320-212

0236 AIB 0083 F-GHQK 320-211

0237 AIB 0084 F-GHQM 320-211

0239 AIB 0078 F-GHQL 320-211

0240 AIB 0013 EC-ICR 320-211

0241 AIB 0014 EC-ICS 320-211

0242 AIB 0215 C-FTJQ 320-211

0243 AIB 0051 PT-MZP 320-231

0244 AIB 0003 F-GJVF 320-211

0245 AIB 0010 JA8390 320-211

0246 AIB 0015 TS-INM 320-211

0247 AIB 0504 VT-EVO 320-231

0248 AIB 0216 C-FTJR 320-211

0249 AIB 0052 ER-AXT 320-231

0250 AIB 0053 PT-MZO 320-231

0251 AIB 0054 PT-MZS 320-231

0252 AIB 0001 F-OHME 320-231

0253 AIB 0217 C-FTJS 320-211





0254 AIB 0218 C-FGYL 320-211

0255 AIB 0219 C-FGYS 320-211

0256 AIB 0006 5B-DBB 320-231

0257 AIB 0505 VT-EVP 320-231

0258 AIB 0101 9A-CTF 320-211

0259 AIB 0002 F-OHMF 320-231

0260 AIB 0003 F-OHMG 320-231

0261 AIB 0004 F-OHMH 320-231

0262 AIB 0321 N321US 320-211

0263 AIB 0322 N322US 320-211

0264 AIB 0016 EC-ICT 320-211

0265 AIB 0220 C-FKCK 320-211

0266 AIB 0017 EC-FLP 320-211

0267 AIB 0029 D-AIQL 320-211

0268 AIB 0030 D-AIQM 320-211

0269 AIB 0031 D-AIQN 320-211

0270 AIB 0403 F-GJVG 320-211

0272 AIB 0323 EI-DIR 320-211

0273 AIB 0324 N324US 320-211

0274 AIB 0018 EC-FLQ 320-211

0275 AIB 0005 F-OHMI 320-231

0276 AIB 0006 F-OHMJ 320-231

0277 AIB 0221 C-FKCO 320-211

0278 AIB 0080 F-GHQO 320-211

0279 AIB 0406 PK-RMA 320-212

0280 AIB 0507 N280RX 320-231

0281 AIB 0325 N325US 320-211

0282 AIB 0326 N326US 320-211

0283 AIB 0407 TC-FBY 320-212





0284 AIB 0408 C-FLSS 320-211

0285 AIB 0046 F-GFKY 320-211

0286 AIB 0047 F-GFKZ 320-211

0287 AIB 0048 F-GKXA 320-211

0288 AIB 0103 TC-FBF 320-212

R 0289 AIB 0201 A9C-EP 320-212

0290 AIB 0222 C-FKCR 320-211

0291 AIB 0508 N291MX 320-231

0292 AIB 0509 N292MX 320-231

0293 AIB 0002 F-GYAI 320-211

0294 AIB 0055 LZ-BHB 320-212

0295 AIB 0007 5B-DBC 320-231

0296 AIB 0007 F-OHMK 320-231

0297 AIB 0327 N327NW 320-211

0298 AIB 0328 N328NW 320-211

0299 AIB 0056 TS-INF 320-212

0300 AIB 0011 JA8391 320-211

0301 AIB 0057 TS-INI 320-211

0302 AIB 0409 C-FMEQ 320-211

0303 AIB 0019 EC-ICU 320-211

0304 AIB 0003 4R-ABC 320-231

0305 AIB 0410 LZ-BHE 320-212

0306 AIB 0329 N329NW 320-211

0307 AIB 0330 N330NW 320-211

0308 AIB 0511 VT-EVS 320-231

0309 AIB 0411 C-FLSU 320-211

0310 AIB 0223 YL-LCC 320-211

R 0311 AIB 0224 OE-LAS 320-211

0312 AIB 0020 EC-ICV 320-211





0313 AIB 0801 TC-OAC 320-212

0314 AIB 0512 VT-EVT 320-231

0315 AIB 0004 4R-ABD 320-231

0316 AIB 0008 5B-DBD 320-231

0317 AIB 0644 N644AW 320-231

0318 AIB 0331 N331NW 320-211

0319 AIB 0332 N332NW 320-211

0320 AIB 0008 F-OHML 320-231

0321 AIB 0009 F-OHMM 320-231

0322 AIB 0008 SU-GCL 320-231

0323 AIB 0021 EC-FNR 320-211

0324 AIB 0225 C-FKPT 320-211

0325 AIB 0802 A9C-EB 320-212

0326 AIB 0002 VT-EYG 320-231

0327 AIB 0515 VT-EVQ 320-231

0328 AIB 0012 JA8392 320-211

0329 AIB 0333 N333NW 320-211

0330 AIB 0226 C-FKOJ 320-211

0331 AIB 0105 4K-AZ54 320-212

0332 AIB 0001 N332MX 320-231

0333 AIB 0227 4X-ABC 320-211

0334 AIB 0055 PT-MZR 320-231

0335 AIB 0056 PT-MZQ 320-231

0336 AIB 0516 VT-EVR 320-231

0337 AIB 0081 F-GHQP 320-211

0338 AIB 0517 EI-DRG 320-231

0339 AIB 0334 EI-DIP 320-212

0340 AIB 0335 N335NW 320-212

0341 AIB 0228 C-FPDN 320-211





0342 AIB 0229 EC-KJG 320-211

0343 AIB 0106 OO-TCK 320-212

0344 AIB 0003 VT-EYH 320-231

0345 AIB 0803 TC-OAD 320-212

0346 AIB 0032 D-AIQP 320-211

0347 AIB 0501 N347TM 320-231

0348 AIB 0058 TS-IND 320-211

0349 AIB 0059 LZ-BHC 320-212

R 0350 AIB 0001 A6-EIZ 320-211

0351 AIB 0006 SU-GBF 320-231

0352 AIB 0082 F-GHQQ 320-211

0353 AIB 0010 F-OHMN 320-231

0354 AIB 0502 VT-EYJ 320-231

0355 AIB 0336 N336NW 320-212

0356 AIB 0022 EC-FQY 320-211

0357 AIB 0503 XA-UCZ 320-231

0358 AIB 0337 N337NW 320-212

0359 AIB 0231 YL-LCD 320-211

0360 AIB 0338 N338NW 320-212

0361 AIB 0009 N361DA 320-231

0362 AIB 0502 VT-EYC 320-231

0363 AIB 0503 I-LINB 320-231

0364 AIB 0002 TC-ONS 321-131

0365 AIB 0013 JA8393 320-211

0366 AIB 0007 SU-GBG 320-231

0367 AIB 0339 N339NW 320-212

0368 AIB 0012 N368MX 320-231

0369 AIB 0002 N369MX 320-231

0370 AIB 0004 TS-IMF 320-211





0371 AIB 0504 EI-DFO 320-211

0372 AIB 0340 N340NW 320-212

0373 AIB 0504 N304ML 320-231

0375 AIB 0804 A9C-ED 320-212

0376 AIB 0401 VT-EYA 320-231

0377 AIB 0085 F-GHQR 320-211

0378 AIB 0232 C-FMSX 320-211

0379 AIB 0001 G-MPCD 320-212

0380 AIB 0341 N341NW 320-212

0381 AIB 0342 N342NW 320-212

0382 AIB 0033 D-AIQR 320-211

0383 AIB 0014 JA8394 320-211

0384 AIB 0233 4X-ABD 320-211

0385 AIB 0001 TC-ONJ 321-131

0386 AIB 0402 VT-EYB 320-231

0387 AIB 0343 N343NW 320-212

0388 AIB 0344 N344NW 320-212

0389 AIB 0002 G-OZBB 320-212

0390 AIB 0005 TS-IMG 320-211

0391 AIB 0062 PK-RMC 320-212

0392 AIB 0003 G-MONX 320-212

0393 AIB 0001 I-LINF 320-231

0394 AIB 0002 AP-BGU 320-231

0395 AIB 0107 CS-TNE 320-211

0396 AIB 0020 VT-ESA 320-231

0398 AIB 0021 VT-ESB 320-231

0399 AIB 0345 N345NW 320-212

0400 AIB 0346 TS-INL 320-212

0401 AIB 0034 D-AIQS 320-211





0402 AIB 0006 TS-IMH 320-211

0403 AIB 0415 C-FNVU 320-211

0404 AIB 0416 C-FNVV 320-211

0405 AIB 0008 N405MX 320-231

0406 AIB 0002 4R-ABB 320-231

R 0407 AIB 0202 A9C-ER 320-212

0408 AIB 0347 N347NW 320-212

R 0409 AIB 0251 A9C-EO 320-212

0410 AIB 0348 N348NW 320-212

0411 AIB 0505 VT-EYK 320-231

0412 AIB 0107 D-AIRH 321-131

0413 AIB 0015 JA8395 320-211

0414 AIB 0003 I-LING 320-231

0415 AIB 0007 N415MX 320-231

0416 AIB 0022 VT-ESC 320-231

0417 AIB 0349 N349NW 320-212

0418 AIB 0350 N350NA 320-212

0419 AIB 0805 A9C-EE 320-212

0420 AIB 0109 LV-BNZ 320-212

0421 AIB 0806 EI-DNP 320-212

0422 AIB 0502 6Y-JMB 320-212

0423 AIB 0023 VT-ESD 320-231

0424 AIB 0506 G-CRPH 320-231

0425 AIB 0101 OO-TCN 320-232

0426 AIB 0234 EC-KBM 320-211

0427 AIB 0001 EI-DZR 320-212

0428 AIB 0053 N428MX 320-231

0429 AIB 0518 G-BYTH 320-231

0430 AIB 0004 XA-TXT 320-231





0431 AIB 0024 VT-ESE 320-231

0432 AIB 0025 VT-ESF 320-231

0434 AIB 0005 I-BIXU 321-112

0435 AIB 0401 N401UA 320-232

0436 AIB 0110 LV-BOJ 320-212

0437 AIB 0525 G-GTDF 320-231

0438 AIB 0807 EC-JRC 320-212

0439 AIB 0402 N402UA 320-232

0440 AIB 0057 PT-MZN 320-231

0441 AIB 0509 PK-YVE 320-231

0442 AIB 0403 N403UA 320-232

0443 AIB 0005 AP-BGV 320-231

0444 AIB 0519 EI-DOD 320-231

0445 AIB 0808 EC-JTA 320-212

0446 AIB 0501 YL-LCF 320-212

0447 AIB 0006 N447MX 320-231

0448 AIB 0640 N640AW 320-232

0449 AIB 0520 PK-YVD 320-231

0450 AIB 0404 N404UA 320-232

0451 AIB 0026 VT-ESG 320-231

0452 AIB 0405 N405UA 320-232

0453 AIB 0125 PT-MZM 320-232

0454 AIB 0406 N406UA 320-232

0455 AIB 0301 VT-WAA 320-232

0456 AIB 0407 N407UA 320-232

0457 AIB 0408 N408UA 320-232

0458 AIB 0101 D-AIRA 321-131

0459 AIB 0809 A9C-EI 320-212

0460 AIB 0053 TC-OGK 320-233





0461 AIB 0054 TC-OGL 320-233

0462 AIB 0409 N409UA 320-232

0463 AIB 0410 N410UA 320-232

0464 AIB 0411 N411UA 320-232

0465 AIB 0412 N412UA 320-232

0466 AIB 0810 A9C-EJ 320-212

0467 AIB 0521 N467RX 320-231

0468 AIB 0102 D-AIRB 321-131

0469 AIB 0027 VT-ESH 320-231

0470 AIB 0413 N413UA 320-232

0471 AIB 0302 VT-WAB 320-232

0472 AIB 0414 N414UA 320-232

0473 AIB 0103 D-AIRC 321-131

0474 AIB 0104 D-AIRD 321-131

0475 AIB 0415 N415UA 320-232

0476 AIB 0522 G-GTDL 320-231

0477 AIB 0001 I-BIXA 321-112

0478 AIB 0523 VT-EYI 320-231

0479 AIB 0416 N416UA 320-232

0480 AIB 0524 VT-EYL 320-231

0482 AIB 0016 JA8396 320-211

0483 AIB 0417 N417UA 320-232

0484 AIB 0105 D-AIRE 321-131

0485 AIB 0418 N418UA 320-232

0486 AIB 0028 VT-ESI 320-231

0487 AIB 0419 N419UA 320-232

0488 AIB 0002 I-BIXE 321-112

0489 AIB 0420 N420UA 320-232

0490 AIB 0029 VT-ESJ 320-231





0491 AIB 0411 F-GJVW 320-211

0492 AIB 0030 VT-ESK 320-231

0493 AIB 0106 D-AIRF 321-131

0494 AIB 0003 I-BIXI 321-112

0495 AIB 0004 I-BIXO 321-112

0496 AIB 0054 EC-JIB 320-232

0497 AIB 0812 A9C-EL 320-212

0498 AIB 0101 F-GMZA 321-111

0499 AIB 0031 VT-ESL 320-231

0500 AIB 0421 N421UA 320-232

0501 AIB 0017 JA8609 320-211

0502 AIB 0108 D-AIRK 321-131

0503 AIB 0422 N422UA 320-232

0504 AIB 0423 N423UA 320-232

0505 AIB 0109 D-AIRL 321-131

0506 AIB 0424 N424UA 320-232

0507 AIB 0018 JA8654 320-211

0508 AIB 0425 N425UA 320-232

0509 AIB 0102 F-GMZB 321-111

0510 AIB 0426 N426UA 320-232

0511 AIB 0008 TS-IMI 320-211

0512 AIB 0427 N427UA 320-232

0513 AIB 0011 I-BIXL 321-112

0514 AIB 0012 I-BIXM 321-112

0515 AIB 0009 I-BIXF 321-112

0516 AIB 0010 I-BIXG 321-112

0517 AIB 0276 F-GYAP 321-111

0518 AIB 0110 D-AIRM 321-131

0519 AIB 0277 F-GYAZ 321-111





0520 AIB 0300 HB-IOC 321-111

0521 AIB 0103 F-GMZC 321-111

0522 AIB 0301 HB-IOD 321-111

0523 AIB 0428 N428UA 320-232

0524 AIB 0006 I-BIXB 321-112

0525 AIB 0051 EI-DXY 320-212

0526 AIB 0007 I-BIXC 321-112

0527 AIB 0619 N619AW 320-232

0528 AIB 0001 VP-BRB 320-212

0529 AIB 0104 F-GMZD 321-111

0530 AIB 0001 EP-MHK 320-232

0531 AIB 0019 JA8304 320-211

0532 AIB 0008 I-BIXD 321-112

0533 AIB 0001 F-GYFK 320-214

0534 AIB 0020 JA8313 320-211

0535 AIB 0280 F-GYAN 321-111

0537 AIB 0814 A9C-EN 320-212

0538 AIB 0101 B-22601 321-131

0539 AIB 0429 N429UA 320-232

0540 AIB 0051 B-2340 320-232

0541 AIB 0302 HB-IOF 321-111

0542 AIB 0105 EI-CUM 320-232

0543 AIB 0605 N605AW 320-232

0544 AIB 0105 F-GMZE 321-111

0545 AIB 0100 HB-IJB 320-214

0546 AIB 0285 C-GBIP 319-114

0548 AIB 0002 F-GYFL 320-214

0549 AIB 0021 JA8300 320-211

0550 AIB 0201 B-2286 321-131





0551 AIB 0052 B-2341 320-232

0552 AIB 0476 OE-LBA 321-111

0553 AIB 0101 HB-IJD 320-214

0554 AIB 0022 JA8400 320-211

0555 AIB 0102 B-22602 321-131

0556 AIB 0053 B-2342 320-233

0557 AIB 0202 B-MAB 321-131

0558 AIB 0001 F-HBAE 320-233

0559 AIB 0102 HB-IJE 320-214

0560 AIB 0111 D-AIRN 321-131

0561 AIB 0002 F-HBAD 320-233

0562 AIB 0103 HB-IJF 320-214

0563 AIB 0112 D-AIRO 321-131

0564 AIB 0113 D-AIRP 321-131

0565 AIB 0602 N602AW 320-232

0566 AIB 0232 XA-MXF 320-214

0567 AIB 0114 D-AIRR 321-131

0568 AIB 0430 N430UA 320-232

0569 AIB 0003 JY-AYI 320-212

0570 AIB 0477 OE-LBB 321-111

0571 AIB 0431 N431UA 320-232

0572 AIB 0251 C-FYNS 319-114

0573 AIB 0054 B-6025 320-232

0574 AIB 0104 HB-IJH 320-214

0575 AIB 0001 EP-MHN 320-232

0576 AIB 0013 I-BIXN 321-112

0577 AIB 0105 HB-IJI 320-214

0578 AIB 0001 HB-IPV 319-112

0579 AIB 0552 A9C-BAY 320-212





0580 AIB 0052 EC-JRX 320-232

0581 AIB 0478 OE-LBC 321-111

0582 AIB 0055 B-6026 320-232

0583 AIB 0014 I-BIXP 321-112

0584 AIB 0642 N642AW 320-232

0585 AIB 0106 HB-IJJ 320-214

0586 AIB 0015 I-BIXQ 321-112

0587 AIB 0432 N432UA 320-232

0588 AIB 0202 F-OOUA 319-112

0589 AIB 0433 N433UA 320-232

0590 AIB 0001 VN-A301 320-214

0591 AIB 0202 B-2293 321-131

0592 AIB 0434 N434UA 320-232

0593 AIB 0016 I-BIXR 321-112

0594 AIB 0002 VN-A302 320-214

0595 AIB 0115 D-AIRS 321-131

0596 AIB 0107 HB-IJK 320-214

0597 AIB 0204 B-MAR 321-131

0598 AIB 0901 F-GPMA 319-113

0599 AIB 0017 I-BIXS 321-112

0600 AIB 0902 F-GPMB 319-113

0601 AIB 0003 VN-A303 320-214

0603 AIB 0108 HB-IJL 320-214

0604 AIB 0205 TC-TUB 321-131

0605 AIB 0004 VN-A304 320-214

0606 AIB 0104 B-22605 321-131

0607 AIB 0005 VN-A305 320-214

0608 AIB 0903 F-GPMC 319-113

0609 AIB 0201 D-AILA 319-114





0610 AIB 0202 D-AILB 319-114

0611 AIB 0006 VN-A306 320-214

0612 AIB 0002 HB-IPX 319-112

0613 AIB 0435 N435UA 320-232

0614 AIB 0206 TC-TUC 321-131

0615 AIB 0014 F-OKRM 320-211

0616 AIB 0203 D-AILC 319-114

0617 AIB 0007 VN-A307 320-214

0618 AIB 0904 F-GPMD 319-113

0619 AIB 0008 VN-A308 320-214

0620 AIB 0207 B-MAF 321-131

0621 AIB 0003 HB-IPY 319-112

0622 AIB 0015 ER-AXV 320-211

0623 AIB 0204 D-AILD 319-114

0624 AIB 0001 6Y-JAF 320-214

0625 AIB 0905 F-GPME 319-113

0626 AIB 0002 6Y-JAG 320-214

0627 AIB 0205 D-AILE 319-114

0628 AIB 0003 6Y-JAI 320-214

0629 AIB 0205 CS-TTQ 319-112

0630 AIB 0004 6Y-JAJ 320-214

0631 AIB 0208 B-MAG 321-131

0633 AIB 0103 B-HTF 321-231

0634 AIB 0252 C-FYIY 319-114

0635 AIB 0109 HB-IJM 320-214

0636 AIB 0206 D-AILF 319-114

0637 AIB 0906 F-GPMF 319-113

0638 AIB 0436 N436UA 320-232

0639 AIB 0253 F-HBMI 319-114





0640 AIB 0104 TC-OGI 320-232

0641 AIB 0207 D-AILH 319-114

0642 AIB 0282 F-GYAO 321-111

0643 AIB 0110 HB-IJN 320-214

0644 AIB 0101 OO-SSP 319-113

0645 AIB 0553 A9C-BAZ 320-212

0646 AIB 0013 D-AKNF 319-112

0647 AIB 0801 EI-DVD 319-113

0648 AIB 0009 VN-A309 320-214

R 0649 AIB 0151 VP-BIU 319-114

0650 AIB 0010 VN-A311 320-214

0651 AIB 0208 D-AILI 319-114

0652 AIB 0116 D-AIRT 321-131

0653 AIB 0201 OO-TCP 320-214

0654 AIB 0014 D-AKNG 319-112

0655 AIB 0437 N437UA 320-232

0656 AIB 0255 C-FYJE 319-114

0657 AIB 0202 F-GRSE 320-214

0658 AIB 0023 JA8997 320-211

0659 AIB 0002 D-ATRA 320-232

0660 AIB 0802 EI-DVU 319-113

0661 AIB 0603 N603AW 320-232

0662 AIB 0017 EC-KIK 320-211

0663 AIB 0252 TC-OAE 321-231

0664 AIB 0303 HB-IOH 321-111

0665 AIB 0051 B-2356 320-214

0666 AIB 0351 6Y-JMD 321-211

0667 AIB 0103 SU-LBI 320-232

0668 AIB 0253 TC-OAF 321-231





0669 AIB 0024 JA8946 320-211

0670 AIB 0256 C-FYJG 319-114

0671 AIB 0554 9A-CTM 320-211

0672 AIB 0257 C-FYJH 319-114

0673 AIB 0111 HB-IJO 320-214

0674 AIB 0101 OK-CEC 321-211

R 0675 AIB 0101 A9C-ES 321-211

0676 AIB 0107 TC-OGJ 320-232

0677 AIB 0001 G-OMYJ 321-211

0678 AIB 0438 N438UA 320-232

0679 AIB 0209 D-AILK 319-114

0680 AIB 0101 SU-GBT 321-231

0681 AIB 0112 HB-IJP 320-214

0682 AIB 0258 C-FYJI 319-114

0683 AIB 0439 N439UA 320-232

0684 AIB 0102 OK-CED 321-211

0685 AIB 0025 JA8947 320-211

0686 AIB 0801 N801UA 319-131

0687 AIB 0102 SU-GBU 321-231

0688 AIB 0259 C-FYJP 319-114

0689 AIB 0210 D-AILL 319-114

0690 AIB 0802 N802UA 319-131

0691 AIB 0260 C-FYKC 319-114

0692 AIB 0117 D-AIRU 321-131

0693 AIB 0261 C-FYKR 319-114

0694 AIB 0211 D-AILM 319-114

0695 AIB 0262 C-FYKW 319-114

0696 AIB 0001 B-2343 320-233

0697 AIB 0263 C-FZUG 319-114





0698 AIB 0002 B-2345 320-233

0699 AIB 0118 D-AIRW 321-131

0700 AIB 0212 D-AILN 319-114

0701 AIB 0113 HB-IJQ 320-214

0702 AIB 0440 N440UA 320-232

0703 AIB 0114 HB-IJR 320-214

0704 AIB 0003 B-2346 320-233

0705 AIB 0004 B-2347 320-233

0706 AIB 0001 RP-C3221 320-214

0707 AIB 0201 B-2354 320-214

0709 AIB 0005 B-2459 320-232

0710 AIB 0006 B-2401 320-232

0711 AIB 0264 C-FZUH 319-114

R 0712 AIB 0007 B-2350 320-232

0713 AIB 0004 HB-IPU 319-112

0714 AIB 0101 VP-BFY 320-214

0715 AIB 0103 SU-GBV 321-231

0716 AIB 0003 G-OMYA 320-214

0717 AIB 0213 D-AILP 319-114

0718 AIB 0008 B-2351 320-233

0719 AIB 0265 C-FZUJ 319-114

0720 AIB 0009 B-2352 320-232

0721 AIB 0266 C-FZUL 319-114

0722 AIB 0010 B-2353 320-232

0723 AIB 0214 D-AILR 319-114

0724 AIB 0202 B-2355 320-214

0725 AIB 0104 SU-GBW 321-231

0726 AIB 0101 YL-BCB 320-211

0727 AIB 0005 HB-IPT 319-112





0728 AIB 0267 C-GAPY 319-114

0729 AIB 0215 D-AILS 319-114

0730 AIB 0102 VP-BFX 320-214

0731 AIB 0105 B-22606 321-131

0732 AIB 0268 C-GAQL 319-114

0733 AIB 0201 UR-DAC 320-233

0734 AIB 0006 HB-IPS 319-112

0735 AIB 0006 VP-BFZ 320-214

0736 AIB 0269 C-GAQX 319-114

0737 AIB 0007 I-EEZH 320-214

0738 AIB 0216 D-AILT 319-114

0739 AIB 0101 SU-LBH 320-233

0740 AIB 0270 C-GAQZ 319-114

0741 AIB 0202 N452TA 320-233

0742 AIB 0271 C-GARG 319-114

0743 AIB 0102 SU-LBG 320-233

0744 AIB 0217 D-AILU 319-114

0745 AIB 0003 RP-C3223 320-214

0746 AIB 0106 B-22607 321-131

0747 AIB 0203 UR-DAD 320-233

0748 AIB 0803 N803UA 319-131

0749 AIB 0008 I-EEZI 320-214

0750 AIB 0001 CS-TTA 319-111

0751 AIB 0441 N441UA 320-232

0752 AIB 0272 C-GARJ 319-114

0754 AIB 0052 B-2357 320-214

0755 AIB 0002 CS-TTB 319-111

0756 AIB 0051 B-HSD 320-232

0757 AIB 0273 C-GARO 319-114





0758 AIB 0126 PT-MZV 320-232

0759 AIB 0804 N804UA 319-131

0760 AIB 0109 AP-BGW 320-232

R 0761 AIB 0102 A9C-ET 321-211

0762 AIB 0647 N647AW 320-232

0763 AIB 0051 CS-TTC 319-111

0764 AIB 0009 VP-BXS 320-214

0765 AIB 0018 I-BIXT 321-112

0766 AIB 0351 N351NW 320-212

0767 AIB 0001 9A-CTG 319-112

0768 AIB 0426 OE-LBN 320-214

0769 AIB 0274 C-GBHM 319-114

0770 AIB 0648 N648AW 320-232

0771 AIB 0001 TC-FBG 321-231

0772 AIB 0001 B-2360 320-214

0773 AIB 0275 C-GBHN 319-114

0774 AIB 0001 D-AICA 320-212

0775 AIB 0352 6Y-JME 321-211

0776 AIB 0427 OE-LBO 320-214

0777 AIB 0131 F-GTAD 321-212

0778 AIB 0352 N352NW 320-212

0779 AIB 0276 C-GBHO 319-114

0780 AIB 0442 N442UA 320-232

0781 AIB 0101 G-OOPH 321-211

0782 AIB 0115 HB-IJS 320-214

0783 AIB 0805 N805UA 319-131

0784 AIB 0052 B-HSE 320-232

0785 AIB 0277 C-GBHR 319-114

0786 AIB 0353 N353NW 320-212





0787 AIB 0151 TC-OAI 321-231

0788 AIB 0806 N806UA 319-131

0790 AIB 0052 CS-TTD 319-111

0791 AIB 0003 B-22310 320-232

0792 AIB 0104 EI-LVD 321-231

0793 AIB 0002 TS-INN 320-212

0794 AIB 0015 D-AKNH 319-112

0795 AIB 0555 CS-TKJ 320-212

0796 AIB 0132 F-GTAE 321-212

0797 AIB 0428 OE-LBP 320-214

0798 AIB 0807 N807UA 319-131

0799 AIB 0002 B-2361 320-214

0800 AIB 0278 C-GBHY 319-114

0801 AIB 0354 N354NW 320-212

0802 AIB 0102 HL7767 321-231

0803 AIB 0649 N649AW 320-232

0804 AIB 0808 N808UA 319-131

0805 AIB 0111 B-MAH 320-232

0806 AIB 0302 TC-JMC 321-231

0807 AIB 0355 N355NW 320-212

0808 AIB 0002 F-GUAA 321-211

0809 AIB 0003 D-AICC 320-212

0810 AIB 0301 TC-JMD 321-231

0811 AIB 0052 TC-SKI 321-231

0812 AIB 0001 B-HSG 320-232

0813 AIB 0279 C-GBHZ 319-114

0814 AIB 0556 EI-DJH 320-212

0815 AIB 0501 EI-CPC 321-211

0816 AIB 0053 EI-DOP 320-232





0817 AIB 0280 C-GBIA 319-114

0818 AIB 0356 N356NW 320-212

0819 AIB 0019 I-BIXV 321-112

0820 AIB 0443 N443UA 320-232

0821 AIB 0003 CS-TTE 319-111

0822 AIB 0004 B-22311 320-232

0823 AIB 0003 F-HBAB 321-211

0824 AIB 0444 N444UA 320-232

0825 AIB 0809 N809UA 319-131

0826 AIB 0445 N445UA 320-232

0827 AIB 0284 F-GYAQ 321-211

0828 AIB 0003 B-2362 320-214

0829 AIB 0281 C-GBIJ 319-114

0830 AIB 0357 N357NW 320-212

0831 AIB 0282 C-GBIK 319-114

0832 AIB 0358 N358NW 320-212

0833 AIB 0002 9A-CTH 319-112

0834 AIB 0446 N446UA 320-232

0835 AIB 0001 G-MIDC 321-231

0836 AIB 0447 N447UA 320-232

0837 AIB 0004 CS-TTF 319-111

0838 AIB 0053 B-2358 320-214

0839 AIB 0003 HA-LPA 320-233

0840 AIB 0283 C-GBIM 319-114

0841 AIB 0502 EI-CPD 321-211

0842 AIB 0448 N448UA 320-232

0843 AIB 0810 N810UA 319-131

0844 AIB 0102 N102UW 320-214

0845 AIB 0284 C-GBIN 319-114





0846 AIB 0359 N359NW 320-212

0847 AIB 0811 N811UA 319-131

0848 AIB 0020 I-BIXZ 321-112

0849 AIB 0011 B-2365 320-232

0850 AIB 0812 N812UA 319-131

0851 AIB 0449 N449UA 320-232

0852 AIB 0002 G-OOPE 321-211

0853 AIB 0218 D-AILW 319-114

0854 AIB 0054 B-2359 320-214

0855 AIB 0002 TC-FBT 321-231

0856 AIB 0650 N650AW 320-232

0857 AIB 0002 EP-MHJ 320-232

0858 AIB 0813 N813UA 319-131

0859 AIB 0012 B-2366 320-232

0860 AIB 0219 D-AILX 319-114

0861 AIB 0103 N103US 320-214

0862 AIB 0814 N814UA 319-131

0863 AIB 0104 N104UW 320-214

0864 AIB 0201 G-OZBL 321-231

0865 AIB 0451 N451UA 320-232

0866 AIB 0651 N651AW 320-232

0867 AIB 0815 N815UA 319-131

0868 AIB 0105 N105UW 320-214

0869 AIB 0101 TS-IMJ 319-114

0870 AIB 0245 CS-TQD 320-214

0871 AIB 0816 N816UA 319-131

0872 AIB 0059 B-6256 320-232

0873 AIB 0817 N817UA 319-131

0874 AIB 0060 B-6257 320-233





0875 AIB 0220 D-AILY 319-114

0876 AIB 0203 B-2376 320-214

0877 AIB 0054 B-HSH 320-232

0878 AIB 0101 B-2370 321-231

0879 AIB 0004 B-6258 320-214

0880 AIB 0102 TS-IMK 319-114

0881 AIB 0013 B-2367 320-232

0882 AIB 0818 N818UA 319-131

0883 AIB 0004 B-2363 320-214

0884 AIB 0004 D-AICD 320-212

0885 AIB 0700 N700UW 319-112

0886 AIB 0001 YK-AKA 320-232

0887 AIB 0119 D-AIRX 321-131

0888 AIB 0002 F-HBAC 320-214

0889 AIB 0801 N801AW 319-132

0890 AIB 0701 N701UW 319-112

0891 AIB 0285 F-GYAR 321-211

0892 AIB 0004 HA-LPC 320-233

0893 AIB 0819 N819UA 319-131

0894 AIB 0005 D-AICE 320-212

0895 AIB 0014 B-2368 320-232

0896 AIB 0702 N702UW 319-112

0897 AIB 0055 B-2372 320-214

0898 AIB 0820 N820UA 319-131

0899 AIB 0002 9V-SLB 320-232

0900 AIB 0015 B-2369 320-232

0901 AIB 0120 D-AIRY 321-131

0902 AIB 0057 B-6049 320-233

0903 AIB 0360 N360NW 320-212





0904 AIB 0703 N703UW 319-112

0905 AIB 0006 D-AICF 320-212

0906 AIB 0005 CS-TTG 319-111

0907 AIB 0361 N361NW 320-212

0908 AIB 0001 B-MAJ 321-231

0909 AIB 0056 B-2375 320-214

0910 AIB 0001 A6-ESH 319-133

0911 AIB 0362 N362NW 320-212

0912 AIB 0058 B-2348 320-233

0913 AIB 0001 EK-RA01 319-132

0914 AIB 0005 B-2201 320-214

0915 AIB 0102 B-2371 321-231

0916 AIB 0001 D-ANNA 320-233

0917 AIB 0006 CS-TTH 319-111

0918 AIB 0002 YK-AKB 320-232

0919 AIB 0001 B-2373 320-233

0920 AIB 0479 OE-LBD 321-211

0921 AIB 0204 B-2377 320-214

0922 AIB 0704 N704US 319-112

0923 AIB 0363 N363NW 320-212

0924 AIB 0802 N802AW 319-132

0925 AIB 0101 B-2202 320-214

0926 AIB 0001 EI-CPE 321-211

0927 AIB 0001 A7-AAG 320-232

R 0928 AIB 0007 B-MAX 320-232

0929 AIB 0705 N705UW 319-112

0930 AIB 0055 B-HSI 320-232

0931 AIB 0803 N803AW 319-132

0932 AIB 0551 DG-EH 320-232





0933 AIB 0007 CS-TTI 319-111

0934 AIB 0201 G-MIDZ 320-232

0935 AIB 0480 OE-LBE 321-211

0936 AIB 0008 RP-C3229 320-214

0937 AIB 0001 SU-KBA 320-212

0938 AIB 0976 F-GRHA 319-111

0939 AIB 0057 B-2378 320-214

0940 AIB 0021 I-BIXH 321-112

0941 AIB 0001 OH-LZA 321-211

0942 AIB 0701 HB-IHX 320-214

0943 AIB 0552 VT-ADY 320-232

0944 AIB 0821 N821UA 319-131

0945 AIB 0101 CS-TNG 320-214

0946 AIB 0706 B-6152 319-112

0947 AIB 0702 HB-IHY 320-214

0948 AIB 0822 N822UA 319-131

0949 AIB 0707 B-6155 319-112

0950 AIB 0016 B-2391 320-232

0951 AIB 0101 I-BIKA 320-214

0952 AIB 0823 N823UA 319-131

0953 AIB 0652 N652AW 320-232

0954 AIB 0152 TC-OAK 321-231

0955 AIB 0452 N452UA 320-232

0956 AIB 0001 VN-A343 321-211

0957 AIB 0007 D-AICG 320-212

0958 AIB 0009 TS-IML 320-211

0959 AIB 0022 I-BIXJ 321-112

0960 AIB 0151 CS-TNH 320-214

0961 AIB 0002 OH-LZB 321-211





0962 AIB 0364 N364NW 320-212

0963 AIB 0053 N963DE 321-231

0964 AIB 0365 N365NW 320-212

0965 AIB 0824 N824UA 319-131

0966 AIB 0017 B-2392 320-232

0967 AIB 0058 B-2379 320-214

0968 AIB 0103 TC-IEF 321-231

0969 AIB 0003 9V-SLC 320-232

0970 AIB 0101 TS-IQA 321-211

0971 AIB 0008 D-AICH 320-212

0972 AIB 0708 N708UW 319-112

0973 AIB 0401 F-GRSI 320-214

0974 AIB 0104 TC-IEG 321-231

0975 AIB 0010 TS-IMM 320-211

0976 AIB 0001 PT-MZA 319-132

0977 AIB 0553 VT-ADZ 320-232

0978 AIB 0007 B-6328 320-214

0979 AIB 0053 CS-TTJ 319-111

0980 AIB 0825 N825UA 319-131

0981 AIB 0366 N366NW 320-212

0982 AIB 0102 CS-TNI 320-214

0983 AIB 0101 G-MARA 321-231

0984 AIB 0059 B-2205 320-214

0985 AIB 0951 F-GRHB 319-111

0986 AIB 0060 B-2206 320-214

0987 AIB 0304 HB-IOK 321-111

0988 AIB 0367 N367NW 320-212

0989 AIB 0826 N826UA 319-131

R 0990 AIB 0051 VN-A195 320-232





0991 AIB 0503 EI-CPF 321-211

0992 AIB 0101 EC-JZQ 320-214

0993 AIB 0101 B-HTD 321-231

0994 AIB 0418 B-2416 320-214

0995 AIB 0102 TS-IQB 321-211

0996 AIB 0368 N368NW 320-212

0997 AIB 0709 N709UW 319-112

0998 AIB 0977 F-GRHC 319-111

0999 AIB 0102 I-BIKE 320-214

1000 AIB 0978 F-GRHD 319-111

1001 AIB 0453 N453UA 320-232

1002 AIB 0901 TC-ANA 319-115

1003 AIB 0653 N653AW 320-232

1004 AIB 0153 TC-OAL 321-231

1005 AIB 0102 B-2203 320-214

1006 AIB 0102 F-HBAF 321-211

1007 AIB 0056 B-6027 320-233

1008 AIB 0054 AP-BRJ 321-231

1009 AIB 0151 9A-CTJ 320-214

1010 AIB 0002 PT-MZB 319-132

1011 AIB 0369 N369NW 320-212

1012 AIB 0503 TC-KTY 321-211

1013 AIB 0002 B-2397 320-233

1014 AIB 0202 G-MIDY 320-232

1015 AIB 0102 G-OJEG 321-231

1016 AIB 0016 D-AKNI 319-112

1017 AIB 0103 F-OIVU 321-211

1018 AIB 0007 HB-IPR 319-112

1019 AIB 0710 N710UW 319-112





1020 AIB 0952 F-GRHE 319-111

1021 AIB 0201 EC-HUH 321-211

1022 AIB 0827 N827UA 319-131

1023 AIB 0002 EI-CPG 321-211

1024 AIB 0102 B-HTE 321-231

1025 AIB 0953 F-GRHF 319-111

1026 AIB 0703 HB-IHZ 320-214

1027 AIB 0202 EC-HUI 321-211

1028 AIB 0201 B-2207 320-214

1029 AIB 0003 9A-CTI 319-112

1030 AIB 0202 B-2209 320-214

1031 AIB 0828 N828UA 319-131

1032 AIB 0003 YK-AKC 320-232

1033 AIB 0711 N711UW 319-112

1034 AIB 0008 CS-TTK 319-111

1035 AIB 0018 B-2393 320-232

1036 AIB 0954 F-GRHG 319-111

1037 AIB 0370 N370NW 320-212

1038 AIB 0712 N712US 319-112

1039 AIB 0019 B-2395 320-232

1040 AIB 0713 N713UW 319-112

1041 AIB 0061 B-2211 320-214

1042 AIB 0301 P4-NAS 321-231

1043 AIB 0804 N804AW 319-132

1044 AIB 0106 N106US 320-214

1045 AIB 0251 G-OZBM 321-231

1046 AIB 0714 N714US 319-112

1047 AIB 0102 EC-HAF 320-214

1048 AIB 0551 EI-DFP 319-112





1049 AIB 0805 N805AW 319-132

1050 AIB 0654 N654AW 320-232

1051 AIB 0715 N715UW 319-112

1052 AIB 0107 N107US 320-214

1053 AIB 0001 D-ADNA 319-133

1054 AIB 0001 SU-LBJ 320-214

1055 AIB 0716 N716UW 319-112

1056 AIB 0806 N806AW 319-132

1057 AIB 0020 B-2396 320-232

1058 AIB 0501 N301NB 319-114

1059 AIB 0103 EC-HAG 320-214

1060 AIB 0103 B-6285 321-231

1061 AIB 0108 N108UW 320-214

1062 AIB 0502 N302NB 319-114

R 1063 AIB 0005 EC-KLU 320-214

1064 AIB 0807 N807AW 319-132

1065 AIB 0109 N109UW 320-214

1066 AIB 0301 N471TA 319-132

1067 AIB 0105 EC-HDK 320-214

1068 AIB 0101 F-GYFM 319-112

1069 AIB 0717 N717UW 319-112

1070 AIB 0203 B-2208 320-214

1071 AIB 0001 VP-BTU 319-114

1072 AIB 0103 B-2400 320-214

1073 AIB 0101 OH-LVA 319-112

1074 AIB 0101 9V-SBA 319-132

1075 AIB 0655 N655AW 320-232

1076 AIB 0004 YK-AKD 320-232

1077 AIB 0001 D-AKNK 319-112





1078 AIB 0002 VP-BTV 319-114

1079 AIB 0656 N656AW 320-232

1080 AIB 0151 D-AISB 321-231

1081 AIB 0301 G-MRJK 320-214

1082 AIB 0001 G-EUPA 319-131

1083 AIB 0657 N657AW 320-232

1084 AIB 0002 D-AKNL 319-112

1085 AIB 0005 YK-AKE 320-232

1086 AIB 0533 F-OHJX 319-112

1087 AIB 0152 EC-HDN 320-214

1088 AIB 0808 N808AW 319-132

1089 AIB 0003 D-AKNM 319-112

1090 AIB 0003 VP-BTW 319-114

1091 AIB 0004 VP-BTX 319-114

1092 AIB 0003 PT-MZC 319-132

1093 AIB 0104 B-2399 320-214

1094 AIB 0003 EI-CPH 321-211

1095 AIB 0721 N721UW 319-112

1096 AIB 0004 PT-MZD 319-132

1097 AIB 0722 N722US 319-112

1098 AIB 0102 9V-SBB 319-132

1099 AIB 0106 EC-HDO 320-214

1100 AIB 0009 CS-TTL 319-111

1101 AIB 0107 EC-HDP 320-214

1102 AIB 0554 EI-DEY 319-112

1103 AIB 0005 PT-MZE 319-132

1104 AIB 0454 N454UA 320-232

1105 AIB 0455 N455UA 320-232

1106 AIB 0010 CS-TTM 319-111





1107 AIB 0102 OH-LVB 319-112

1108 AIB 0105 B-2398 320-214

1109 AIB 0723 N723UW 319-112

1110 AIB 0658 N658AW 320-232

1111 AIB 0809 N809AW 319-132

1112 AIB 0110 N110UW 320-214

1113 AIB 0302 N472TA 319-132

1114 AIB 0111 N111US 320-214

1115 AIB 0002 G-EUPB 319-131

1116 AIB 0810 N810AW 319-132

1117 AIB 0006 YK-AKF 320-232

1118 AIB 0003 G-EUPC 319-131

1119 AIB 0108 EC-HDT 320-214

1120 AIB 0011 CS-TTN 319-111

1121 AIB 0001 TS-INA 320-214

1122 AIB 0724 N724UW 319-112

1123 AIB 0503 N503JB 320-232

1124 AIB 0555 F-OHJY 319-112

1125 AIB 0031 I-EEZK 320-214

1126 AIB 0005 VP-BTN 319-114

1127 AIB 0012 CS-TTO 319-111

1128 AIB 0456 N456UA 320-232

1129 AIB 0006 VP-BTO 319-114

1130 AIB 0005 EC-IMU 320-214

1131 AIB 0007 VP-BTP 319-114

1132 AIB 0247 XA-IJT 320-214

1133 AIB 0133 F-GTAH 321-212

1134 AIB 0112 N112US 320-214

1135 AIB 0725 N725UW 319-112





1136 AIB 0004 D-AKNN 319-112

1137 AIB 0429 OE-LBQ 320-214

1138 AIB 0103 I-BIKI 320-214

1139 AIB 0006 PT-MZF 319-132

1140 AIB 0303 N473TA 319-132

1141 AIB 0113 N113UW 320-214

1142 AIB 0004 G-EUPD 319-131

1143 AIB 0101 PT-MZG 320-232

1144 AIB 0305 HB-IOL 321-111

1145 AIB 0102 F-GYJM 319-112

1146 AIB 0457 N457UA 320-232

1147 AIB 0005 D-AKNO 319-112

1148 AIB 0114 N114UW 320-214

1149 AIB 0101 VP-BTQ 319-114

1150 AIB 0430 OE-LBR 320-214

1151 AIB 0955 F-GRHH 319-111

1152 AIB 0266 N266AV 320-214

1153 AIB 0202 G-OZBN 321-231

1154 AIB 0351 EC-HGR 319-111

1155 AIB 0006 D-AKNP 319-112

1156 AIB 0504 N504JB 320-232

1157 AIB 0002 MM-62174 319-115

1158 AIB 0102 PT-MZH 320-232

1159 AIB 0304 N474TA 319-132

1160 AIB 0557 OO-SSG 319-112

1161 AIB 0152 D-AISC 321-231

1162 AIB 0248 XA-INJ 320-214

1163 AIB 0458 N458UA 320-232

1164 AIB 0008 VP-BTS 319-114





1165 AIB 0013 CS-TTP 319-111

1166 AIB 0659 N659AW 320-232

1167 AIB 0102 VP-BTT 319-114

1168 AIB 0104 I-BIKO 320-214

1169 AIB 0979 F-GRHI 319-111

1170 AIB 0007 D-AKNQ 319-112

1171 AIB 0009 RP-C3230 320-214

1172 AIB 0017 D-AKNJ 319-112

1173 AIB 0505 N505JB 320-232

1174 AIB 0005 G-MIDL 321-231

1175 AIB 0051 TS-INB 320-214

1176 AIB 0980 F-GRHJ 319-111

1177 AIB 0301 G-MIDX 320-232

1178 AIB 0812 N812AW 319-132

1179 AIB 0249 XA-AIJ 320-214

1180 AIB 0352 EC-HGS 319-111

1181 AIB 0103 CS-TNJ 320-214

1182 AIB 0730 N730US 319-112

1183 AIB 0203 EC-KEC 320-232

1184 AIB 0108 OH-LVH 319-112

1185 AIB 0003 OH-LZC 321-211

1187 AIB 0011 TS-IMN 320-211

1188 AIB 0153 D-AISD 321-231

1189 AIB 0431 OE-LBS 320-214

1190 AIB 0956 F-GRHK 319-111

1191 AIB 0514 N314NB 319-114

1192 AIB 0459 N459UA 320-232

1193 AIB 0005 G-EUPE 319-131

1194 AIB 0351 G-MEDE 320-232





1195 AIB 0301 VH-VWZ 321-231

1196 AIB 0604 N604AW 320-232

1197 AIB 0006 G-EUPF 319-131

1198 AIB 0267 N267AV 320-214

1199 AIB 0154 AP-BJA 321-231

1200 AIB 0153 EC-HGY 320-214

1201 AIB 0981 F-GRHL 319-111

R 1202 AIB 0003 EP-AGB 321-231

1203 AIB 0732 N732US 319-112

1204 AIB 0302 P4-OAS 321-231

1205 AIB 0733 N733UW 319-112

1206 AIB 0104 CS-TNK 320-214

1207 AIB 0252 G-OZBO 321-231

1208 AIB 0154 EC-HGZ 320-214

1209 AIB 0008 D-AKNR 319-112

1210 AIB 0010 RP-C3231 320-214

1211 AIB 0829 N829UA 319-131

1212 AIB 0001 VP-CVX 319-133

1213 AIB 0101 6Y-JMF 320-214

1214 AIB 0154 D-AISE 321-231

1215 AIB 0001 PR-MBP 320-232

1216 AIB 0982 F-GRHM 319-111

1217 AIB 0105 I-BIKU 320-214

1218 AIB 0155 AP-BJB 321-231

1219 AIB 0253 TC-JME 321-211

1220 AIB 0023 I-BIXK 321-112

1221 AIB 0155 EC-HHA 320-214

1222 AIB 0007 G-EUPG 319-131

1223 AIB 0813 N813AW 319-132





1224 AIB 0117 N117UW 320-214

1225 AIB 0008 G-EUPH 319-131

1226 AIB 0106 I-BIKB 320-214

1227 AIB 0253 HL7761 321-231

1228 AIB 0103 9V-SBC 319-132

1229 AIB 0109 EC-KNM 320-214

1230 AIB 0515 N315NB 319-114

1231 AIB 0105 CS-TNL 320-214

1232 AIB 0009 G-EUPJ 319-131

1233 AIB 0252 TC-JMF 321-211

1234 AIB 0660 N660AW 320-232

1235 AIB 0506 N506JB 320-232

1236 AIB 0010 G-EUPK 319-131

1237 AIB 0152 9A-CTK 320-214

1238 AIB 0103 G-DHJH 321-211

1239 AIB 0011 G-EUPL 319-131

1240 AIB 0101 D-ANNB 320-232

1241 AIB 0004 OH-LZD 321-211

1242 AIB 0201 EI-CVA 320-214

1243 AIB 0830 N830UA 319-131

1244 AIB 0250 XA-IJA 320-214

1245 AIB 0737 N737US 319-112

1246 AIB 0103 PT-MZI 320-232

1247 AIB 0353 EC-HGT 319-111

1248 AIB 0460 N460UA 320-232

1249 AIB 0516 N316NB 319-114

1250 AIB 0104 G-NIKO 321-211

1251 AIB 0104 PT-MZJ 320-232

1252 AIB 0004 9A-CTL 319-112





1253 AIB 0002 B-HSJ 320-232

1254 AIB 0738 N738US 319-112

1255 AIB 0110 EC-HSF 320-214

1256 AIB 0001 CS-TLU 319-133

1257 AIB 0102 D-ANNC 320-232

1258 AIB 0012 G-EUPM 319-131

1259 AIB 0251 XA-ITJ 320-214

1260 AIB 0155 D-AISF 321-231

1261 AIB 0013 G-EUPN 319-131

1262 AIB 0111 EC-HYC 320-214

1263 AIB 0739 B-6151 319-112

1264 AIB 0118 N118US 320-214

1265 AIB 0740 N740UW 319-112

1266 AIB 0461 N461UA 320-232

1267 AIB 0957 F-GRHN 319-111

1268 AIB 0119 N119US 320-214

1269 AIB 0741 N741UW 319-112

1270 AIB 0509 N509JB 320-232

1271 AIB 0958 F-GRHO 319-111

1272 AIB 0462 N462UA 320-232

1273 AIB 0156 D-AISG 321-231

1274 AIB 0662 N662AW 320-232

1275 AIB 0742 N742PS 319-112

1276 AIB 0001 EC-HPM 321-231

1277 AIB 0009 D-AKNS 319-112

1279 AIB 0014 G-EUPO 319-131

1280 AIB 0510 N510JB 320-232

1281 AIB 0814 N814AW 319-132

1282 AIB 0463 N463UA 320-232





1283 AIB 0559 EI-DEZ 319-112

1284 AIB 0661 N661AW 320-232

1285 AIB 0151 B-2331 319-112

1286 AIB 0005 B-6280 320-214

1287 AIB 0744 N744US 319-112

1288 AIB 0113 EC-HYD 320-214

1289 AIB 0745 N745VJ 319-112

1290 AIB 0464 N464UA 320-232

1291 AIB 0831 N831UA 319-131

1292 AIB 0114 EC-HUJ 320-214

1293 AIB 0104 B-6300 321-231

1294 AIB 0121 N121UW 320-214

1295 AIB 0015 G-EUPP 319-131

1296 AIB 0205 B-2210 320-214

1297 AIB 0746 N746UW 319-112

1298 AIB 0122 N122US 320-214

1299 AIB 0134 F-GTAI 321-212

R 1300 AIB 0001 SU-PBH 320-233

1301 AIB 0747 N747UW 319-112

1302 AIB 0516 N516JB 320-232

1303 AIB 0152 B-2332 319-112

1304 AIB 0001 LV-BRA 320-233

1305 AIB 0560 EI-DFA 319-112

1306 AIB 0001 OO-TCO 320-214

1307 AIB 0201 CS-TJE 321-211

1308 AIB 0252 XA-ALM 320-214

1309 AIB 0103 OH-LVC 319-112

1310 AIB 0123 N123UW 320-214

1311 AIB 0748 N748UW 319-112





1312 AIB 0204 B-2335 320-214

1313 AIB 0749 N749US 319-112

1314 AIB 0124 N124US 320-214

1315 AIB 0750 N750UW 319-112

1316 AIB 0062 B-2212 320-214

1317 AIB 0751 N751UW 319-112

1318 AIB 0115 EC-HUK 320-214

1319 AIB 0752 N752US 319-112

1320 AIB 0002 G-OOAR 320-214

1321 AIB 0832 N832UA 319-131

1322 AIB 0253 XA-ACO 320-214

1323 AIB 0815 N815AW 319-132

1324 AIB 0517 N317NB 319-114

1325 AIB 0518 N318NB 319-114

1326 AIB 0753 N753US 319-112

1327 AIB 0517 N517JB 320-232

1328 AIB 0754 N754VJ 319-112

1329 AIB 0016 G-EUPR 319-131

1330 AIB 0205 B-2336 320-214

1331 AIB 0755 N755US 319-112

1332 AIB 0002 CC-COD 320-233

1333 AIB 0002 EC-HQZ 321-231

1334 AIB 0211 EI-TAD 320-233

1335 AIB 0001 A7-HHJ 319-133

1336 AIB 0561 OO-SSK 319-112

1337 AIB 0035 D-AIQT 320-211

1338 AIB 0017 G-EUPS 319-131

1339 AIB 0212 PR-MBM 320-233

1340 AIB 0756 N756US 319-112





1341 AIB 0465 N465UA 320-232

1342 AIB 0757 N757UW 319-112

1343 AIB 0466 N466UA 320-232

1344 AIB 0959 F-GRHP 319-111

1345 AIB 0063 B-2213 320-214

1346 AIB 0519 N319NB 319-114

1347 AIB 0116 EC-HUL 320-214

1348 AIB 0758 N758US 319-112

1349 AIB 0101 EC-HRP 320-232

1350 AIB 0816 N816AW 319-132

R 1351 AIB 0003 LV-BRY 320-233

1352 AIB 0104 OH-LVD 319-112

R 1353 AIB 0002 SU-PBG 320-233

1354 AIB 0760 N760US 319-112

1355 AIB 0004 CC-COF 320-233

1356 AIB 0101 HL7594 321-131

1357 AIB 0206 B-2337 320-214

1358 AIB 0762 N762US 319-112

1359 AIB 0467 N467UA 320-232

1360 AIB 0763 N763US 319-112

1361 AIB 0207 B-2338 320-214

1362 AIB 0354 EC-HKO 319-111

1363 AIB 0468 N468UA 320-232

1364 AIB 0109 OH-LVI 319-112

1365 AIB 0036 D-AIQU 320-211

1366 AIB 0051 EC-HRG 321-231

1367 AIB 0037 D-AIQW 320-211

1368 AIB 0105 PT-MZK 320-232

1369 AIB 0764 N764US 319-112





1370 AIB 0302 G-OZBK 320-214

1371 AIB 0765 N765US 319-112

1372 AIB 0006 B-6250 320-214

1373 AIB 0817 N817AW 319-132

1375 AIB 0818 N818AW 319-132

1376 AIB 0106 PT-MZL 320-232

1377 AIB 0153 B-2333 319-112

1378 AIB 0766 N766US 319-112

1379 AIB 0156 EC-HQG 320-214

1380 AIB 0018 G-EUPT 319-131

1381 AIB 0009 D-AICI 320-212

1382 AIB 0767 N767UW 319-112

1383 AIB 0204 EC-KOX 320-232

1384 AIB 0019 G-EUPU 319-131

1385 AIB 0101 D-ALTB 320-214

1386 AIB 0154 B-2334 319-112

1387 AIB 0432 OE-LBT 320-214

1388 AIB 0563 OO-SSM 319-112

1389 AIB 0768 N768US 319-112

1390 AIB 0102 6Y-JMG 320-214

1391 AIB 0769 N769US 319-112

1392 AIB 0520 N320NB 319-114

1393 AIB 0770 N770UW 319-112

1394 AIB 0202 EI-CVB 320-214

1395 AIB 0819 N819AW 319-132

1396 AIB 0157 EC-HQI 320-214

1397 AIB 0820 N820AW 319-132

1398 AIB 0519 N519JB 320-232

1399 AIB 0202 CS-TJF 321-211





1400 AIB 0215 N470TA 320-233

1401 AIB 0833 N833UA 319-131

1402 AIB 0010 D-AICJ 320-212

1403 AIB 0161 N161UW 321-211

1404 AIB 0960 F-GRHQ 319-111

1405 AIB 0201 OH-LXA 320-214

1406 AIB 0821 N821AW 319-132

R 1407 AIB 0302 EC-KPX 320-232

1408 AIB 0302 VH-VWY 321-231

1409 AIB 0469 N469UA 320-232

1410 AIB 0822 N822AW 319-132

1411 AIB 0014 G-ERAA 320-232

1412 AIB 0162 N162UW 321-211

1413 AIB 0021 EC-KBU 320-214

1414 AIB 0521 N321NB 319-114

1415 AIB 0961 F-GRHR 319-111

1416 AIB 0011 D-AICK 320-212

1417 AIB 0163 N163US 321-211

1418 AIB 0205 G-MIDT 320-232

1419 AIB 0663 N663AW 320-232

1420 AIB 0834 N834UA 319-131

1421 AIB 0156 TC-OAN 321-231

1422 AIB 0004 9V-SLD 320-232

1423 AIB 0020 G-EUPV 319-131

1424 AIB 0303 G-MIDS 320-232

1425 AIB 0164 N189UW 321-211

1426 AIB 0835 N835UA 319-131

1427 AIB 0470 N470UA 320-232

R 1428 AIB 0108 G-OZBS 321-231





1429 AIB 0564 N429MX 319-112

1430 AIB 0158 EC-HQJ 320-214

1431 AIB 0165 N165US 321-211

1432 AIB 0471 N471UA 320-232

R 1433 AIB 0109 G-OZBP 321-231

1434 AIB 0522 N322NB 319-114

1435 AIB 0472 N472UA 320-232

1436 AIB 0166 N190UW 321-211

1437 AIB 0012 D-AICL 320-212

R 1438 AIB 0303 TC-ETF 321-231

1439 AIB 0001 OK-GEA 320-214

1440 AIB 0021 G-EUPW 319-131

1441 AIB 0151 D-ALTC 320-214

1442 AIB 0167 N167US 321-211

1443 AIB 0203 EI-CVC 320-214

1444 AIB 0962 F-GRHS 319-111

1445 AIB 0022 G-EUPX 319-131

1446 AIB 0520 N520JB 320-232

1447 AIB 0168 N191UW 321-211

1448 AIB 0107 I-BIKC 320-214

1449 AIB 0963 F-GRHT 319-111

1450 AIB 0002 OK-GEB 320-214

1451 AIB 0105 F-HCAI 321-211

1452 AIB 0521 N521JB 320-232

1453 AIB 0523 N323NB 319-114

1454 AIB 0159 EC-HQK 320-214

1455 AIB 0169 N169UW 321-211

1456 AIB 0524 N324NB 319-114

1457 AIB 0108 I-BIKD 320-214





1458 AIB 0481 OE-LBF 321-211

1459 AIB 0138 PR-MBG 320-232

1460 AIB 0836 N836UA 319-131

1461 AIB 0160 EC-HQL 320-214

1462 AIB 0170 N170US 321-211

1463 AIB 0823 N823AW 319-132

1464 AIB 0106 D-ANNG 320-232

1465 AIB 0171 N171US 321-211

1466 AIB 0023 G-EUPY 319-131

1467 AIB 0204 EI-CVD 320-214

1468 AIB 0001 0001 319-133

1469 AIB 0473 N473UA 320-232

1470 AIB 0202 OH-LXB 320-214

1471 AIB 0983 F-GRHU 319-111

1472 AIB 0172 N172US 321-211

1473 AIB 0109 I-BIKF 320-214

1474 AIB 0837 N837UA 319-131

1475 AIB 0474 N474UA 320-232

1476 AIB 0135 F-GTAJ 321-212

1477 AIB 0838 N838UA 319-131

1478 AIB 0433 OE-LBU 320-214

1479 AIB 0103 TS-IMO 319-114

1480 AIB 0110 I-BIKG 320-214

1481 AIB 0173 N173US 321-211

1482 AIB 0351 VT-WAC 320-233

1483 AIB 0525 N325NB 319-114

1484 AIB 0161 EC-HQM 320-214

1485 AIB 0001 F-RBFA 319-115

1486 AIB 0107 PT-MZT 320-232





1487 AIB 0105 A7-ADK 321-231

R 1488 AIB 0203 VQ-BAR 319-112

1489 AIB 0111 I-BIKL 320-214

1490 AIB 0824 N824AW 319-132

1491 AIB 0005 LV-BOI 320-233

1492 AIB 0174 N174US 321-211

1493 AIB 0152 D-ALTD 320-214

R 1494 AIB 0565 HZ-AJW 319-112

1495 AIB 0475 N475UA 320-232

1496 AIB 0175 N192UW 321-211

1497 AIB 0102 EC-HXA 320-232

1498 AIB 0526 N326NB 319-114

1499 AIB 0176 N176UW 321-211

1500 AIB 0061 B-6295 320-233

1501 AIB 0527 N327NB 319-114

1502 AIB 0651 F-GKXC 320-214

1503 AIB 0201 6Y-JMH 321-211

1504 AIB 0201 OE-LTU 320-214

1505 AIB 0964 F-GRHV 319-111

1506 AIB 0523 N523JB 320-232

1507 AIB 0839 N839UA 319-131

1508 AIB 0476 N476UA 320-232

1509 AIB 0218 N483TA 320-233

1510 AIB 0024 G-EUPZ 319-131

1511 AIB 0003 HL7703 321-131

1512 AIB 0006 LV-BHU 320-233

1513 AIB 0025 G-EUOA 319-131

1514 AIB 0477 N477UA 320-232

1515 AIB 0902 N902FR 319-111





1516 AIB 0117 EC-HTA 320-214

1517 AIB 0177 N177US 321-211

1518 AIB 0108 PT-MZU 320-232

1519 AIB 0178 N178US 321-211

1520 AIB 0528 N328NB 319-114

1521 AIB 0179 N179UW 321-211

1522 AIB 0840 N840UA 319-131

1523 AIB 0219 N484TA 320-233

1524 AIB 0965 F-GRHX 319-111

1525 AIB 0180 N180US 321-211

1526 AIB 0007 CC-COI 320-233

1527 AIB 0825 N825AW 319-132

1528 AIB 0524 N524JB 320-232

1529 AIB 0026 G-EUOB 319-131

1530 AIB 0118 EC-HTB 320-214

1531 AIB 0181 N181UW 321-211

1532 AIB 0208 B-2219 320-214

1533 AIB 0478 N478UA 320-232

1534 AIB 0826 N826AW 319-132

1535 AIB 0371 N371NW 320-212

1536 AIB 0182 N182UW 321-211

1537 AIB 0027 G-EUOC 319-131

1538 AIB 0479 N479UA 320-232

1539 AIB 0183 N183UW 321-211

1540 AIB 0119 EC-HTC 320-214

1541 AIB 0155 B-2215 319-112

1542 AIB 0209 B-2220 320-214

1543 AIB 0529 N329NB 319-114

1544 AIB 0203 OH-LXC 320-214





1545 AIB 0841 N841UA 319-131

1546 AIB 0103 D-ANND 320-232

1547 AIB 0827 N827AW 319-132

R 1548 AIB 0008 LV-BTM 320-233

1549 AIB 0530 N330NB 319-114

1550 AIB 0162 EC-HTD 320-214

1551 AIB 0156 B-2216 319-112

1552 AIB 0828 N828AW 319-132

1553 AIB 0202 D-ALTF 320-214

1554 AIB 0203 EC-IIG 321-211

1555 AIB 0480 N480UA 320-232

1556 AIB 0002 F-RBFB 319-115

1557 AIB 0104 D-ANNE 320-232

1558 AIB 0028 G-EUOD 319-131

1559 AIB 0481 N481UA 320-232

R 1560 AIB 0204 VQ-BAQ 319-112

1561 AIB 0005 9V-SLE 320-232

1562 AIB 0286 C-GITP 319-112

1563 AIB 0829 N829AW 319-132

R 1564 AIB 0260 N260AV 320-214

1565 AIB 0830 N830AW 319-132

1566 AIB 0001 A7-ADA 320-232

1567 AIB 0531 N331NB 319-114

1568 AIB 0009 CC-COL 320-233

1569 AIB 0842 N842UA 319-131

1570 AIB 0532 N332NB 319-114

1571 AIB 0001 G-OOPP 320-214

1572 AIB 0204 EC-IGK 321-211

1573 AIB 0843 N843UA 319-131





1574 AIB 0029 G-EUOE 319-131

1575 AIB 0301 PR-MBI 319-132

1576 AIB 0831 N831AW 319-132

1577 AIB 0287 C-GITR 319-112

1578 AIB 0003 EC-HZU 320-214

1579 AIB 0904 N904FR 319-111

1580 AIB 0109 PT-MZW 320-232

1581 AIB 0844 N844UA 319-131

1582 AIB 0533 N333NB 319-114

1583 AIB 0905 N905FR 319-111

1584 AIB 0482 N482UA 320-232

1585 AIB 0845 N845UA 319-131

1586 AIB 0483 N483UA 320-232

1587 AIB 0001 OY-KBK 321-232

1588 AIB 0204 OH-LXD 320-214

1589 AIB 0001 VP-CIE 319-133

1590 AIB 0030 G-EUOF 319-131

R 1591 AIB 0528 PR-MBX 320-232

1592 AIB 0001 3B-NBF 319-112

1593 AIB 0110 PT-MZZ 320-232

1594 AIB 0031 G-EUOG 319-131

1595 AIB 0111 PR-MAA 320-232

1596 AIB 0301 B-2280 321-231

1597 AIB 0101 EC-KEN 320-214

1598 AIB 0001 XA-UAQ 319-112

R 1599 AIB 0001 A6-AMM 318-112

1600 AIB 0846 N846UA 319-131

1601 AIB 0157 B-2217 319-112

1602 AIB 0451 C-GITU 321-211





1603 AIB 0158 B-2222 319-112

1604 AIB 0032 G-EUOH 319-131

1605 AIB 0002 C-GTDH 320-214

1606 AIB 0033 G-EUOI 319-131

1607 AIB 0302 D-ALSD 321-211

1608 AIB 0011 PR-MAH 319-132

1609 AIB 0484 N484UA 320-232

1610 AIB 0529 N529JB 320-232

1611 AIB 0452 C-GITY 321-211

1612 AIB 0051 N612MX 319-112

1613 AIB 0112 PT-MZX 320-232

1614 AIB 0302 B-2281 321-231

1615 AIB 0261 N261AV 320-214

1616 AIB 0966 F-GRHY 319-111

1617 AIB 0485 N485UA 320-232

1618 AIB 0201 N618MX 319-112

1619 AIB 0002 OY-KBL 321-232

1620 AIB 0486 N486UA 320-232

1621 AIB 0664 N664AW 320-232

1622 AIB 0967 F-GRHZ 319-111

1623 AIB 0453 C-GIUB 321-211

1624 AIB 0220 EI-TAB 320-233

1625 AIB 0002 N62TY 319-112

1626 AIB 0010 CC-COM 320-233

1627 AIB 0847 N847UA 319-131

1628 AIB 0113 PT-MZY 320-232

1629 AIB 0301 D-ALSA 321-211

1630 AIB 0288 XA-MXG 319-112

1631 AIB 0103 EC-IAZ 320-232





1632 AIB 0454 C-GIUE 321-211

1633 AIB 0372 N372NW 320-212

1634 AIB 0202 N634MX 319-112

1635 AIB 0005 HA-LPB 320-233

1636 AIB 0201 HL7711 321-231

1637 AIB 0003 G-OOPU 320-214

1638 AIB 0455 C-GIUF 321-211

1639 AIB 0210 B-2221 320-214

1640 AIB 0968 F-GRXA 319-111

1641 AIB 0373 N373NW 320-212

1642 AIB 0003 OY-KBB 321-232

1643 AIB 0832 N832AW 319-132

1644 AIB 0665 N665AW 320-232

1645 AIB 0969 F-GRXB 319-111

1646 AIB 0374 N374NW 320-212

1647 AIB 0848 N848UA 319-131

1648 AIB 0002 A7-ADB 320-232

1649 AIB 0849 N849UA 319-131

1650 AIB 0105 D-ANNF 320-232

1651 AIB 0184 N184US 321-211

1652 AIB 0533 PR-MBQ 320-232

1653 AIB 0850 N850UA 319-131

1654 AIB 0151 B-2225 319-111

1655 AIB 0120 EC-IEF 320-214

1656 AIB 0101 A7-CJA 319-133

1657 AIB 0102 EC-KBQ 320-214

1658 AIB 0136 F-GTAK 321-212

1659 AIB 0534 N334NB 319-114

1660 AIB 0805 N805FR 318-111





1661 AIB 0201 G-EUUA 320-232

1662 AIB 0535 N335NB 319-114

1663 AIB 0114 PR-MAB 320-232

1664 AIB 0851 N851UA 319-131

1665 AIB 0208 G-EUUH 320-232

1666 AIB 0185 N185UW 321-211

1667 AIB 0001 CS-TMW 320-214

1668 AIB 0289 VT-SCD 319-112

1669 AIB 0487 N487UA 320-232

1670 AIB 0251 HL7712 321-231

1671 AIB 0852 N852UA 319-131

1672 AIB 0115 PR-MAC 320-232

1673 AIB 0290 XA-MXH 319-112

1674 AIB 0121 EC-IEG 320-214

1675 AIB 0004 OY-KBH 321-232

1676 AIB 0221 EI-TAC 320-233

1677 AIB 0984 F-GRXC 319-111

1678 AIB 0205 OH-LXE 320-214

1679 AIB 0152 B-2223 319-111

1680 AIB 0488 N488UA 320-232

1681 AIB 0205 EC-ILO 321-211

1682 AIB 0104 EC-ICL 320-232

1683 AIB 0536 N336NB 319-114

1684 AIB 0906 N906FR 319-111

1685 AIB 0537 N337NB 319-114

1686 AIB 0008 B-6320 320-214

1687 AIB 0002 G-TTOB 320-232

1688 AIB 0853 N853UA 319-131

1689 AIB 0202 G-EUUB 320-232





1690 AIB 0051 G-MEDF 321-231

1691 AIB 0137 F-GTAL 321-212

1692 AIB 0208 PR-MHB 320-214

1693 AIB 0538 N338NB 319-114

1694 AIB 0122 EC-IEI 320-214

1695 AIB 0104 B-HTG 321-231

1696 AIB 0203 G-EUUC 320-232

1697 AIB 0304 G-MIDR 320-232

1698 AIB 0104 9V-SBD 319-132

1699 AIB 0985 F-GRXD 319-111

1700 AIB 0012 TS-IMP 320-211

1701 AIB 0186 N186US 321-211

1702 AIB 0489 N489UA 320-232

1703 AIB 0012 PR-MAI 319-132

1704 AIB 0187 N187US 321-211

1705 AIB 0534 N534JB 320-232

1706 AIB 0101 N706MX 319-112

1707 AIB 0103 G-OZBE 321-231

1708 AIB 0212 G-EUUL 320-232

1709 AIB 0539 N339NB 319-114

1710 AIB 0667 N667AW 320-232

1711 AIB 0052 G-MEDG 321-231

1712 AIB 0206 OH-LXF 320-214

1713 AIB 0203 CS-TJG 321-211

1714 AIB 0540 N340NB 319-114

1715 AIB 0003 G-TTOC 320-232

1716 AIB 0206 EC-ILP 321-211

1717 AIB 0209 PR-MHC 320-214

1718 AIB 0291 VT-SCE 319-112





1719 AIB 0235 C-GJVT 320-214

1720 AIB 0353 G-OOAV 321-211

1721 AIB 0056 B-HSK 320-232

1722 AIB 0201 I-BIMA 319-112

1723 AIB 0004 G-TTOD 320-232

1724 AIB 0188 N188US 321-211

1725 AIB 0262 N262AV 320-214

1726 AIB 0456 C-GJVX 321-211

1727 AIB 0253 D-APAC 319-132

1728 AIB 0490 N490UA 320-232

1729 AIB 0101 5B-DBO 319-132

1730 AIB 0222 N486TA 320-233

1731 AIB 0854 N854UA 319-131

1732 AIB 0305 G-MIDP 320-232

1733 AIB 0986 F-GRXE 319-111

1734 AIB 0053 HL7713 321-231

1735 AIB 0207 OH-LXG 320-214

1736 AIB 0123 EC-ILQ 320-214

1737 AIB 0855 N855UA 319-131

1738 AIB 0541 N341NB 319-114

1739 AIB 0535 N535JB 320-232

1740 AIB 0202 I-BIME 319-112

1741 AIB 0491 N491UA 320-232

R 1742 AIB 0292 XA-MXI 319-112

R 1743 AIB 0205 VQ-BAV 319-112

1744 AIB 0002 TS-INC 320-214

1745 AIB 0203 I-BIMI 319-112

1746 AIB 0542 N342NB 319-114

1747 AIB 0103 6Y-JMI 320-214





1748 AIB 0457 C-GJWD 321-211

1749 AIB 0151 EC-IEJ 320-232

1750 AIB 0102 N750MX 319-112

1751 AIB 0104 B-6266 320-214

1752 AIB 0543 N343NB 319-114

1753 AIB 0153 B-2339 319-111

1754 AIB 0005 G-TTOE 320-232

1755 AIB 0492 N492UA 320-232

1756 AIB 0293 CS-TTR 319-112

1757 AIB 0402 PR-MHT 320-214

1758 AIB 0601 B-MAK 319-132

1759 AIB 0908 N908FR 319-111

1760 AIB 0204 G-EUUD 320-232

R 1761 AIB 0201 VP-BIT 319-111

1762 AIB 0102 D-ALTG 320-214

1763 AIB 0104 G-OZBF 321-231

1764 AIB 0668 N668AW 320-232

1765 AIB 0294 CS-TTS 319-112

1766 AIB 0544 N344NB 319-114

1767 AIB 0004 EC-KDD 320-214

1768 AIB 0102 5B-DBP 319-132

R 1769 AIB 0302 B-6380 320-214

1770 AIB 0204 I-BIMO 319-112

1771 AIB 0116 PR-MAD 320-232

1772 AIB 0458 C-GJWI 321-211

1773 AIB 0003 A7-ADC 320-232

1774 AIB 0545 N345NB 319-114

1775 AIB 0210 PR-MHD 320-214

1776 AIB 0303 B-2282 321-231





1777 AIB 0403 G-OOPW 320-214

1778 AIB 0159 B-2227 319-112

1779 AIB 0205 I-BIMJ 319-112

1780 AIB 0404 C-GTDP 320-214

1781 AIB 0910 N910FR 319-112

1782 AIB 0205 G-EUUE 320-232

1783 AIB 0459 C-GJWN 321-211

1784 AIB 0536 N536JB 320-232

1785 AIB 0108 D-ANNI 320-232

1786 AIB 0160 B-2226 319-112

1787 AIB 0303 OO-TCJ 320-214

1788 AIB 0304 B-2283 321-231

1789 AIB 0375 N375NC 320-212

1790 AIB 0602 B-MAL 319-132

1791 AIB 0105 OH-LVE 319-112

1792 AIB 0669 N669AW 320-232

1793 AIB 0124 EC-ILR 320-214

R 1794 AIB 0110 G-OZBR 321-231

1795 AIB 0003 MM-62209 319-115

1796 AIB 0546 N346NB 319-114

1797 AIB 0001 D-ALTH 320-214

1798 AIB 0005 OY-KBE 321-232

1799 AIB 0304 CS-TNM 320-214

1800 AIB 0547 N347NB 319-114

1801 AIB 0007 PR-MAL 319-132

1802 AIB 0542 PR-MBR 320-232

1803 AIB 0912 N912FR 319-111

1804 AIB 0117 PR-MAE 320-232

1805 AIB 0295 XA-MXJ 319-112





1806 AIB 0103 D-ALTI 320-214

1807 AIB 0006 OY-KBF 321-232

1808 AIB 0106 OH-LVF 319-112

1809 AIB 0125 EC-ILS 320-214

1810 AIB 0548 N348NB 319-114

1811 AIB 0460 C-GJWO 321-211

1812 AIB 0376 N376NW 320-212

1814 AIB 0206 G-EUUF 320-232

1815 AIB 0549 N349NB 319-114

1816 AIB 0305 CS-TNN 320-214

1817 AIB 0007 LN-RKI 321-232

1818 AIB 0118 PR-MAJ 320-232

1819 AIB 0009 VP-BHF 319-114

1820 AIB 0551 N351NB 319-114

1821 AIB 0493 N493UA 320-232

1823 AIB 0107 D-ANNH 320-232

1824 AIB 0552 N352NB 319-114

1825 AIB 0119 PR-MAK 320-232

1826 AIB 0008 PR-MAM 319-132

R 1827 AIB 0546 PR-MBZ 320-232

1828 AIB 0553 N353NB 319-114

1829 AIB 0207 G-EUUG 320-232

1831 AIB 0009 PR-MAN 319-132

1832 AIB 0120 PR-MAG 320-232

1833 AIB 0554 N354NB 319-114

1834 AIB 0006 HA-LPF 320-233

1835 AIB 0544 PR-MBS 320-232

1836 AIB 0207 EC-IJN 321-211

1837 AIB 0010 PR-MAO 319-132





1838 AIB 0002 D-ALTJ 320-214

1839 AIB 0555 N355NB 319-114

1840 AIB 0494 N494UA 320-232

1841 AIB 0914 N914FR 319-111

1842 AIB 0495 N495UA 320-232

1843 AIB 0003 EC-IJU 321-231

1844 AIB 0833 N833AW 319-132

1845 AIB 0496 N496UA 320-232

1846 AIB 0201 F-GXAH 319-112

1847 AIB 0497 N497UA 320-232

1848 AIB 0008 LN-RKK 321-232

1849 AIB 0547 N547JB 320-232

1850 AIB 0254 B-MAP 321-231

R 1851 AIB 0206 VQ-BAU 319-112

R 1852 AIB 0306 B-6349 320-214

R 1853 AIB 0201 C-GKOB 319-112

1854 AIB 0011 LV-BET 320-233

1855 AIB 0013 PR-MAQ 319-132

1856 AIB 0051 TC-JLJ 320-232

1857 AIB 0127 PR-MAP 320-232

1858 AIB 0012 LV-BFY 320-233

1859 AIB 0138 F-GTAM 321-212

R 1860 AIB 0263 N263AV 320-214

1861 AIB 0552 N552JB 320-232

1862 AIB 0152 EC-IIZ 320-232

R 1863 AIB 0207 VQ-BAS 319-112

1864 AIB 0236 C-GKOD 320-214

1865 AIB 0498 N498UA 320-232

1866 AIB 0651 N866MX 319-112





1867 AIB 0264 N264AV 320-214

1868 AIB 0548 N548JB 320-232

1869 AIB 0103 G-TTIC 321-231

1870 AIB 0010 VP-BHG 319-114

1871 AIB 0209 G-EUUI 320-232

1872 AIB 0652 N872MX 319-112

1873 AIB 0603 F-GKXD 320-214

1874 AIB 0237 C-GKOE 320-214

1875 AIB 0557 N357NB 319-114

R 1876 AIB 0208 VQ-BAT 319-112

1877 AIB 0013 LV-BFO 320-233

1878 AIB 0001 F-ORME 321-231

1879 AIB 0652 F-GKXE 320-214

1880 AIB 0254 D-APAD 319-132

1881 AIB 0001 OY-VKA 321-211

1882 AIB 0653 N882MX 319-112

1883 AIB 0210 G-EUUJ 320-232

R 1884 AIB 0901 A9C-EU 319-112

1885 AIB 0604 F-GKXF 320-214

1886 AIB 0297 VP-CAN 319-112

1887 AIB 0051 OY-VKE 321-211

1888 AIB 0128 PR-MAR 320-232

1889 AIB 0102 OY-VKM 320-214

R 1890 AIB 0202 VP-BIQ 319-111

R 1891 AIB 0550 PR-MBY 320-232

1892 AIB 0007 HA-LPE 320-233

1893 AIB 0603 B-MAM 319-132

1894 AIB 0653 F-GKXG 320-214

1895 AIB 0004 A7-ADD 320-232





1896 AIB 0109 D-ANNJ 320-232

1897 AIB 0558 N358NB 319-114

1898 AIB 0554 N554JB 320-232

1899 AIB 0211 G-EUUK 320-232

1900 AIB 0605 F-GKXJ 320-214

R 1901 AIB 0902 A9C-EV 319-112

1902 AIB 0008 HA-LPD 320-233

1903 AIB 0014 LV-BGI 320-233

1904 AIB 0556 N556JB 320-232

1905 AIB 0354 6Y-JMR 321-211

1906 AIB 0211 B-2228 320-214

1907 AIB 0213 G-EUUM 320-232

1908 AIB 0001 HS-TYR 319-115

1909 AIB 0052 TC-JLK 320-232

1910 AIB 0214 G-EUUN 320-232

1911 AIB 0212 B-2229 320-214

1912 AIB 0604 B-MAN 319-132

1913 AIB 0208 OH-LXH 320-214

1914 AIB 0105 EC-ILH 320-232

1915 AIB 0558 N558JB 320-232

1916 AIB 0107 OH-LVG 319-112

1917 AIB 0559 N559JB 320-232

1918 AIB 0006 G-TTOF 320-232

1920 AIB 0307 I-EEZD 320-214

1921 AIB 0002 OY-VKB 321-211

1922 AIB 0352 G-MEDH 320-232

1923 AIB 0559 N359NB 319-114

1924 AIB 0606 F-GKXH 320-214

1925 AIB 0656 N925MX 319-112





1926 AIB 0255 B-MAQ 321-231

1927 AIB 0561 N561JB 320-232

1928 AIB 0201 A7-ADS 321-231

1929 AIB 0101 OO-TCH 320-214

1931 AIB 0003 D-ALTK 320-214

1932 AIB 0003 OY-VKC 321-211

1933 AIB 0106 EC-IMB 320-232

1934 AIB 0306 N476TA 319-132

1935 AIB 0601 N601AW 320-232

1936 AIB 0002 3B-NBH 319-112

1937 AIB 0308 I-EEZE 320-214

1938 AIB 0970 F-GRXF 319-111

1939 AIB 0801 N801FR 318-111

1940 AIB 0238 C-FZUB 320-214

1941 AIB 0105 G-OZBG 321-231

1942 AIB 0103 G-DHRG 320-214

1943 AIB 0918 N918FR 319-111

1944 AIB 0101 A6-EIA 320-232

1945 AIB 0102 A6-EIB 320-232

1946 AIB 0052 EC-INB 321-231

1947 AIB 0201 A6-EID 319-132

1948 AIB 0562 N562JB 320-232

1949 AIB 0607 F-GKXI 320-214

1950 AIB 0101 EI-LVA 321-231

1951 AIB 0150 HB-IJU 320-214

1952 AIB 0307 N477TA 319-132

1953 AIB 0002 F-ORMF 321-231

1954 AIB 0104 OY-VKS 320-214

1955 AIB 0202 A6-EIE 319-132





1956 AIB 0003 F-ORMG 321-231

1957 AIB 0005 A7-ADE 320-232

1958 AIB 0215 G-EUUO 320-232

1959 AIB 0560 N360NB 319-114

1960 AIB 0004 OY-VKD 321-211

1961 AIB 0101 G-SUEW 320-214

1962 AIB 0605 B-MAO 319-132

R 1963 AIB 0202 N529AD 319-112

1964 AIB 0213 B-2230 320-214

1965 AIB 0105 G-DHJZ 320-214

1966 AIB 0355 6Y-JMS 321-211

1967 AIB 0004 F-ORMH 321-231

1968 AIB 0102 D-AICN 320-214

1969 AIB 0007 G-TTOG 320-232

1970 AIB 0102 EI-LVB 321-231

1971 AIB 0101 B-6018 319-133

R 1972 AIB 0052 OY-VKT 321-211

1973 AIB 0026 JA201A 320-211

1974 AIB 0305 B-2284 321-231

1975 AIB 0309 OO-TCI 320-214

1976 AIB 0561 N361NB 319-114

1977 AIB 0005 F-ORMI 321-231

1978 AIB 0005 OH-LZE 321-211

1979 AIB 0107 EC-INM 320-232

1980 AIB 0919 N919FR 319-111

1981 AIB 0214 B-6001 320-214

1982 AIB 0562 N362NB 319-114

1983 AIB 0025 I-EEZF 320-214

1984 AIB 0151 B-HTH 321-231





1986 AIB 0102 B-6019 319-133

1987 AIB 0206 G-MIDO 320-232

1988 AIB 0356 6Y-JMW 321-211

1989 AIB 0209 OH-LXI 320-214

1990 AIB 0563 N363NB 319-114

1991 AIB 0802 N802FR 318-111

1993 AIB 0008 G-TTOH 320-232

1994 AIB 0351 D-ALSB 321-211

1995 AIB 0306 B-2285 321-231

1996 AIB 0053 TC-JLL 320-232

1997 AIB 0920 N920FR 319-111

1998 AIB 0108 EC-IOH 320-232

1999 AIB 0101 VH-VHD 319-115

2000 AIB 0001 B-6022 319-131

2001 AIB 0026 I-EEZG 320-214

2002 AIB 0564 N364NB 319-114

2003 AIB 0106 G-KKAZ 320-214

2004 AIB 0103 B-6020 319-133

2005 AIB 0352 D-ALSC 321-211

2006 AIB 0563 N563JB 320-232

2007 AIB 0002 B-6023 319-131

2008 AIB 0104 B-6021 319-133

2009 AIB 0004 D-ALTL 320-214

2010 AIB 0921 N921FR 319-111

2011 AIB 0103 EC-INZ 320-214

2012 AIB 0922 N922FR 319-111

2013 AIB 0565 N365NB 319-114

R 2014 AIB 0401 PR-MBT 320-233

2015 AIB 0003 B-6024 319-131





2016 AIB 0201 P4-SAS 320-232

2017 AIB 0803 N803FR 318-111

2018 AIB 0239 C-FXCD 320-214

2019 AIB 0923 N923FR 319-111

2020 AIB 0564 N564JB 320-232

2021 AIB 0152 B-HTI 321-231

2022 AIB 0215 B-6002 320-214

2023 AIB 0001 V8-RBP 319-132

2024 AIB 0151 HB-IJV 320-214

2026 AIB 0566 N366NB 319-114

2027 AIB 0109 EC-IPI 320-232

2028 AIB 0011 VP-BHI 319-114

2029 AIB 0601 N670AW 320-232

2030 AIB 0924 N924FR 319-111

2031 AIB 0565 N565JB 320-232

2032 AIB 0002 V8-RBR 319-132

2033 AIB 0206 I-BIMB 319-112

2034 AIB 0216 B-6003 320-214

2035 AIB 0801 F-GUGA 318-111

2036 AIB 0217 B-6005 320-214

2037 AIB 0001 G-EZAM 319-111

2038 AIB 0216 G-EUUP 320-232

2039 AIB 0568 N368NB 319-114

2040 AIB 0217 G-EUUR 320-232

2041 AIB 0202 HL7722 321-231

2042 AIB 0566 N566JB 320-232

2043 AIB 0002 G-EZDC 319-111

2044 AIB 0402 PR-MBL 320-233

2045 AIB 0203 HL7723 321-231





2046 AIB 0004 9K-AKD 320-212

2047 AIB 0569 N369NB 319-114

2048 AIB 0405 6Y-JMK 320-214

2049 AIB 0218 B-6008 320-214

2050 AIB 0003 G-EZNC 319-111

2051 AIB 0804 N804FR 318-111

2052 AIB 0001 VP-BWA 319-111

2053 AIB 0004 G-EZMH 319-111

2054 AIB 0027 JA202A 320-211

2055 AIB 0006 F-ORMJ 321-231

2056 AIB 0219 B-6007 320-214

2057 AIB 0207 I-BIMC 319-112

2058 AIB 0006 9V-SLF 320-232

2059 AIB 0802 F-GUGB 318-111

2060 AIB 0251 TC-JMG 321-211

2061 AIB 0028 JA203A 320-211

2062 AIB 0005 G-EZSM 319-111

2063 AIB 0568 N568JB 320-232

2064 AIB 0001 CN-RNX 321-211

2065 AIB 0210 OH-LXK 320-214

2066 AIB 0202 XA-CMA 319-112

2067 AIB 0307 B-2288 321-231

2068 AIB 0220 B-6006 320-214

2069 AIB 0002 VP-BDM 319-111

2070 AIB 0201 SU-GBZ 320-232

2071 AIB 0803 F-GUGC 318-111

2072 AIB 0003 VP-BDN 319-111

2073 AIB 0202 SU-GCA 320-232

2074 AIB 0208 I-BIMD 319-112





2075 AIB 0569 N569JB 320-232

2076 AIB 0002 CN-RNY 321-211

2077 AIB 0602 N671AW 320-232

2078 AIB 0203 XA-MXA 319-112

2079 AIB 0203 SU-GCB 320-232

2080 AIB 0308 B-2287 321-231

2081 AIB 0804 F-GUGD 318-111

2082 AIB 0377 N377NW 320-211

2083 AIB 0209 I-BIMF 319-112

R 2084 AIB 0223 HC-CGW 320-233

2085 AIB 0001 ZK-OJA 320-232

2086 AIB 0210 I-BIMG 319-112

2087 AIB 0570 N370NB 319-114

2088 AIB 0204 SU-GCC 320-232

2089 AIB 0101 CC-COU 319-132

2090 AIB 0002 ZK-OJB 320-232

2091 AIB 0004 VP-BDO 319-111

2092 AIB 0378 N378NW 320-211

2093 AIB 0051 VP-BWG 319-111

2094 AIB 0205 SU-GCD 320-232

2095 AIB 0571 N371NB 319-114

2096 AIB 0102 CC-COX 319-132

2097 AIB 0006 A7-ADF 320-232

2098 AIB 0401 G-DBCA 319-131

2099 AIB 0570 N570JB 320-232

2100 AIB 0805 F-GUGE 318-111

2101 AIB 0211 I-BIMH 319-112

2102 AIB 0224 N489TA 320-233

2103 AIB 0925 N925FR 319-111





2104 AIB 0126 EC-JFH 320-214

2105 AIB 0106 G-OZBH 321-231

2106 AIB 0101 VP-BDK 320-214

2107 AIB 0202 A7-ADT 321-231

2108 AIB 0103 LZ-MDT 320-232

2109 AIB 0806 F-GUGF 318-111

2110 AIB 0054 HL7729 321-231

2112 AIB 0003 ZK-OJC 320-232

2113 AIB 0701 9H-AEG 319-112

2114 AIB 0002 EC-JDO 320-214

2115 AIB 0208 EC-ITN 321-211

2116 AIB 0102 VP-BWD 320-214

2117 AIB 0055 TC-KTD 321-211

2118 AIB 0225 N488TA 320-233

2119 AIB 0006 G-EZEA 319-111

2120 AIB 0007 G-EZEB 319-111

2121 AIB 0007 A7-ADG 320-232

2122 AIB 0702 9H-AEH 319-112

2123 AIB 0027 EC-ISI 320-214

2124 AIB 0110 OH-LVK 319-112

2125 AIB 0571 N571JB 320-232

2126 AIB 0657 XA-NCA 319-112

2127 AIB 0212 I-BIML 319-112

2128 AIB 0202 P4-PAS 320-232

2129 AIB 0008 G-EZEC 319-111

2130 AIB 0004 ZK-OJD 320-232

2131 AIB 0451 OE-LDA 319-112

2132 AIB 0579 N579JB 320-232

2133 AIB 0103 VP-BWE 320-214





2134 AIB 0152 HB-IJW 320-214

2135 AIB 0101 V8-RBS 320-232

2136 AIB 0580 N580JB 320-232

2137 AIB 0009 G-TTOI 320-232

2138 AIB 0008 A7-ADH 320-232

2139 AIB 0102 V8-RBT 320-232

2140 AIB 0654 F-GKXK 320-214

R 2141 AIB 0581 RP-C8897 320-232

2142 AIB 0406 9H-AEF 320-214

2143 AIB 0127 EC-JFG 320-214

2144 AIB 0104 VP-BWF 320-214

2145 AIB 0240 C-FZQS 320-214

2146 AIB 0211 OH-LXL 320-214

R 2147 AIB 0582 RP-C8898 320-232

2148 AIB 0005 ZK-OJE 320-232

2149 AIB 0584 N584JB 320-232

2150 AIB 0583 N583JB 320-232

2151 AIB 0105 VP-BWH 320-214

2152 AIB 0001 F-OJSB 320-232

2153 AIB 0006 ZK-OJF 320-232

2154 AIB 0212 OH-LXM 320-214

2155 AIB 0224 B-6016 320-214

2156 AIB 0022 9V-VLA 320-232

2157 AIB 0010 G-TTOJ 320-232

2158 AIB 0051 A6-ABA 320-214

2159 AIB 0585 N585JB 320-232

2160 AIB 0586 N586JB 320-232

2161 AIB 0009 A7-ADI 320-232

2162 AIB 0006 RP-C3228 320-214





2163 AIB 0106 VP-BWI 320-214

2164 AIB 0023 9V-VLB 320-232

2165 AIB 0001 HZ-XY7 320-214

2166 AIB 0052 A6-ABB 320-214

2167 AIB 0151 A6-EIC 320-232

2168 AIB 0153 EC-IVG 320-232

2169 AIB 0101 VH-JQG 320-232

2170 AIB 0009 G-EZED 319-111

2171 AIB 0236 B-6028 320-214

2172 AIB 0004 B-6031 319-131

2173 AIB 0007 ZK-OJG 320-232

2174 AIB 0452 OE-LDB 319-112

2175 AIB 0268 N268AV 320-214

2176 AIB 0010 G-EZEF 319-111

2177 AIB 0587 N587JB 320-232

2178 AIB 0310 CS-TNP 320-214

2179 AIB 0052 VP-BWJ 319-111

2180 AIB 0101 G-OOPX 320-214

2181 AIB 0011 G-EZEG 319-111

2182 AIB 0237 B-6029 320-214

2183 AIB 0007 RP-C3227 320-214

2184 AIB 0012 HB-JZF 319-111

2185 AIB 0102 VH-JQL 320-232

2186 AIB 0703 9H-AEJ 319-112

2187 AIB 0269 N269AV 320-214

2188 AIB 0402 G-DBCB 319-131

2189 AIB 0409 9H-AEI 320-214

2190 AIB 0053 G-MEDJ 321-231

2191 AIB 0205 EI-DEA 320-214





2192 AIB 0001 P4-ARL 319-133

2193 AIB 0672 N672AW 320-232

2194 AIB 0403 G-DBCC 319-131

2195 AIB 0105 9V-TAB 320-232

2196 AIB 0013 HB-JZG 319-111

2197 AIB 0103 VH-JQX 320-232

2198 AIB 0926 N926FR 319-111

2199 AIB 0238 B-6030 320-214

2200 AIB 0105 B-6039 319-132

2201 AIB 0588 N588JB 320-232

2202 AIB 0005 B-6032 319-131

2203 AIB 0106 B-6040 319-132

2204 AIB 0502 9V-TAA 320-232

2205 AIB 0006 B-6033 319-131

2206 AIB 0206 EI-DEB 320-214

2207 AIB 0003 EC-IZD 320-214

2208 AIB 0006 OH-LZF 321-211

2209 AIB 0927 N927FR 319-111

2210 AIB 0110 EC-IYG 320-232

2211 AIB 0256 SE-RDN 321-231

2212 AIB 0221 B-6015 320-214

2213 AIB 0751 F-GRXG 319-115

2214 AIB 0014 G-EZEJ 319-111

2215 AIB 0589 N589JB 320-232

2216 AIB 0257 SE-RDO 321-231

2217 AIB 0207 EI-DEC 320-214

2218 AIB 0806 N806FR 318-111

2219 AIB 0222 B-6009 320-214

2220 AIB 0209 EC-IXD 321-211





2221 AIB 0223 B-6010 320-214

2222 AIB 0053 VP-BWK 319-111

2223 AIB 0111 EC-IZK 320-232

2224 AIB 0015 G-EZEK 319-111

2225 AIB 0128 EC-IZH 320-214

2226 AIB 0252 HL7730 321-231

2227 AIB 0004 EC-JAB 320-214

2228 AIB 0752 F-GRXH 319-115

2229 AIB 0003 B-HSL 320-232

2230 AIB 0016 HB-JZH 319-111

2231 AIB 0590 N590JB 320-232

2232 AIB 0107 B-6041 319-132

2233 AIB 0151 VP-BWM 320-214

2234 AIB 0107 G-OZBI 321-231

2235 AIB 0225 B-6011 320-214

2236 AIB 0928 N928FR 319-111

2237 AIB 0101 B-6034 319-115

2238 AIB 0004 B-HSM 320-232

2239 AIB 0226 B-6012 320-214

2240 AIB 0929 N929FR 319-111

2241 AIB 0930 N930FR 319-111

2242 AIB 0129 EC-IZR 320-214

2243 AIB 0054 VP-BWL 319-111

2244 AIB 0227 B-6013 320-214

2245 AIB 0017 HB-JZI 319-111

2246 AIB 0591 N591JB 320-232

2247 AIB 0204 HL7731 321-231

2248 AIB 0130 EC-KOH 320-214

2249 AIB 0018 G-EZEO 319-111





2250 AIB 0208 EI-DEE 320-214

2251 AIB 0019 G-EZEP 319-111

2252 AIB 0007 9V-SLG 320-233

2253 AIB 0931 N931FR 319-111

2254 AIB 0001 HS-PGU 320-232

2255 AIB 0001 VN-A344 321-231

2256 AIB 0209 EI-DEF 320-214

2257 AIB 0008 ZK-OJH 320-232

2258 AIB 0932 N932FR 319-111

2259 AIB 0592 N592JB 320-232

2260 AIB 0933 N933FR 319-111

2261 AIB 0002 VN-A345 321-231

2262 AIB 0453 OE-LDC 319-112

2263 AIB 0001 FAB2101 319-133

2264 AIB 0301 EC-JAZ 319-111

2265 AIB 0020 HB-JZJ 319-111

2266 AIB 0111 OH-LVL 319-112

2267 AIB 0003 VN-A347 321-231

2268 AIB 0001 ZS-SFD 319-131

2269 AIB 0102 B-6035 319-115

2270 AIB 0210 EC-JNI 321-211

2271 AIB 0021 G-EZET 319-111

2272 AIB 0210 EI-DEG 320-214

2273 AIB 0108 B-6042 319-132

2274 AIB 0228 B-6017 320-214

2275 AIB 0201 B-2403 320-232

2276 AIB 0807 N807FR 318-111

2277 AIB 0803 N803BR 319-132

2278 AIB 0053 A6-ABC 320-214





2279 AIB 0753 F-GRXI 319-115

2280 AIB 0593 N593JB 320-232

2281 AIB 0002 ZS-SFE 319-131

2282 AIB 0226 N490TA 320-233

2283 AIB 0022 G-EZEU 319-111

2284 AIB 0594 N594JB 320-232

2285 AIB 0103 B-6036 319-115

2286 AIB 0595 N595JB 320-232

2287 AIB 0934 N934FR 319-111

2288 AIB 0010 A7-ADJ 320-232

2289 AIB 0023 G-EZEV 319-111

2290 AIB 0205 HL7735 321-231

2291 AIB 0414 9H-AEK 320-214

2292 AIB 0001 VH-VQZ 320-232

2293 AIB 0104 B-6037 319-115

2294 AIB 0211 EI-DEH 320-214

2295 AIB 0103 CC-COY 319-132

2296 AIB 0804 F-GXAG 319-132

2297 AIB 0009 ZK-OJI 320-232

2298 AIB 0105 B-6038 319-115

2299 AIB 0002 VH-VQY 320-232

2300 AIB 0024 G-EZEW 319-111

2301 AIB 0227 N491TA 320-233

2302 AIB 0834 N834AW 319-132

2303 AIB 0004 VN-A348 321-231

2304 AIB 0104 CC-COZ 319-132

2305 AIB 0101 G-EUXC 321-231

2306 AIB 0001 A5-RGF 319-115

2307 AIB 0597 N597JB 320-232





2308 AIB 0003 ZS-SFF 319-131

2309 AIB 0301 B-2289 321-211

2310 AIB 0002 HS-PGV 320-232

2311 AIB 0302 EC-JEI 319-111

2312 AIB 0673 N673AW 320-232

2313 AIB 0301 B-6043 319-133

2314 AIB 0598 N598JB 320-232

2315 AIB 0302 B-2290 321-211

2316 AIB 0001 9V-JSA 320-232

2317 AIB 0807 F-GUGG 318-111

2318 AIB 0935 N935FR 319-111

2319 AIB 0025 HB-JZK 319-111

2320 AIB 0102 G-EUXD 321-231

2321 AIB 0105 CC-CPE 319-132

2322 AIB 0003 VH-VQX 320-232

2323 AIB 0103 G-EUXE 321-231

2324 AIB 0104 G-EUXF 321-231

2325 AIB 0270 N270AV 320-214

2326 AIB 0004 ZS-SFG 319-131

2327 AIB 0271 N271AV 320-214

2328 AIB 0801 XA-UBQ 318-111

2329 AIB 0004 VH-VQW 320-232

2330 AIB 0201 VP-BWN 321-211

2331 AIB 0002 9V-TAC 320-232

2332 AIB 0704 9H-AEL 319-112

2333 AIB 0802 XA-UBR 318-111

2334 AIB 0202 B-2407 320-232

2335 AIB 0101 D-ABGD 319-132

2336 AIB 0599 N599JB 320-232





2337 AIB 0202 VP-BWO 321-211

2338 AIB 0005 VH-VQV 320-232

2339 AIB 0308 N478TA 319-132

2340 AIB 0003 9V-TAD 320-232

2341 AIB 0102 A7-CJB 319-133

2342 AIB 0203 VP-BWP 321-211

2343 AIB 0203 B-2405 320-232

2344 AIB 0808 F-GUGH 318-111

2345 AIB 0204 B-2374 320-232

2346 AIB 0002 A5-RGG 319-115

2347 AIB 0131 EC-KHJ 320-214

2348 AIB 0302 B-6045 319-133

2349 AIB 0054 A6-ABD 320-214

2350 AIB 0809 F-GUGI 318-111

2351 AIB 0105 G-EUXG 321-231

2352 AIB 0603 N603JB 320-232

2353 AIB 0026 HB-JZL 319-111

2354 AIB 0051 B-2406 320-214

2355 AIB 0005 ZS-SFH 319-131

2356 AIB 0002 9V-JSB 320-232

2357 AIB 0211 EC-JDM 321-211

2358 AIB 0803 XA-UBS 318-111

2359 AIB 0674 N674AW 320-232

2360 AIB 0027 G-EZEZ 319-111

2361 AIB 0052 B-2408 320-214

2362 AIB 0806 N806BR 319-132

2363 AIB 0106 G-EUXH 321-231

2364 AIB 0212 EI-DEJ 320-214

2365 AIB 0303 EC-JDL 319-111





2366 AIB 0651 VT-ADV 320-232

2367 AIB 0804 XA-UBT 318-111

2368 AIB 0605 N605JB 320-232

2369 AIB 0012 VP-BHJ 319-114

2370 AIB 0028 HB-JZM 319-111

2371 AIB 0109 B-2294 319-132

2372 AIB 0121 PR-MAS 320-232

2373 AIB 0013 VP-BHK 319-114

2374 AIB 0213 EI-DEI 320-214

2375 AIB 0006 ZS-SFI 319-131

2376 AIB 0652 VT-ADW 320-232

2377 AIB 0805 XA-UBU 318-111

2378 AIB 0029 G-EZMS 319-111

2379 AIB 0007 ZS-SFJ 319-131

2380 AIB 0030 G-EJJB 319-111

2381 AIB 0212 EC-JEJ 321-211

2382 AIB 0705 9H-AEM 319-112

2383 AIB 0104 D-ABGA 319-132

2384 AIB 0606 N606JB 320-232

2385 AIB 0031 G-EZPG 319-111

2386 AIB 0607 N607JB 320-232

2387 AIB 0032 HB-JZN 319-111

2388 AIB 0005 EC-JFF 320-214

2389 AIB 0404 G-DBCD 319-131

2390 AIB 0416 CS-TKK 320-214

2391 AIB 0132 EC-JFN 320-214

2392 AIB 0936 N936FR 319-111

2393 AIB 0122 PR-MAV 320-232

2394 AIB 0806 XA-UBV 318-111





2395 AIB 0003 9V-JSC 320-232

2396 AIB 0609 EC-JQT 319-132

2397 AIB 0301 HL7737 320-232

2398 AIB 0033 HB-JZO 319-111

2399 AIB 0214 EI-DEK 320-214

2400 AIB 0937 N937FR 319-111

2401 AIB 0004 9V-JSD 320-232

2402 AIB 0034 G-EZNM 319-111

2403 AIB 0001 VP-CMS 320-232

2404 AIB 0610 TC-IZM 319-132

2405 AIB 0675 N675AW 320-232

2406 AIB 0938 N938FR 319-111

2407 AIB 0006 EC-JGM 320-214

2408 AIB 0110 B-2295 319-132

2409 AIB 0215 EI-DEL 320-214

2410 AIB 0258 SE-RDP 321-231

2411 AIB 0216 EI-DEM 320-214

2412 AIB 0035 G-EJAR 319-111

2413 AIB 0101 VT-KFA 320-232

2414 AIB 0611 TC-IZR 319-132

2415 AIB 0608 N608JB 320-232

2416 AIB 0454 OE-LDD 319-112

2417 AIB 0123 PR-MAW 320-232

2418 AIB 0008 ZS-SFK 319-131

2419 AIB 0004 RP-C3240 320-214

2420 AIB 0036 G-EZIA 319-111

2421 AIB 0001 VP-CCJ 319-133

2422 AIB 0676 N676AW 320-232

2423 AIB 0151 VH-JQW 320-232





2424 AIB 0101 N501NK 319-132

2425 AIB 0417 CS-TKL 320-214

2426 AIB 0111 B-2296 319-132

2427 AIB 0037 HB-JZP 319-111

2428 AIB 0005 B-HSN 320-232

2429 AIB 0405 G-DBCE 319-131

2430 AIB 0677 N677AW 320-232

2431 AIB 0612 EC-JQU 319-132

2432 AIB 0217 EI-DEN 320-214

2433 AIB 0102 N502NK 319-132

2434 AIB 0228 N492TA 320-233

2435 AIB 0112 B-2297 319-132

2436 AIB 0038 G-EZIC 319-111

2437 AIB 0229 B-2410 320-214

2438 AIB 0009 ZS-SFL 319-131

2439 AIB 0005 RP-C3241 320-214

2440 AIB 0001 F-ONAS 319-115

2441 AIB 0353 G-MEDK 320-232

2442 AIB 0039 G-EZID 319-111

2443 AIB 0102 VT-KFB 320-232

2444 AIB 0309 N479TA 319-132

2445 AIB 0139 PR-MBJ 320-232

2446 AIB 0040 G-EZIE 319-111

2447 AIB 0612 N612JB 320-232

2448 AIB 0939 N939FR 319-111

2449 AIB 0613 N613JB 320-232

2450 AIB 0041 HB-JZQ 319-111

2451 AIB 0230 B-2411 320-214

2452 AIB 0613 TC-IZH 319-132





2453 AIB 0152 VH-JQH 320-232

2454 AIB 0007 B-2404 319-131

2455 AIB 0006 VH-VQU 320-232

2456 AIB 0754 F-GRXJ 319-115

2457 AIB 0153 VH-JQE 320-232

2458 AIB 0835 N835AW 319-132

2459 AIB 0302 HL7738 320-232

2460 AIB 0042 G-EZIG 319-111

2461 AIB 0615 N615JB 320-232

2462 AIB 0104 G-TTID 321-231

2463 AIB 0043 G-EZIH 319-111

2464 AIB 0014 VP-BHL 319-114

2465 AIB 0940 N940FR 319-111

2466 AIB 0406 G-DBCF 319-131

2467 AIB 0103 D-ABGB 319-132

2468 AIB 0102 D-ABGC 319-132

2469 AIB 0010 ZS-SFM 319-131

2470 AIB 0103 N503NK 319-132

2471 AIB 0044 G-EZII 319-111

2472 AIB 0213 EC-JGS 321-211

2473 AIB 0104 N504NK 319-132

2474 AIB 0015 VP-BHV 319-114

2475 AIB 0007 VH-VQT 320-232

2476 AIB 0005 N587NK 321-231

2477 AIB 0045 G-EZIJ 319-111

2478 AIB 0231 B-2412 320-214

2479 AIB 0154 EC-JJD 320-232

2480 AIB 0005 VN-A349 321-231

2481 AIB 0046 G-EZIK 319-111





2482 AIB 0678 N678AW 320-232

2483 AIB 0941 N941FR 319-112

2484 AIB 0053 B-6251 320-214

2485 AIB 0105 N505NK 319-132

2486 AIB 0218 EI-DEO 320-214

2487 AIB 0101 4K-AZ01 319-115

2488 AIB 0214 EC-JDR 321-211

2489 AIB 0618 N618JB 320-232

2490 AIB 0106 N506NK 319-132

2491 AIB 0621 N621JB 320-232

2492 AIB 0047 G-EZIL 319-111

2493 AIB 0232 B-2413 320-214

2494 AIB 0455 OE-LDE 319-112

2495 AIB 0048 G-EZIM 319-111

2496 AIB 0103 VT-KFC 320-232

2497 AIB 0942 N942FR 319-111

2498 AIB 0233 B-2415 320-214

2499 AIB 0106 B-2364 319-115

2501 AIB 0011 ZS-SFN 319-131

2502 AIB 0104 VT-KFD 320-232

2503 AIB 0049 G-EZIN 319-111

2504 AIB 0623 N623JB 320-232

2505 AIB 0113 B-6205 319-132

2506 AIB 0054 B-6252 320-214

2507 AIB 0004 MM-62243 319-115

2508 AIB 0107 B-6004 319-115

2509 AIB 0003 HS-PGW 320-232

2510 AIB 0303 B-6054 319-133

2511 AIB 0055 B-6253 320-214





2512 AIB 0050 G-EZIO 319-111

2513 AIB 0124 PR-MAZ 320-232

2514 AIB 0051 G-EZIP 319-111

2515 AIB 0008 VH-VQS 320-232

2516 AIB 0001 4K-AZ03 319-111

2517 AIB 0008 9V-SLH 320-233

2518 AIB 0943 N943FR 319-112

2519 AIB 0251 B-6200 319-115

2520 AIB 0624 N624JB 320-232

2521 AIB 0309 B-2417 321-231

2522 AIB 0001 VT-KFE 320-232

2523 AIB 0807 XA-UBW 318-111

2524 AIB 0501 VT-DKZ 320-232

2525 AIB 0108 B-6014 319-115

2526 AIB 0009 VH-VQR 320-232

2527 AIB 0052 G-EZIR 319-111

2528 AIB 0053 G-EZIS 319-111

2529 AIB 0001 OE-LEA 320-214

2530 AIB 0310 B-2418 321-231

2531 AIB 0002 VT-KFF 320-232

2532 AIB 0109 B-6044 319-115

2533 AIB 0011 ZK-OJM 320-232

2534 AIB 0304 B-2298 319-133

2535 AIB 0625 N625JB 320-232

2536 AIB 0108 G-EUXI 321-231

2537 AIB 0010 VH-VQQ 320-232

2538 AIB 0054 G-EZIT 319-111

R 2539 AIB 0401 D-ABDA 320-214

2540 AIB 0007 EC-JMB 320-214





2541 AIB 0252 B-6201 319-115

2542 AIB 0219 EI-DEP 320-214

2543 AIB 0303 B-2291 321-211

2544 AIB 0808 XA-UBX 318-111

2545 AIB 0110 B-6046 319-115

2546 AIB 0253 B-6202 319-115

2547 AIB 0456 OE-LDF 319-112

2548 AIB 0055 G-EZIU 319-111

2549 AIB 0304 B-2292 321-211

2550 AIB 0101 G-NMAK 319-115

2551 AIB 0111 B-6047 319-115

2552 AIB 0809 XA-UBY 318-111

2553 AIB 0401 N566TA 321-231

2554 AIB 0151 B-6203 319-112

2555 AIB 0152 B-6208 319-112

2556 AIB 0001 RP-C3189 319-111

2557 AIB 0001 B-6210 319-115

2558 AIB 0153 B-6209 319-112

2559 AIB 0008 B-6048 319-131

2560 AIB 0107 N507NK 319-132

2561 AIB 0002 B-6211 319-115

2562 AIB 0106 B-6259 320-214

2563 AIB 0215 EC-JLI 321-211

2564 AIB 0502 VT-DKY 320-232

2565 AIB 0056 G-EZIV 319-111

2566 AIB 0001 A4O-AA 320-232

2567 AIB 0108 N508NK 319-132

2568 AIB 0105 9V-SBE 319-132

2569 AIB 0001 9K-CAA 320-214





2570 AIB 0836 N836AW 319-132

2571 AIB 0004 LZ-WZA 320-232

2572 AIB 0106 CC-CPF 319-132

2573 AIB 0011 VH-VQP 320-232

2574 AIB 0114 B-6206 319-132

2575 AIB 0810 XA-UBZ 318-111

2576 AIB 0003 VT-KFG 320-232

2577 AIB 0627 N627JB 320-232

2578 AIB 0057 G-EZIW 319-111

2579 AIB 0115 B-6207 319-132

2580 AIB 0629 N629JB 320-232

2581 AIB 0003 B-6212 319-115

2582 AIB 0810 F-GUGJ 318-111

2583 AIB 0220 EI-DER 320-214

2584 AIB 0002 9K-CAB 320-214

2585 AIB 0107 CC-CPI 319-132

2586 AIB 0002 RP-C3190 319-111

2587 AIB 0012 VH-VQO 320-232

2588 AIB 0002 4K-AZ04 319-111

2589 AIB 0155 EC-JNC 320-232

2590 AIB 0006 N588NK 321-231

2591 AIB 0107 B-6260 320-214

R 2592 AIB 0001 9H-AFK 319-115

2593 AIB 0204 VT-SCA 319-112

2594 AIB 0012 ZK-OJN 320-232

2595 AIB 0837 N837AW 319-132

2596 AIB 0008 EC-JNA 320-214

2597 AIB 0305 B-2299 319-133

2598 AIB 0101 JY-AYD 320-232





2599 AIB 0216 EC-JMR 321-211

2600 AIB 0013 VH-VQN 320-232

2601 AIB 0811 F-GUGK 318-111

2602 AIB 0129 PR-MAX 320-232

2603 AIB 0109 N509NK 319-132

2604 AIB 0008 9V-JSH 320-232

2605 AIB 0058 G-EZIX 319-111

2606 AIB 0108 B-6261 320-214

2607 AIB 0010 D-AKNT 319-112

2608 AIB 0014 VH-VQM 320-232

2609 AIB 0054 TC-JPA 320-232

2610 AIB 0402 N567TA 321-231

2611 AIB 0051 B-6215 319-112

2612 AIB 0001 9M-AFA 320-216

2613 AIB 0679 N679AW 320-232

2614 AIB 0009 B-6213 319-131

2615 AIB 0838 N838AW 319-132

2616 AIB 0621 N621VA 320-214

2617 AIB 0052 B-6198 319-112

2618 AIB 0016 VP-BHP 319-114

R 2619 AIB 0402 D-ABDB 320-214

2620 AIB 0001 JA01MC 320-214

2621 AIB 0201 VT-KFH 319-131

2622 AIB 0110 N510NK 319-132

2623 AIB 0009 EC-JNT 320-214

2624 AIB 0205 VT-SCB 319-112

2625 AIB 0003 RP-C3191 319-111

2626 AIB 0055 TC-JPB 320-232

2627 AIB 0109 B-6262 320-214





2628 AIB 0011 D-AKNU 319-112

2629 AIB 0206 VT-SCC 319-112

2630 AIB 0680 N680AW 320-232

2631 AIB 0001 TC-OGU 319-132

2632 AIB 0012 D-AKNV 319-112

2633 AIB 0002 9M-AFB 320-214

2634 AIB 0202 VT-KFI 319-131

2635 AIB 0221 EI-DES 320-214

2636 AIB 0059 G-EZIY 319-111

2637 AIB 0056 B-6255 320-214

2638 AIB 0004 RP-C3192 319-111

2639 AIB 0306 B-2300 319-133

2640 AIB 0630 N630JB 320-232

2641 AIB 0017 VP-BHQ 319-114

2642 AIB 0015 VH-VQL 320-232

2643 AIB 0010 B-6216 319-131

2644 AIB 0053 B-6199 319-112

2645 AIB 0701 VT-DKV 320-232

2646 AIB 0060 G-EZIZ 319-111

2647 AIB 0632 N632JB 320-232

2648 AIB 0001 PK-YVA 319-132

2649 AIB 0102 F-OHGV 320-232

2650 AIB 0301 VT-VJM 319-133

2651 AIB 0016 VH-VQK 320-232

2652 AIB 0457 OE-LDG 319-112

2653 AIB 0054 G-MEDL 321-231

R 2654 AIB 0403 D-ABDC 320-214

2655 AIB 0002 TC-OGV 319-132

2656 AIB 0003 9M-AFC 320-214





2657 AIB 0310 XA-VOI 319-132

2658 AIB 0002 JA02MC 320-214

2659 AIB 0111 N511NK 319-132

2660 AIB 0002 PK-YVC 319-132

2661 AIB 0130 PR-MAY 320-232

2662 AIB 0207 XA-UER 319-112

2663 AIB 0013 ZK-OJO 320-232

2664 AIB 0203 VT-KFJ 319-131

2665 AIB 0419 9H-AEN 320-214

2666 AIB 0311 XA-VOL 319-132

2667 AIB 0116 B-6219 319-132

2668 AIB 0002 OE-LEO 320-214

2669 AIB 0839 N839AW 319-132

2670 AIB 0004 VT-KFK 320-232

2671 AIB 0633 N633JB 320-232

2672 AIB 0001 B-6196 319-115

2673 AIB 0112 N512NK 319-132

2674 AIB 0622 N622VA 320-214

2675 AIB 0001 D-AIJO 319-115

2676 AIB 0702 VT-DKU 320-232

2677 AIB 0061 G-EZAA 319-111

2678 AIB 0010 A6-ABZ 320-214

2679 AIB 0114 N514NK 319-132

2680 AIB 0205 B-6275 320-232

2681 AIB 0062 G-EZAB 319-111

2682 AIB 0105 G-TTIE 321-231

2683 AIB 0004 9M-AFD 320-214

2684 AIB 0002 B-6197 319-115

2685 AIB 0004 D-ABDD 320-214





2686 AIB 0812 F-GUGL 318-111

2687 AIB 0403 N568TA 321-231

2688 AIB 0007 HA-LPH 320-232

2689 AIB 0206 B-6276 320-232

2690 AIB 0840 N840AW 319-132

2691 AIB 0063 G-EZAC 319-111

2692 AIB 0103 JY-AYF 320-232

2693 AIB 0401 B-6217 319-115

2694 AIB 0407 G-DBCG 319-131

2695 AIB 0003 JA03MC 320-214

2696 AIB 0005 D-ABDE 320-214

2697 AIB 0408 G-DBCH 319-131

R 2698 AIB 0115 EI-ECX 319-132

2699 AIB 0005 9M-AFE 320-214

R 2700 AIB 0944 A9C-BAX 319-111

2701 AIB 0207 B-6277 320-232

2702 AIB 0064 G-EZAD 319-111

2703 AIB 0017 VH-VQJ 320-232

2704 AIB 0116 N516NK 319-132

2705 AIB 0608 F-GKXL 320-214

2706 AIB 0002 319-115

2707 AIB 0357 F-GYAJ 321-211

2708 AIB 0057 B-6263 320-214

2709 AIB 0065 G-EZAE 319-111

2710 AIB 0634 N634JB 320-232

2711 AIB 0117 N517NK 319-132

2712 AIB 0001 A6-ABE 320-214

2713 AIB 0311 B-6265 321-231

2714 AIB 0208 B-6278 320-232





2715 AIB 0066 G-EZAF 319-111

2716 AIB 0755 F-GRXK 319-115

2717 AIB 0018 VH-VQI 320-232

R 2718 AIB 0118 5B-DCF 319-132

2719 AIB 0051 OK-LEE 320-214

2720 AIB 0409 G-DBCI 319-131

2721 AIB 0609 F-GKXM 320-214

2723 AIB 0119 N519NK 319-132

2724 AIB 0001 9V-TAE 320-232

2725 AIB 0635 N635JB 320-232

2726 AIB 0003 CN-ROF 321-211

2727 AIB 0067 G-EZAG 319-111

2728 AIB 0002 9V-TAF 320-232

2729 AIB 0068 G-EZAH 319-111

2730 AIB 0201 JY-AYG 321-231

2731 AIB 0505 VT-DKR 320-232

2732 AIB 0001 LZ-MDA 320-232

2733 AIB 0054 B-6222 319-112

2734 AIB 0131 PR-MBA 320-232

2735 AIB 0069 G-EZAI 319-111

2736 AIB 0251 EC-JQZ 321-212

2737 AIB 0132 PR-MBB 320-232

2738 AIB 0101 TC-JLM 319-132

2739 AIB 0102 TC-JLN 319-132

2740 AIB 0623 PR-MHH 320-214

2741 AIB 0312 B-6267 321-231

2742 AIB 0070 G-EZAJ 319-111

2743 AIB 0058 B-6269 320-214

2744 AIB 0071 G-EZAK 319-111





2745 AIB 0006 EC-JQP 320-214

2746 AIB 0055 B-6221 319-112

2747 AIB 0506 VT-DKS 320-232

2748 AIB 0001 N-3618F 319-115

2749 AIB 0003 OE-LEE 320-214

2750 AIB 0813 F-GUGM 318-111

2751 AIB 0945 N945FR 319-111

2752 AIB 0113 HA-LPI 320-232

2753 AIB 0507 VT-DKT 320-232

2754 AIB 0072 G-EZAL 319-111

2755 AIB 0636 N636JB 320-232

2756 AIB 0252 EC-JRE 321-212

2757 AIB 0402 B-6218 319-115

2758 AIB 0052 OK-LEF 320-214

2759 AIB 0313 B-6270 321-231

2760 AIB 0006 9M-AFF 320-214

2761 AIB 0011 OE-LEV 320-214

2762 AIB 0001 B-6229 319-112

2763 AIB 0946 N946FR 319-111

2764 AIB 0002 A6-ABF 320-214

2765 AIB 0073 G-EZAN 319-111

2766 AIB 0019 VH-VQH 320-232

2767 AIB 0314 B-6271 321-231

2768 AIB 0420 9H-AEO 320-214

2769 AIB 0074 G-EZAO 319-111

2770 AIB 0059 B-6272 320-214

2771 AIB 0001 XA-VOA 319-133

2772 AIB 0209 B-6279 320-232

R 2773 AIB 0521 N521VA 319-112





2774 AIB 0002 B-6230 319-112

2775 AIB 0009 9V-SLI 320-233

2776 AIB 0133 EC-JSB 320-214

2777 AIB 0075 G-EZAP 319-111

2778 AIB 0624 N624VA 320-214

2779 AIB 0076 G-EZAS 319-111

2780 AIB 0002 XA-VOB 319-133

2781 AIB 0637 N637JB 320-232

2782 AIB 0077 G-EZAT 319-111

2783 AIB 0133 PR-MBC 320-232

R 2784 AIB 0120 PK-RMI 319-132

2785 AIB 0012 EC-JSY 320-214

2786 AIB 0005 RP-C3193 319-111

2787 AIB 0020 VH-VQG 320-232

2788 AIB 0003 4K-AZ05 319-111

2789 AIB 0053 OK-LEG 320-214

2790 AIB 0006 RP-C3194 319-111

2791 AIB 0229 EI-TAG 320-233

2792 AIB 0003 9K-CAC 320-214

2793 AIB 0202 JY-AYH 321-231

2794 AIB 0013 EC-JTQ 320-214

2795 AIB 0078 G-EZAU 319-111

2796 AIB 0060 B-6281 320-214

R 2797 AIB 0121 PK-RMH 319-132

2798 AIB 0014 EC-JTR 320-214

2799 AIB 0055 G-MEDM 321-231

2800 AIB 0625 N625VA 320-214

2801 AIB 0001 319-115

2802 AIB 0638 N638JB 320-232





2803 AIB 0079 G-EZAV 319-111

2804 AIB 0503 LZ-MDM 320-232

2805 AIB 0112 B-6223 319-115

2806 AIB 0947 N947FR 319-111

2807 AIB 0134 EC-JSK 320-214

2808 AIB 0303 HL7744 320-232

2809 AIB 0315 B-6273 321-231

2810 AIB 0222 EI-DET 320-214

R 2811 AIB 0522 N522VA 319-112

2812 AIB 0080 G-EZAW 319-111

2813 AIB 0101 D-AGWA 319-132

2814 AIB 0639 N639JB 320-232

2815 AIB 0117 B-6220 319-132

2816 AIB 0101 9M-AFG 320-216

2817 AIB 0005 VT-KFL 320-232

2818 AIB 0081 G-EZAX 319-111

2819 AIB 0113 B-6225 319-115

2820 AIB 0006 D-ABDF 320-214

2821 AIB 0007 RP-C3196 319-111

2822 AIB 0004 9K-CAD 320-214

2823 AIB 0303 TC-JRA 321-231

2824 AIB 0061 B-6282 320-214

2825 AIB 0403 B-6231 319-115

2826 AIB 0102 9M-AFH 320-216

2827 AIB 0082 G-EZAY 319-111

2828 AIB 0001 P4-TAS 320-232

2829 AIB 0083 G-EZAZ 319-111

2830 AIB 0626 N626VA 320-214

2831 AIB 0008 RP-C3195 319-111





2832 AIB 0640 N640JB 320-232

2833 AIB 0102 D-AGWB 319-132

2834 AIB 0062 B-6283 320-214

2835 AIB 0007 D-ABDG 320-214

R 2836 AIB 0948 N948FR 319-112

2837 AIB 0001 319-115

2838 AIB 0134 PR-MBD 320-232

2839 AIB 0114 B-6226 319-115

2840 AIB 0304 HL7745 320-232

2841 AIB 0003 B-6153 319-115

2842 AIB 0103 9M-AFI 320-216

2843 AIB 0304 EC-JVE 319-111

2844 AIB 0001 VT-INA 320-232

2845 AIB 0108 CC-CPJ 319-132

2846 AIB 0008 D-ABDH 320-214

2847 AIB 0115 B-6227 319-115

2848 AIB 0641 N641JB 320-232

2849 AIB 0056 B-6156 319-112

2850 AIB 0101 OY-KBO 319-132

2851 AIB 0627 N627VA 320-214

2852 AIB 0009 RP-C3197 319-111

2853 AIB 0009 D-ABDI 320-214

2854 AIB 0084 G-EZBB 319-111

2855 AIB 0063 B-6288 320-214

2856 AIB 0151 VT-KFM 320-232

R 2857 AIB 0949 N949FR 319-112

2858 AIB 0109 CC-CPL 319-132

2859 AIB 0135 PR-MBE 320-232

2860 AIB 0085 G-EZBA 319-111





2861 AIB 0064 B-6289 320-214

2862 AIB 0404 N564TA 321-231

2863 AIB 0002 VT-INB 320-232

2864 AIB 0110 CC-CPM 319-132

2865 AIB 0010 D-ABDJ 320-214

2866 AIB 0086 G-EZBC 319-111

2867 AIB 0004 OE-LEX 320-214

2868 AIB 0304 TC-JRB 321-231

2869 AIB 0001 EI-DSA 320-216

2870 AIB 0305 EC-JXA 319-111

2871 AIB 0643 N643JB 320-232

2872 AIB 0111 CC-CPO 319-132

2873 AIB 0087 G-EZBD 319-111

2874 AIB 0703 VT-ADU 320-232

2875 AIB 0107 VP-BQP 320-214

2876 AIB 0010 RP-C3198 319-111

2877 AIB 0065 B-6290 320-214

2878 AIB 0101 RP-C8600 319-112

2879 AIB 0001 B-6232 319-112

2880 AIB 0644 N644JB 320-232

2881 AIB 0104 9M-AFJ 320-216

2882 AIB 0305 B-2419 321-211

2883 AIB 0003 VT-INC 320-232

2884 AIB 0088 G-EZBE 319-111

2885 AIB 0105 9M-AFK 320-216

2886 AIB 0112 CC-CPQ 319-132

2887 AIB 0113 CC-CPX 319-132

2888 AIB 0102 OY-KBP 319-132

2889 AIB 0306 EC-JXJ 319-111





2890 AIB 0116 B-6228 319-115

2891 AIB 0057 B-6157 319-112

2892 AIB 0114 CC-CQK 319-132

2893 AIB 0122 N522NK 319-132

2894 AIB 0115 CC-CQL 319-132

2895 AIB 0306 B-2420 321-211

2896 AIB 0136 PR-MBF 320-232

2897 AIB 0307 EC-JXV 319-111

2898 AIB 0123 N523NK 319-132

2899 AIB 0066 B-6287 320-214

2900 AIB 0645 N645JB 320-232

2901 AIB 0118 B-6158 319-132

2902 AIB 0005 OE-LEU 320-214

2903 AIB 0204 VP-BQR 321-211

2904 AIB 0137 PR-MBH 320-232

2905 AIB 0007 B-6159 319-112

2906 AIB 0003 VH-VNB 320-232

2907 AIB 0901 VT-SCF 319-112

2908 AIB 0503 VT-ADT 320-232

2909 AIB 0004 B-6286 320-214

R 2910 AIB 0101 9H-AFM 318-112

2911 AIB 0004 VT-IND 320-232

2912 AIB 0205 VP-BQS 321-211

2913 AIB 0002 B-6233 319-112

2914 AIB 0504 VT-ADS 320-232

2915 AIB 0067 B-6291 320-214

2916 AIB 0401 VT-KFN 321-232

2917 AIB 0230 N493TA 320-233

2918 AIB 0814 F-GUGN 318-111





2919 AIB 0402 VT-KFP 321-232

2920 AIB 0108 VP-BQV 320-214

2921 AIB 0001 P4-VNL 319-115

2922 AIB 0508 VT-ADR 320-232

2923 AIB 0089 G-EZBF 319-111

2924 AIB 0201 PR-MHA 320-214

2925 AIB 0102 RP-C8601 319-112

2926 AIB 0106 9M-AFL 320-216

2927 AIB 0403 VT-KFQ 321-232

2928 AIB 0056 TC-JPC 320-232

2929 AIB 0124 N524NK 319-132

2930 AIB 0003 A6-ABG 320-214

2931 AIB 0001 YR-ASA 318-111

2932 AIB 0002 EI-DSB 320-216

2933 AIB 0404 VT-KFR 321-232

2934 AIB 0057 TC-JPD 320-232

2935 AIB 0008 B-6165 319-112

2936 AIB 0316 B-6302 321-231

2937 AIB 0001 SU-BPU 320-214

2938 AIB 0971 F-GRXL 319-111

2939 AIB 0001 B-6301 320-214

2940 AIB 0119 B-6160 319-132

2941 AIB 0058 TC-JPE 320-232

2942 AIB 0125 N525NK 319-132

2943 AIB 0305 HL7753 320-232

2944 AIB 0107 9M-AFM 320-216

2945 AIB 0646 N646JB 320-232

2946 AIB 0090 G-EZBG 319-111

2947 AIB 0109 VP-BQW 320-214





2948 AIB 0120 B-6161 319-132

2949 AIB 0001 D-AIDR 319-115

2950 AIB 0068 B-6303 320-214

2951 AIB 0815 F-GUGO 318-111

2952 AIB 0004 9V-TAH 320-232

2953 AIB 0104 F-OHGX 320-232

2954 AIB 0103 RP-C8602 319-112

2955 AIB 0002 YR-ASB 318-111

2956 AIB 0108 9M-AFN 320-216

2957 AIB 0206 VP-BQX 321-211

2958 AIB 0005 VT-INE 320-232

2959 AIB 0091 G-EZBH 319-111

2960 AIB 0069 B-6292 320-214

2961 AIB 0972 F-GRXM 319-111

2962 AIB 0015 EC-JYX 320-214

2963 AIB 0126 N526NK 319-132

2964 AIB 0004 A6-ABH 320-214

2965 AIB 0207 VP-BQT 321-211

2966 AIB 0002 SU-BPV 320-214

2967 AIB 0816 F-GUGP 318-111

2968 AIB 0011 D-ABDK 320-214

2969 AIB 0121 B-6162 319-132

2970 AIB 0648 N648JB 320-232

2971 AIB 0317 B-6305 321-231

2972 AIB 0817 F-GUGQ 318-111

2973 AIB 0005 B-6296 320-214

2974 AIB 0006 VN-A350 321-231

2975 AIB 0101 B-6298 320-214

2976 AIB 0103 D-AGWC 319-132





2977 AIB 0649 N649JB 320-232

2978 AIB 0127 N527NK 319-132

2979 AIB 0003 N501VL 319-133

2980 AIB 0006 B-6297 320-214

2981 AIB 0410 G-DBCJ 319-131

2982 AIB 0005 9V-TAI 320-232

2983 AIB 0128 N528NK 319-132

2984 AIB 0059 TC-JPF 320-232

2985 AIB 0058 B-6169 319-112

2986 AIB 0070 B-6293 320-214

2987 AIB 0151 P4-UAS 320-232

2988 AIB 0016 EC-JZI 320-214

2989 AIB 0109 9M-AFO 320-216

2990 AIB 0006 VT-INF 320-232

2991 AIB 0012 D-ABDL 320-214

2992 AIB 0651 N651JB 320-232

2993 AIB 0628 N628VA 320-214

2994 AIB 0101 RP-C3242 320-214

2995 AIB 0003 EI-DSC 320-216

2996 AIB 0253 EC-JZM 321-212

2997 AIB 0255 XA-VOC 319-132

2998 AIB 0101 JA204A 320-214

2999 AIB 0305 TC-JRC 321-231

3000 AIB 0110 9M-AFP 320-216

3001 AIB 0201 CC-CVA 318-121

3002 AIB 0206 PR-MHG 320-214

3003 AIB 0092 G-EZBI 319-111

R 3004 AIB 0251 A6-EIF 320-232

3005 AIB 0007 VN-A351 321-231





3006 AIB 0013 D-ABDM 320-214

3007 AIB 0129 N529NK 319-132

3008 AIB 0655 F-GKXN 320-214

3009 AIB 0818 F-GUGR 318-111

3010 AIB 0060 TC-JPG 320-232

3011 AIB 0104 D-AGWD 319-132

3012 AIB 0509 VT-DNZ 320-232

3013 AIB 0008 VN-A352 321-231

3014 AIB 0002 B-6309 320-214

3015 AIB 0306 TC-JRD 321-231

3016 AIB 0005 9K-CAE 320-214

3017 AIB 0130 N530NK 319-132

3018 AIB 0111 9M-AFQ 320-216

3019 AIB 0101 OE-LEK 319-112

3020 AIB 0122 B-6168 319-132

3021 AIB 0014 D-ABDN 320-214

3022 AIB 0009 VN-A353 321-231

3023 AIB 0003 B-6310 320-214

3024 AIB 0003 B-6163 319-112

3025 AIB 0004 JA04MC 320-214

3026 AIB 0131 N531NK 319-132

3027 AIB 0102 B-6311 320-214

3028 AIB 0950 N950FR 319-111

3029 AIB 0652 N652JB 320-232

3030 AIB 0202 CC-CVB 318-121

3031 AIB 0054 OK-MEH 320-214

3032 AIB 0014 PR-MBN 319-132

3033 AIB 0001 SX-DVG 320-232

3034 AIB 0405 VT-KFS 321-232





3035 AIB 0202 PR-MHI 320-214

3036 AIB 0093 G-EZBJ 319-111

3037 AIB 0629 PR-MHL 320-214

3038 AIB 0808 N808FR 318-111

3039 AIB 0653 N653JB 320-232

3040 AIB 0017 EC-KAX 320-214

3041 AIB 0094 G-EZBK 319-111

3042 AIB 0231 N494TA 320-233

3043 AIB 0201 OK-MEK 319-112

3044 AIB 0005 A6-ABI 320-214

3045 AIB 0004 XA-VOD 319-133

3046 AIB 0001 OE-LGS 319-115

3047 AIB 0203 PR-MHJ 320-214

3048 AIB 0102 RP-C3243 320-214

3049 AIB 0411 G-DBCK 319-131

R 3050 AIB 0252 A6-EIG 320-232

3051 AIB 0151 F-GTAN 321-212

3052 AIB 0110 VP-BRY 320-214

3053 AIB 0095 G-EZBL 319-111

3054 AIB 0308 EC-KBJ 319-111

3055 AIB 0015 D-ABDO 320-214

3056 AIB 0422 9H-AEP 320-214

3057 AIB 0312 N480TA 319-132

3058 AIB 0204 PR-MHK 320-214

3059 AIB 0096 G-EZBM 319-111

3060 AIB 0055 OK-MEI 320-214

3061 AIB 0097 G-EZBN 319-111

3062 AIB 0203 CC-CVF 318-121

3063 AIB 0111 VP-BRX 320-214





3064 AIB 0112 9M-AFR 320-216

3065 AIB 0756 F-GRXN 319-115

3066 AIB 0002 SX-DVH 320-232

3067 AIB 0318 B-6306 321-231

3068 AIB 0423 9H-AEQ 320-214

3069 AIB 0005 XA-VOE 319-133

3070 AIB 0004 CN-ROM 321-211

3071 AIB 0106 A7-ADU 320-232

3072 AIB 0655 N655JB 320-232

R 3073 AIB 0003 VP-BED 319-115

3074 AIB 0003 SX-DVI 320-232

3075 AIB 0319 B-6307 321-231

3076 AIB 0004 EI-DSD 320-216

3077 AIB 0006 XA-VOF 319-133

3078 AIB 0309 EC-KBX 319-111

3079 AIB 0005 EI-DSE 320-216

3080 AIB 0006 EI-DSF 320-216

3081 AIB 0109 G-EUXJ 321-231

3082 AIB 0098 G-EZBO 319-111

3083 AIB 0018 EC-KDH 320-214

3084 AIB 0099 G-EZBP 319-111

3085 AIB 0002 D-AICY 319-115

3086 AIB 0009 VT-INI 320-232

3087 AIB 0011 RP-C8604 320-214

3088 AIB 0100 G-EZBR 319-111

3089 AIB 0152 VT-KFT 320-232

3090 AIB 0101 G-EZBT 319-111

3091 AIB 0656 N656JB 320-232

3092 AIB 0809 N809FR 318-111





3093 AIB 0016 D-ABDP 320-214

3094 AIB 0202 OK-MEL 319-112

3095 AIB 0019 EC-KDG 320-214

3096 AIB 0201 TS-IMQ 319-112

3097 AIB 0056 OK-MEJ 320-214

3098 AIB 0152 F-GTAO 321-212

3099 AIB 0102 JA205A 320-214

3100 AIB 0001 LX-GJC 318-112

3101 AIB 0630 N630VA 320-214

3102 AIB 0310 EC-KDI 319-111

3103 AIB 0232 N495TA 320-233

3104 AIB 0106 9V-SBF 319-132

3105 AIB 0153 VT-KFV 320-232

3106 AIB 0106 G-TTIF 321-231

3107 AIB 0012 RP-C8605 320-214

3108 AIB 0104 RP-C8603 319-112

3109 AIB 0401 EC-KCU 320-216

3110 AIB 0810 N810FR 318-111

3111 AIB 0205 PR-MHE 320-214

3112 AIB 0320 B-6308 321-231

3113 AIB 0233 N496TA 320-233

3114 AIB 0307 D-AYYA 319-133

3115 AIB 0007 EI-DSG 320-216

3116 AIB 0308 D-AYYB 319-133

3117 AIB 0113 9M-AFS 320-216

3118 AIB 0102 G-EZBU 319-111

3119 AIB 0657 N657JB 320-232

3120 AIB 0406 VT-KFW 321-232

3121 AIB 0017 D-ABDQ 320-214





3122 AIB 0103 G-EZBV 319-111

3123 AIB 0424 N213MX 320-214

3124 AIB 0309 D-AYYC 319-133

3125 AIB 0504 LZ-MDB 320-232

3126 AIB 0307 TC-JRE 321-231

3127 AIB 0001 HA-LPJ 320-232

3128 AIB 0105 D-AGWE 319-132

3129 AIB 0223 EI-DVE 320-214

3130 AIB 0101 VT-PPA 321-211

3131 AIB 0425 B-6312 320-214

3132 AIB 0009 B-6313 320-214

3133 AIB 0002 P4-MIS 319-115

3134 AIB 0104 G-EZBW 319-111

3135 AIB 0631 N631VA 320-214

3136 AIB 0224 EI-DVF 320-214

3137 AIB 0105 G-EZBX 319-111

3138 AIB 0006 I-WEBA 320-214

3139 AIB 0201 D-ABGE 319-112

3140 AIB 0114 9M-AFT 320-216

3141 AIB 0152 P4-VAS 320-232

3142 AIB 0101 HS-PGS 319-132

3143 AIB 0002 HA-LPK 320-232

3144 AIB 0123 B-6239 319-132

3145 AIB 0402 EC-KDT 320-216

3146 AIB 0102 VT-PPB 321-211

3147 AIB 0103 JA206A 320-214

3148 AIB 0104 JA207A 320-214

3149 AIB 0001 XA-UHE 320-214

3150 AIB 0658 N658JB 320-232





3151 AIB 0403 EC-KDX 320-216

R 3152 AIB 0201 A6-ABN 320-214

3153 AIB 0426 B-6315 320-214

3154 AIB 0115 9M-AFU 320-216

3155 AIB 0632 N632VA 320-214

3156 AIB 0140 PR-MBO 320-232

3157 AIB 0112 VP-BRZ 320-214

3158 AIB 0003 B-6322 320-232

3159 AIB 0010 VT-INJ 320-232

3160 AIB 0002 XA-VAI 320-214

3161 AIB 0007 I-WEBB 320-214

3162 AIB 0510 VT-DNY 320-232

3163 AIB 0812 N812FR 318-111

3164 AIB 0001 VP-BXT 320-214

3165 AIB 0132 N532NK 319-132

3166 AIB 0003 HA-LPL 320-232

3167 AIB 0004 B-6323 320-232

3168 AIB 0404 B-6167 319-115

3169 AIB 0311 EC-KEV 319-111

3170 AIB 0234 B-6333 320-214

R 3171 AIB 0001 SU-KBB 319-112

3172 AIB 0106 D-AGWF 319-132

3173 AIB 0116 9M-AFV 320-216

3174 AIB 0404 EC-KFI 320-216

3175 AIB 0007 XA-VOG 319-133

3176 AIB 0106 G-EZBY 319-111

3177 AIB 0004 HA-LPM 320-232

3178 AIB 0008 EI-DSH 320-216

3179 AIB 0312 EC-KFT 319-111





3180 AIB 0207 PR-MHF 320-214

3181 AIB 0523 N523VA 319-112

3182 AIB 0117 9M-AFX 320-216

3183 AIB 0511 VT-DNX 320-232

3184 AIB 0107 G-EZBZ 319-111

3185 AIB 0061 TC-JPH 320-232

3186 AIB 0405 B-6172 319-115

3187 AIB 0013 RP-C8606 320-214

3188 AIB 0202 D-ABGF 319-112

3189 AIB 0105 JA208A 320-214

3190 AIB 0659 N659JB 320-232

3191 AIB 0208 VP-BRW 321-211

3192 AIB 0011 VT-INK 320-232

3193 AIB 0107 D-AGWG 319-132

3194 AIB 0118 9M-AFY 320-216

3195 AIB 0011 B-6235 319-131

3196 AIB 0005 B-6325 320-232

3197 AIB 0235 B-6335 320-214

3198 AIB 0010 VN-A354 321-231

3199 AIB 0001 UN-A2001 320-214

3200 AIB 0012 B-6236 319-131

3201 AIB 0119 9M-AFZ 320-216

3202 AIB 0203 D-ABGG 319-112

3203 AIB 0405 EC-KHN 320-216

3204 AIB 0524 N524VA 319-112

3205 AIB 0014 RP-C8607 320-214

3206 AIB 0010 B-6316 320-214

3207 AIB 0308 TC-JRF 321-231

3208 AIB 0062 TC-JPI 320-232





3209 AIB 0313 EC-KHM 319-111

3210 AIB 0006 B-6321 320-232

3211 AIB 0211 PR-MHM 320-214

3212 AIB 0103 VT-PPD 321-211

3213 AIB 0009 EI-DSI 320-216

3214 AIB 0204 CC-CVH 318-121

3215 AIB 0101 B-6336 320-214

3216 AIB 0205 CC-CVN 318-121

3217 AIB 0321 B-6317 321-231

3218 AIB 0101 A6-ABJ 320-214

3219 AIB 0512 VT-DNW 320-232

3220 AIB 0003 YR-ASC 318-111

3221 AIB 0102 B-6337 320-214

3222 AIB 0401 PT-MXA 321-231

3223 AIB 0120 9M-AHA 320-216

3224 AIB 0001 5A-ONA 320-214

3225 AIB 0004 YR-ASD 318-111

3226 AIB 0117 B-6237 319-115

3227 AIB 0012 VT-INL 320-232

3228 AIB 0661 N661JB 320-232

3229 AIB 0402 PT-MXB 321-231

3230 AIB 0633 N633VA 320-214

3231 AIB 0151 OY-KBR 319-131

3232 AIB 0121 9M-AHB 320-216

3233 AIB 0307 B-6329 321-211

3234 AIB 0103 B-6340 320-214

3235 AIB 0110 G-EUXK 321-231

3236 AIB 0002 5A-ONB 320-214

3237 AIB 0406 EC-KJD 320-216





3238 AIB 0001 VP-CKS 318-112

3239 AIB 0063 TC-JPJ 320-232

3240 AIB 0212 PR-MHN 320-214

3241 AIB 0322 B-6319 321-231

3242 AIB 0018 D-ABDR 320-214

3243 AIB 0001 VP-CBN 319-115

3244 AIB 0306 HL7762 320-232

3245 AIB 0204 D-ABGH 319-112

R 3246 AIB 0202 A6-ABM 320-214

3247 AIB 0308 B-6330 321-211

3248 AIB 0313 N520TA 319-132

3249 AIB 0309 B-6331 321-211

3250 AIB 0118 B-6238 319-115

3251 AIB 0323 B-6318 321-231

3252 AIB 0257 PK-RMD 319-132

3253 AIB 0008 XA-VOH 319-133

3254 AIB 0111 G-EUXL 321-231

3255 AIB 0314 EC-KJC 319-111

3256 AIB 0001 VT-WAE 320-214

3257 AIB 0064 TC-JPK 320-232

3258 AIB 0124 B-6240 319-132

R 3259 AIB 0013 TC-TCC 320-232

3260 AIB 0001 OE-IAC 319-115

3261 AIB 0122 9M-AHC 320-216

3262 AIB 0310 B-6332 321-211

3263 AIB 0662 N662JB 320-232

3264 AIB 0101 PK-RME 320-232

3265 AIB 0157 D-AISH 321-231

3266 AIB 0213 PR-MHP 320-214





3267 AIB 0209 VP-BUM 321-211

3268 AIB 0104 B-6341 320-214

3269 AIB 0125 B-6241 319-132

3270 AIB 0154 VT-KFX 320-232

3271 AIB 0902 VT-SCG 319-112

3272 AIB 0103 RP-C3244 320-214

3273 AIB 0015 RP-C8609 320-214

3274 AIB 0401 A7-ADV 321-231

3275 AIB 0006 VH-VNC 320-232

3276 AIB 0314 N521TA 319-132

3277 AIB 0123 HS-ABA 320-216

3278 AIB 0214 PR-MHO 320-214

3279 AIB 0009 XA-VOJ 319-133

3280 AIB 0015 CC-CQM 320-233

3281 AIB 0055 VP-BUK 319-111

3282 AIB 0003 SU-BPW 320-214

3283 AIB 0309 TC-JRG 321-231

3284 AIB 0215 PR-MHQ 320-214

3285 AIB 0059 B-6177 319-112

3286 AIB 0003 XA-MXM 320-214

3287 AIB 0663 N663JB 320-232

3288 AIB 0903 VT-SCH 319-112

3289 AIB 0019 D-ABDS 320-214

3290 AIB 0112 G-EUXM 321-231

3291 AIB 0124 9M-AHD 320-216

3292 AIB 0152 OY-KBT 319-131

3293 AIB 0023 EC-KKT 320-214

3294 AIB 0403 PT-MXC 321-231

3295 AIB 0010 EI-DSJ 320-216





3296 AIB 0007 VH-VND 320-232

3297 AIB 0206 HL7763 321-231

3298 AIB 0056 VP-BUN 319-111

3299 AIB 0125 HS-ABB 320-216

3300 AIB 0904 VT-SCI 319-112

3301 AIB 0218 G-EUUS 320-232

3302 AIB 0451 VT-KFY 321-232

3303 AIB 0065 TC-JPL 320-232

3304 AIB 0008 XA-MXK 320-214

3305 AIB 0905 VT-SCJ 319-112

3306 AIB 0002 VT-WAF 320-214

3307 AIB 0301 B-6327 321-213

R 3308 AIB 0014 TC-TCD 320-232

3309 AIB 0002 N554SX 319-112

3310 AIB 0016 RP-C8610 320-214

3311 AIB 0126 B-6242 319-132

3312 AIB 0004 XA-TLC 320-214

3313 AIB 0216 PR-MHR 320-214

3314 AIB 0219 G-EUUT 320-232

3315 AIB 0011 VN-A356 321-231

3316 AIB 0513 VT-DNV 320-232

3317 AIB 0258 PK-RMF 319-132

3318 AIB 0225 EI-DVG 320-214

3319 AIB 0016 CC-CQN 320-233

3320 AIB 0315 EC-KKS 319-111

3321 AIB 0024 EC-KLB 320-214

3322 AIB 0452 VT-KFZ 321-232

3323 AIB 0004 SU-BPX 320-214

3324 AIB 0525 N525VA 319-112





3325 AIB 0217 PR-MHS 320-214

3326 AIB 0104 VT-PPE 321-211

3327 AIB 0126 9M-AHE 320-216

3328 AIB 0011 EI-DSK 320-216

3329 AIB 0302 B-6326 321-213

3330 AIB 0102 PK-RMG 320-232

3331 AIB 0003 N501SX 319-112

3332 AIB 0008 VH-VNF 320-232

3333 AIB 0001 B-6186 318-112

3334 AIB 0210 VP-BUP 321-211

3335 AIB 0015 VT-INO 320-232

3336 AIB 0057 VP-BUO 319-111

3337 AIB 0103 B-6350 320-214

3338 AIB 0127 HS-ABC 320-216

3339 AIB 0158 D-AISI 321-231

3340 AIB 0105 VT-PPF 321-211

3341 AIB 0066 TC-JPM 320-232

3342 AIB 0127 B-6243 319-132

3343 AIB 0012 EI-DSL 320-216

3344 AIB 0906 VT-SCK 319-112

3345 AIB 0226 EI-DVH 320-214

3346 AIB 0205 D-ABGI 319-112

3347 AIB 0526 N526VA 319-112

3348 AIB 0665 N665JB 320-232

3349 AIB 0006 9K-CAF 320-214

3350 AIB 0310 TC-JRH 321-231

3351 AIB 0220 G-EUUU 320-232

3352 AIB 0108 D-AGWH 319-132

3353 AIB 0128 9M-AHF 320-216





3354 AIB 0005 HA-LPN 320-232

3355 AIB 0012 VN-A357 321-231

3356 AIB 0001 VP-BGF 319-115

3357 AIB 0016 VT-INP 320-232

3358 AIB 0109 D-AGWI 319-132

3359 AIB 0634 N634VA 320-214

3360 AIB 0159 D-AISJ 321-231

3361 AIB 0001 VP-CXZ 320-214

3362 AIB 0013 EI-DSM 320-216

R 3363 AIB 0102 9H-AFL 318-112

3364 AIB 0001 D-AHIH 319-111

3365 AIB 0004 SX-DVJ 320-232

3366 AIB 0427 B-6351 320-214

3367 AIB 0106 VT-PPG 321-211

3368 AIB 0105 B-6338 320-214

3369 AIB 0402 A7-ADW 321-231

3370 AIB 0129 9M-AHG 320-216

3371 AIB 0206 CC-CVP 318-121

3372 AIB 0153 F-GTAP 321-212

3373 AIB 0113 VP-BQU 320-214

3374 AIB 0009 XA-MXL 320-214

3375 AIB 0110 D-AGWJ 319-132

3376 AIB 0407 EC-KLT 320-216

3377 AIB 0316 EC-KME 319-111

3378 AIB 0234 N497TA 320-233

3379 AIB 0514 VP-CHN 320-232

3380 AIB 0317 EC-KMD 319-111

3381 AIB 0703 N703JB 320-232

3382 AIB 0151 G-TTIG 321-231





3383 AIB 0011 B-6352 320-214

3384 AIB 0006 HA-LPO 320-232

R 3385 AIB 0004 AP-BIE 319-112

3386 AIB 0007 B-6347 320-232

3387 AIB 0160 D-AISK 321-231

R 3388 AIB 0005 AP-BIF 319-112

3389 AIB 0201 N201FR 320-214

3390 AIB 0207 CC-CVR 318-121

3391 AIB 0218 PR-MHU 320-214

3392 AIB 0005 SX-DVK 320-232

3393 AIB 0133 N533NK 319-132

3394 AIB 0130 HS-ABD 320-216

3395 AIB 0134 N534NK 319-132

3396 AIB 0002 VP-CXY 320-214

3397 AIB 0403 A7-ADX 321-231

3398 AIB 0635 N635VA 320-214

3399 AIB 0154 F-GTAQ 321-212

3400 AIB 0408 EC-KMI 320-216

3401 AIB 0155 F-GTAR 321-212

3402 AIB 0515 VP-CSS 320-232

3403 AIB 0002 D-AHII 319-111

3404 AIB 0131 9M-AFW 320-216

3405 AIB 0311 TC-JRI 321-231

3406 AIB 0203 OK-NEM 319-112

3407 AIB 0102 OE-LED 319-112

3408 AIB 0001 HK-4549 320-214

3409 AIB 0007 HA-LPQ 320-232

3410 AIB 0114 VP-BKX 320-214

3411 AIB 0108 G-EZDB 319-111





3412 AIB 0014 EI-DSN 320-216

3413 AIB 0109 G-EZDA 319-111

3414 AIB 0017 VT-INQ 320-232

3415 AIB 0206 D-ABGJ 319-112

3416 AIB 0705 N705JB 320-232

3417 AIB 0527 N527VA 319-112

3418 AIB 0235 N498TA 320-233

3419 AIB 0156 F-GTAS 321-212

3420 AIB 0610 F-GKXO 320-214

3421 AIB 0151 HS-PGT 319-132

3422 AIB 0051 D-ABDT 320-214

3423 AIB 0006 SX-DVL 320-232

3424 AIB 0201 HS-PGX 319-132

3425 AIB 0003 VP-CXX 320-214

3426 AIB 0110 G-EZDE 319-111

3427 AIB 0132 9M-AHH 320-216

3428 AIB 0301 JY-AYL 319-132

3429 AIB 0312 TC-JRJ 321-231

3430 AIB 0008 HA-LPR 320-232

3431 AIB 0202 N202FR 320-214

3432 AIB 0111 G-EZDF 319-111

3433 AIB 0010 RP-C3245 320-214

3434 AIB 0161 D-AISL 321-231

3435 AIB 0012 B-6358 320-214

3436 AIB 0204 OK-NEN 319-112

3437 AIB 0307 HL7769 320-232

3438 AIB 0208 CC-CVS 318-121

3439 AIB 0007 SX-DVM 320-232

3440 AIB 0428 B-6357 320-214





3441 AIB 0157 F-GTAT 321-212

3442 AIB 0112 G-EZDD 319-111

3443 AIB 0318 EC-KOY 319-111

3444 AIB 0151 A6-ABK 320-214

3445 AIB 0528 N528VA 319-112

3446 AIB 0429 VP-BCZ 320-214

3447 AIB 0207 D-ABGK 319-112

3448 AIB 0133 9M-AHI 320-216

3449 AIB 0008 B-6348 320-232

3450 AIB 0010 XA-VOK 319-133

3451 AIB 0706 N706JB 320-232

3452 AIB 0205 OK-NEO 319-112

3453 AIB 0018 VT-INR 320-232

3454 AIB 0202 HS-PGY 319-132

3455 AIB 0017 RP-C8611 320-214

3456 AIB 0433 B-6359 320-214

3457 AIB 0019 VT-INS 320-232

3458 AIB 0203 JY-AYJ 321-231

3459 AIB 0324 B-6342 321-231

3460 AIB 0636 N636VA 320-214

3461 AIB 0104 B-6390 320-214

3462 AIB 0101 SX-DVO 321-231

3463 AIB 0614 N502VL 319-132

3464 AIB 0015 EI-DSO 320-216

3465 AIB 0637 N637VA 320-214

3466 AIB 0113 G-EZDH 319-111

3467 AIB 0101 HK-4553 319-115

3468 AIB 0221 G-EUUV 320-232

3469 AIB 0209 CC-CVU 318-121





3470 AIB 0611 F-GKXP 320-214

R 3471 AIB 0311 B-6345 321-211

3472 AIB 0011 RP-C3246 320-214

3473 AIB 0430 VP-BCP 320-214

3474 AIB 0201 VH-VQF 320-232

3475 AIB 0004 VP-CXW 320-214

3476 AIB 0152 A6-ABL 320-214

3477 AIB 0134 9M-AHJ 320-216

3478 AIB 0008 SX-DVN 320-232

3479 AIB 0708 N708JB 320-232

3480 AIB 0201 TS-INO 320-214

3481 AIB 0501 B-6346 320-232

3482 AIB 0016 EI-DSP 320-216

R 3483 AIB 0308 HL-7772 320-232

3484 AIB 0101 P4-WAS 320-232

R 3485 AIB 0106 F-WWIG 320-214

3486 AIB 0135 9M-AHK 320-216

R 3487 AIB 0012 RP-C3247 320-214

3488 AIB 0709 N709JB 320-232

3489 AIB 0136 HS-ABE 320-216

3490 AIB 0431 VP-BCS 320-214

3491 AIB 0615 N503VL 319-132

R 3492 AIB 0013 EK32005 320-214

3493 AIB 0325 B-6343 321-231

3494 AIB 0432 VP-BDT 320-214

3495 AIB 0202 VH-VQE 320-232

3496 AIB 0309 HL7773 320-232

3497 AIB 0020 VT-INT 320-232

3498 AIB 0107 VT-PPH 321-211





3499 AIB 0222 G-EUUW 320-232

3500 AIB 0111 D-AGWK 319-132

3501 AIB 0227 EI-DVI 320-214

3502 AIB 0017 EI-DSR 320-216

3503 AIB 0638 N638VA 320-214

3504 AIB 0201 OE-LES 321-211

3505 AIB 0137 HS-ABF 320-216

3506 AIB 0105 B-6391 320-214

3507 AIB 0326 B-6339 321-231

3508 AIB 0005 XA-XII 320-214

R 3509 AIB 0210 CC-CVV 318-121

3510 AIB 0236 N499TA 320-233

3511 AIB 0115 VP-BKY 320-214

3512 AIB 0056 G-MEDN 321-231

3513 AIB 0001 D-ALEY 319-115

3514 AIB 0006 XA-JCV 320-214

3515 AIB 0018 EI-DSS 320-216

3516 AIB 0052 D-ABDU 320-214

3517 AIB 0712 N712JB 320-232

3518 AIB 0102 HK-4552 319-115

3519 AIB 0102 P4-XAS 320-232

3520 AIB 0103 B-6182 319-132

3521 AIB 0138 9M-AHL 320-216

3522 AIB 0204 JY-AYK 321-231

3523 AIB 0303 B-6361 321-213

R 3524 AIB 0516 PK-RMK 320-232

3525 AIB 0313 TC-JRK 321-231

3526 AIB 0009 SX-DVQ 320-232

3527 AIB 0102 SX-DVP 321-231





3528 AIB 0013 B-6360 320-214

3529 AIB 0025 EC-KRH 320-214

R 3530 AIB 0001 DAIJA 318-112

3531 AIB 0009 UR-WUA 320-232

3532 AIB 0019 EI-DST 320-216

3533 AIB 0003 D-AHIJ 319-112

R 3534 AIB 0112 G-AGWL 319-132

3535 AIB 0017 CC-CQO 320-233

3536 AIB 0139 9M-AHM 320-216

3537 AIB 0114 G-EZDI 319-111

3538 AIB 0237 N680TA 320-233

3539 AIB 0314 TC-JRL 321-231

3540 AIB 0219 PR-MHV 320-214

3541 AIB 0021 VT-INU 320-232

3542 AIB 0003 VP-BVA 319-115

R 3543 AIB 0517 PK-RML 320-232

3544 AIB 0115 G-EZDJ 319-111

3545 AIB 0116 VP-BKC 320-214

3546 AIB 0152 G-TTIH 321-231

3547 AIB 0203 VH-VQD 320-232

3548 AIB 0101 B-6178 319-132

3549 AIB 0140 9M-AHN 320-216

3550 AIB 0223 G-EUUX 320-232

3551 AIB 0907 VT-SCL 319-112

3552 AIB 0327 B-6353 321-231

3553 AIB 0018 RP-C8612 320-214

3554 AIB 0715 N715JB 320-232

3555 AIB 0116 G-EZDK 319-111

3556 AIB 0018 CC-CQP 320-233





3557 AIB 0108 VT-PPI 321-211

3558 AIB 0067 TC-JPN 320-232

3559 AIB 0239 B-6370 320-214

3560 AIB 0004 D-AHIK 319-112

3561 AIB 0102 B-6179 319-132

R 3562 AIB 0010 LZ-WZB 320-232

3563 AIB 0020 EI-DSU 320-216

3564 AIB 0006 LZ-FBA 319-112

3565 AIB 0220 PR-MHX 320-214

3566 AIB 0328 B-6355 321-231

3567 AIB 0068 TC-JPO 320-232

3568 AIB 0141 9M-AHO 320-216

3569 AIB 0117 G-EZDL 319-111

3570 AIB 0051 9V-SLJ 320-233

3571 AIB 0118 G-EZDM 319-111

3572 AIB 0729 N729JB 320-232

3573 AIB 0109 VT-PPJ 321-211

3574 AIB 0117 VP-BZO 320-214

3575 AIB 0153 G-TTII 321-231

3576 AIB 0142 HS-ABG 320-216

3577 AIB 0238 N681TA 320-233

3578 AIB 0104 B-6180 319-132

3579 AIB 0019 RP-C8613 320-214

3580 AIB 0105 B-6181 319-132

3581 AIB 0239 N682TA 320-233

3582 AIB 0143 9M-AHP 320-216

3583 AIB 0151 B-6387 321-231

3584 AIB 0193 N193UW 321-211

3585 AIB 0211 CC-CZJ 318-121





3586 AIB 0208 D-ABGL 319-112

3587 AIB 0329 B-6356 321-231

3588 AIB 0351 PR-MBU 319-132

3589 AIB 0005 D-AHIL 319-112

3590 AIB 0616 N504VL 319-132

N 3591 AIB 0009 320-232

3592 AIB 0162 D-AISN 321-231

3593 AIB 0312 B-6366 321-211

3594 AIB 0221 PR-MHY 320-214

3595 AIB 0352 PR-MBV 319-132

R 3596 AIB 0107 B-6395 320-214

R 3597 AIB 0001 VT-WAG 320-214

3598 AIB 0021 EI-DSV 320-216

3599 AIB 0434 B-6377 320-214

3600 AIB 0013 VN-A358 321-231

R 3601 AIB 0106 B-6393 320-214

3602 AIB 0212 CC-CZN 318-121

3603 AIB 0069 TC-JPP 320-232

3604 AIB 0209 D-ABGM 319-112

R 3605 AIB 0151 B-6396 320-214

3606 AIB 0213 CC-CZQ 318-121

3607 AIB 0224 G-EUUY 320-232

3608 AIB 0119 G-EZDN 319-111

3609 AIB 0022 EI-DSW 320-216

R 3610 AIB 0144 PK-AXA 320-216

3611 AIB 0240 B-6371 320-214

3612 AIB 0313 B-6367 321-211

3613 AIB 0502 B-6372 320-232

3614 AIB 0401 P4-YAS 319-132





3615 AIB 0101 5A-ONC 319-111

R 3616 AIB 0002 VT-WAH 320-214

3617 AIB 0207 D-AUAH 318-112

3618 AIB 0022 VT-INV 320-232

3619 AIB 0110 VT-PPK 321-211

3620 AIB 0908 VT-SCM 319-112

R 3621 AIB 0518 VT-KRD 320-232

3622 AIB 0746 N746JB 320-232

3623 AIB 0304 B-6362 321-213

R 3624 AIB 0201 XA-VOM 320-233

3625 AIB 0163 D-AISO 321-231

R 3626 AIB 0102 A6-ABO 320-214

3627 AIB 0119 VP-BZQ 320-214

3628 AIB 0145 9M-AHQ 320-216

3629 AIB 0194 N194UW 321-211

R 3630 AIB 0222 PR-MHW 320-214

3631 AIB 0118 VP-BZP 320-214

R 3632 AIB 0002 D-AHAD 319-115

3633 AIB 0195 N195UW 321-211

3634 AIB 0120 G-EZDO 319-111

R 3635 AIB 0214 CC-CZR 318-121

3636 AIB 0404 A7-ADY 321-231

R 3637 AIB 0453 VT-KRA 321-232

3638 AIB 0106 319-132

3639 AIB 0314 B-6368 321-211

3640 AIB 0120 VP-BZR 320-214

3641 AIB 0310 HL7776 320-232

R 3642 AIB 0215 CC-CZS 318-121

R 3643 AIB 0023 EI-DSX 320-216





3644 AIB 0121 VP-BZS 320-214

3645 AIB 0330 B-6378 321-231

R 3646 AIB 0014 RP-C3248 320-214

R 3647 AIB 0201 N647AV 319-115

R 3648 AIB 0146 PK-AXC 320-216

3649 AIB 0225 G-EUUZ 320-232

3650 AIB 0503 B-6373 320-232

R 3651 AIB 0319 EC-KUB 319-111

3652 AIB 0020 RP-C8614 320-214

3653 AIB 0305 B-6363 321-213

3654 AIB 0070 TC-JPR 320-232

3655 AIB 0306 B-6365 321-213

3656 AIB 0007 9K-CAG 320-214

3657 AIB 0102 5A-OND 319-111

R 3658 AIB 0223 PR-MHZ 320-214

3659 AIB 0760 N760JB 320-232

R 3660 AIB 0206 OK-NEP 319-112

R 3661 AIB 0210 D-ABGN 319-112

R 3662 AIB 0224 PR-MYA 320-214

R 3663 AIB 0116 CC-CYE 319-132

R 3664 AIB 0002 N664AV 320-214

3665 AIB 0307 B-6382 321-213

R 3666 AIB 0024 EI-DSY 320-216

R 3667 AIB 0007 XA-ZIH 320-214

R 3668 AIB 0204 VH-VQC 320-232

3669 AIB 0405 A7-ADZ 321-231

3670 AIB 0008 9K-CAH 320-214

R 3671 AIB 0117 CC-CYF 319-132

R 3672 AIB 0202 XA-VON 320-233





R 3673 AIB 0454 VT-KRB 321-232

R 3674 AIB 0009 9V-TAJ 320-232

3675 AIB 0121 G-EZDP 319-111

R 3676 AIB 0023 VT-INW 320-232

3677 AIB 0504 B-6375 320-232

3678 AIB 0308 B-6383 321-213

R 3679 AIB 0147 HS-ABH 320-216

R 3680 AIB 0310 B-6185 319-133

3681 AIB 0331 B-6379 321-231

3682 AIB 0315 B-6369 321-211

3683 AIB 0122 G-EZDR 319-111

R 3684 AIB 0529 N529VA 319-112

R 3685 AIB 0302 JY-AYM 319-132

R 3686 AIB 0530 N530VA 319-112

3687 AIB 0909 VT-SCN 319-112

R 3688 AIB 0455 VT-KRC 321-232

R 3689 AIB 0211 D-ABGO 319-112

R 3690 AIB 0008 XA-ABC 320-214

R 3691 AIB 0202 N691AV 319-115

3692 AIB 0505 B-6376 320-232

R 3693 AIB 0107 A6-EIH 320-232

R 3694 AIB 0203 HS-PGZ 319-132

R 3695 AIB 0025 EI-DSZ 320-216

R 3696 AIB 0014 B-6392 320-214

3697 AIB 0226 G-EUYA 320-232

N 3698 AIB 0015 320-214

R 3699 AIB 0122 VP-BME 320-214

R 3700 AIB 0001 D-ABGQ 319-112

R 3701 AIB 0148 9M-AHR 320-216





3702 AIB 0123 G-EZDS 319-111

3703 AIB 0227 G-EUYB 320-232

R 3704 AIB 0002 D-ABGR 319-112

R 3705 AIB 0011 XA-VOO 319-133

R 3706 AIB 0107 F-WWIP 320-214

3707 AIB 0763 N763JB 320-232

R 3708 AIB 0301 D-ABCA 321-211

R 3709 AIB 0010 SX-DVS 320-232

R 3710 AIB 0353 PR-MBW 319-132

R 3711 AIB 0123 VP-BMF 320-214

R 3712 AIB 0507 N507AY 321-231

3713 AIB 0108 A6-EII 320-232

R 3714 AIB 0011 SX-DVR 320-232

R 3715 AIB 0149 PK-AXE 320-216

N 3716 AIB 0506 B-6399 320-232

R 3717 AIB 0751 VT-KRE 321-232

3718 AIB 0071 TC-JPS 320-232

3719 AIB 0072 TC-JPT 320-232

3720 AIB 0124 G-EZDT 319-111

R 3721 AIB 0228 G-EUYC 320-232

3722 AIB 0309 B-6385 321-213

N 3723 AIB 0001 554 320-214

3724 AIB 0766 N766JB 320-232

3725 AIB 0310 B-6386 321-213

R 3726 AIB 0229 G-EUYD 320-232

R 3727 AIB 0501 PR-MYB 319-112

R 3728 AIB 0212 D-ABGP 319-112

R 3729 AIB 0150 HS-ABI 320-216

R 3730 AIB 0152 B-6551 321-231





R 3731 AIB 0021 RP-C8615 320-214

R 3732 AIB 0026 EI-DTA 320-216

R 3733 AIB 0502 PR-MYC 319-112

N 3734 AIB 0010 VH-VNH 320-232

R 3735 AIB 0125 G-EZDU 319-111

N 3736 AIB 0091 F-WWIC 320-232

R 3737 AIB 0014 VN-A359 321-231

R 3738 AIB 0456 VT-KRF 321-232

N 3739 AIB 0001 9K-EAA 320-214

R 3740 AIB 0508 N508AY 321-231

N 3741 AIB 0011 UR-WUB 320-232

R 3742 AIB 0126 G-EZDV 319-111

N 3743 AIB 0205 VH-VQB 320-232

R 3744 AIB 0320 D-AVWZ 319-111

N 3745 AIB 0012 SX-DVT 320-232

R 3746 AIB 0127 G-EZDW 319-111

N 3747 AIB 0009 B-6562 320-214

N 3748 AIB 0519 VT-KRG 320-232

R 3749 AIB 0302 D-ABCB 321-211

N 3750 AIB 0225 PR-MYD 320-214

R 3751 AIB 0208 D-AUAC 318-112

N 3752 AIB 0111 VT-PPL 321-211

N 3753 AIB 0013 SX-DVU 320-232

N 3754 AIB 0128 G-EZDX 319-111

R 3755 AIB 0451 D6-CAT 320-214

N 3756 AIB 0016 B-6550 320-214

N 3757 AIB 0259 9V-TRA 319-132

N 3758 AIB 0152 320-214

N 3759 AIB 0204 HS-PGN 319-132





N 3760 AIB 0768 N768JB 320-232

N 3761 AIB 0404 PT-MXD 321-231

N 3762 AIB 0104 RP-C3249 320-214

N 3763 AIB 0129 G-EZDY 319-111

N 3764 AIB 0332 B-6389 321-231

N 3765 AIB 0151 PK-AXF 320-216

N 3766 AIB 0311 B-6555 321-213

N 3767 AIB 0105 RP-C3250 320-214

N 3768 AIB 0107 B-6192 319-132

N 3769 AIB 0106 CS-TNQ 320-214

N 3770 AIB 0118 CC-CYI 319-132

N 3771 AIB 0012 HA-LPS 320-232

N 3772 AIB 0119 CC-CYJ 319-132

N 3773 AIB 0014 SX-DVV 320-232

N 3774 AIB 0130 G-EZDZ 319-111

N 3775 AIB 0507 320-232

N 3776 AIB 0152 9M-AHS 320-216

N 3777 AIB 0656 F-GKXQ 320-214

N 3778 AIB 0124 VQ-BAX 320-214

N 3779 AIB 0120 CC-CYL 319-132

N 3780 AIB 0032 LZ-FBE 320-214

N 3781 AIB 0452 D6-CAU 320-214

N 3782 AIB 0024 VT-INX 320-232

N 3783 AIB 0206 VH-VQA 320-232

N 3784 AIB 0333 B-6397 321-231

N 3785 AIB 0015 SX-DVW 320-232

N 3786 AIB 0125 VQ-BAY 320-214

N 3787 AIB 0101 F-WWBB 320-214

N 3788 AIB 0131 G-EZFA 319-111





N 3789 AIB 0126 VQ-BAZ 320-214

N 3790 AIB 0706 N790MX 319-112

N 3791 AIB 0002 9K-EAB 320-214

N 3792 AIB 0112 VT-PPM 321-211

N 3793 AIB 0508 B-6558 320-232

N 3794 AIB 0058 VQ-BBA 319-111

N 3795 AIB 0657 F-GKXR 320-214

N 3796 AIB 0509 N509AY 321-231

N 3797 AIB 0509 320-232

N 3798 AIB 0003 VT-WAI 320-214

N 3799 AIB 0132 G-EZFB 319-111

N 3800 AIB 0775 N775JB 320-232

N 3801 AIB 0260 9V-TRB 319-132

N 3802 AIB 0153 F-WWBV 320-214

N 3803 AIB 0303 JY-AYN 319-132

N 3804 AIB 0092 F-WWDJ 320-232

N 3805 AIB 0301 G-EZTA 320-214

N 3806 AIB 0312 B-6556 321-213

N 3807 AIB 0013 HA-LPT 320-232

N 3808 AIB 0133 G-EZFC 319-111

N 3809 AIB 0201 F-WWDV 320-214

N 3810 AIB 0134 G-EZFD 319-111

N 3811 AIB 0779 N779JB 320-232

N 3812 AIB 0520 VT-KRH 320-232

N 3813 AIB 0153 PK-AXG 320-216

N 3814 AIB 0158 F-GTAU 321-211

N 3815 AIB 0027 F-WWIF 320-216

N 3816 AIB 0405 PT-MXE 321-231

N 3817 AIB 0102 F-WWIN 320-214





N 3818 AIB 0006 319-112

N 3819 AIB 0010 320-214

N 3820 AIB 0103 SX-DVZ 321-231

N 3821 AIB 0052 320-233

N 3822 AIB 0910 VT-SCO 319-112

N 3823 AIB 0127 VQ-BBB 320-214

N 3824 AIB 0135 G-EZFE 319-111

N 3825 AIB 0658 320-214

N 3826 AIB 0101 319-115

N 3827 AIB 0004 320-214

N 3828 AIB 0351 B-6183 319-115

N 3829 AIB 0016 SX-DVX 320-232

N 3830 AIB 0202 321-211

N 3831 AIB 0028 320-216

N 3832 AIB 0304 JY-AYP 319-132

N 3833 AIB 0020 320-214

N 3834 AIB 0751 319-111

N 3835 AIB 0128 VQ-BBC 320-214

N 3836 AIB 0401 319-133

N 3837 AIB 0093 320-232

N 3838 AIB 0059 VQ-BDD 319-111

N 3839 AIB 0113 D-AGWM 319-132

N 3840 AIB 0103 320-214

N 3841 AIB 0114 D-AGWN 319-132

N 3843 AIB 0302 G-EZTB 320-214

N 3844 AIB 0136 G-EZFF 319-111

N 3845 AIB 0137 G-EZFG 319-111

N 3846 AIB 0029 320-216

N 3847 AIB 0334 B-6398 321-231





N 3848 AIB 0017 320-214

N 3849 AIB 0109 B-6193 319-133

N 3850 AIB 0017 SX-DVY 320-232

N 3851 AIB 0110 D-AVYW 319-133

N 3852 AIB 0251 320-214

N 3853 AIB 0007 319-112

N 3854 AIB 0138 G-EZFH 319-111

N 3855 AIB 0018 320-214

N 3856 AIB 0102 319-115

N 3857 AIB 0228 320-214

N 3858 AIB 0510 N510UW 321-231

N 3859 AIB 0659 320-214

N 3860 AIB 0128 B-6190 319-132

N 3861 AIB 0435 320-214

N 3862 AIB 0259 D-AVZJ 321-231

N 3863 AIB 0025 VT-INY 320-232

N 3864 AIB 0164 321-231

N 3865 AIB 0213 319-112

N 3866 AIB 0436 320-214

N 3867 AIB 0335 B-6552 321-231

N 3868 AIB 0007 320-214

N 3869 AIB 0405 321-231

N 3871 AIB 0303 G-EZTC 320-214

N 3872 AIB 0008 319-112

N 3873 AIB 0311 320-232

N 3874 AIB 0911 VT-SCP 319-112

N 3875 AIB 0154 PK-AXH 320-216

N 3876 AIB 0402 319-133

N 3877 AIB 0014 320-232





N 3878 AIB 0104 SX-DGA 321-231

N 3879 AIB 0196 321-211

N 3880 AIB 0437 320-214

N 3881 AIB 0519 321-231

N 3882 AIB 0409 320-216

N 3883 AIB 0107 CS-TNR 320-214

N 3884 AIB 0159 321-211

N 3885 AIB 0030 320-216

N 3886 AIB 0209 318-112

N 3887 AIB 0019 320-214

N 3888 AIB 0139 D-AVWH 319-111

N 3889 AIB 0008 320-214

N 3890 AIB 0129 B-6191 319-132

N 3891 AIB 0438 CS-TKO 320-214

N 3892 AIB 0207 OK-OER 319-112

N 3893 AIB 0153 321-231

N 3894 AIB 0103 320-214

N 3895 AIB 0009 319-112

N 3896 AIB 0001 320-214

N 3897 AIB 0001 319-133

N 3898 AIB 0020 320-214

N 3899 AIB 0351 321-231

N 3900 AIB 0005 320-214

N 3901 AIB 0403 319-133

N 3902 AIB 0301 320-232

N 3903 AIB 0352 B-6187 319-115

N 3904 AIB 0512 B-6559 320-232

N 3905 AIB 0101 319-112

N 3906 AIB 0031 320-216





N 3907 AIB 0003 320-214

N 3908 AIB 0226 320-214

N 3909 AIB 0304 320-214

N 3910 AIB 0501 320-232

N 3911 AIB 0152 319-132

N 3912 AIB 0230 320-232

N 3913 AIB 0305 320-214

N 3915 AIB 0006 320-214

N 3916 AIB 0352 321-231

N 3917 AIB 0401 320-232

N 3918 AIB 0912 319-112

N 3919 AIB 0009 320-214

N 3920 AIB 0336 B-6553 321-231

N 3921 AIB 0032 320-216

N 3922 AIB 0306 320-214

N 3923 AIB 0129 320-214

N 3924 AIB 0520 321-231

N 3925 AIB 0251 320-214

N 3926 AIB 0057 321-231

N 3927 AIB 0015 320-232

N 3928 AIB 0197 321-211

N 3930 AIB 0160 321-211

N 3931 AIB 0002 320-214

N 3932 AIB 0210 318-112

N 3933 AIB 0009 320-214

N 3934 AIB 0337 321-231

N 3935 AIB 0101 320-232

N 3936 AIB 0165 321-231

N 3937 AIB 0514 B-6560 320-232





N 3938 AIB 0338 321-231

N 3939 AIB 0010 320-214

N 3940 AIB 0313 321-213

N 3941 AIB 0502 320-232

N 3943 AIB 0026 VT-INZ 320-232

N 3944 AIB 0521 321-231

N 3945 AIB 0021 320-214

N 3946 AIB 0307 320-214

N 3947 AIB 0016 320-232

N 3948 AIB 0353 321-231

N 3949 AIB 0003 320-214

N 3950 AIB 0010 319-112

N 3951 AIB 0339 321-231

N 3952 AIB 0410 320-216

N 3953 AIB 0308 320-214

N 3954 AIB 0130 320-214

N 3955 AIB 0113 321-211

N 3956 AIB 0033 320-216

N 3959 AIB 0503 320-232

N 3960 AIB 0523 321-231

N 3962 AIB 0311 319-133

N 3964 AIB 0260 321-231

N 3965 AIB 0515 320-232

N 3966 AIB 0261 321-231

N 3967 AIB 0201 320-214

N 3968 AIB 0017 320-232

N 3969 AIB 0001 321-231

N 3970 AIB 0913 319-112

N 3971 AIB 0021 320-214





N 3972 AIB 0227 320-214

N 3977 AIB 0524 321-231

N 3981 AIB 0340 321-231

N 3983 AIB 0451 319-112

N 3984 AIB 0252 320-214

N 3989 AIB 0534 321-231

N 3993 AIB 0535 321-231

N 3995 AIB 0027 320-232

N 3996 AIB 0154 321-231

(1) Evolution code


PRELIMINARY PAGESLIST OF MODIFICATIONS

ENV A318/A319/A320/A321 FLEET PLP-LOM. P 1/32FCTM 09 JAN 09

M(1) MODIFICATION Linked SB Incorp. Date TitleE J0071 08 JUL 08 WINGS-WING TIP FENCES-INTRODUCE WING TIPS

INCLUDING FENCES-Applicable to: MSN 0029-3996

E K2113 08 JUL 08 FUSELAGE - REAR FUSELAGE SECTION 16A - DEFINEA321 BASIC STRUCTURE

Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502,0505, 0509, 0513-0522, 0524, 0526, 0529, 0532, 0535, 0538, 0541, 0544, 0550, 0552, 0555, 0557, 0560, 0563-0564,0567, 0570, 0576, 0581, 0583, 0586, 0591, 0593, 0595, 0597, 0599, 0604, 0606, 0614, 0620, 0631-0633, 0642, 0652,0663-0664, 0666, 0668, 0674-0675, 0677, 0680, 0684, 0687, 0692, 0699, 0715, 0725, 0731, 0746, 0761, 0765, 0771,0775, 0777, 0781, 0787, 0792, 0796, 0802, 0806, 0808, 0810-0811, 0815, 0819, 0823, 0827, 0835, 0841, 0848, 0852,0855, 0864, 0878, 0887, 0891, 0901, 0908, 0915, 0920, 0926, 0935, 0940-0941, 0954, 0956, 0959, 0961, 0963,0968, 0970, 0974, 0983, 0987, 0991, 0993, 0995, 1004, 1006, 1008, 1012, 1015, 1017, 1021, 1023-1024, 1027, 1042,1045, 1060, 1080, 1094, 1133, 1144, 1153, 1161, 1174, 1185, 1188, 1195, 1199, 1202, 1204, 1207, 1214, 1218-1220,1227, 1233, 1238, 1241, 1250, 1260, 1273, 1276, 1293, 1299, 1307, 1333, 1356, 1366, 1399, 1403, 1408, 1412, 1417,1421, 1425, 1428, 1431, 1433, 1436, 1438, 1442, 1447, 1451, 1455, 1458, 1462, 1465, 1472, 1476, 1481, 1487, 1492,1496, 1499, 1503, 1511, 1517, 1519, 1521, 1525, 1531, 1536, 1539, 1554, 1572, 1587, 1596, 1602, 1607, 1611, 1614,1619, 1623, 1629, 1632, 1636, 1638, 1642, 1651, 1658, 1666, 1670, 1675, 1681, 1690-1691, 1695, 1701, 1704, 1707,1711, 1713, 1716, 1720, 1724, 1726, 1734, 1748, 1763, 1772, 1776, 1783, 1788, 1794, 1798, 1807, 1811, 1817, 1836,1843, 1848, 1850, 1859, 1869, 1878, 1881, 1887, 1905, 1921, 1926, 1928, 1932, 1941, 1946, 1950, 1953, 1956, 1960,1966-1967, 1970, 1972, 1974, 1977-1978, 1984, 1988, 1994-1995, 2005, 2021, 2041, 2045, 2055, 2060, 2064, 2067,2076, 2080, 2105, 2107, 2110, 2115, 2117, 2190, 2208, 2211, 2216, 2220, 2226, 2234, 2247, 2255, 2261, 2267, 2270,2290, 2303, 2305, 2309, 2315, 2320, 2323-2324, 2330, 2337, 2342, 2351, 2357, 2363, 2381, 2410, 2462, 2472, 2476,2480, 2488, 2521, 2530, 2536, 2543, 2549, 2553, 2563, 2590, 2599, 2610, 2653, 2682, 2687, 2707, 2713, 2726,2730, 2736, 2741, 2756, 2759, 2767, 2793, 2799, 2809, 2823, 2862, 2868, 2882, 2895, 2903, 2912, 2916, 2919, 2927,2933, 2936, 2957, 2965, 2971, 2974, 2996, 2999, 3005, 3013, 3015, 3022, 3034, 3051, 3067, 3070, 3075, 3081, 3098,3106, 3112, 3120, 3126, 3130, 3146, 3191, 3198, 3207, 3212, 3217, 3222, 3229, 3233, 3235, 3241, 3247, 3249, 3251,3254, 3262, 3265, 3267, 3274, 3283, 3290, 3294, 3297, 3302, 3307, 3315, 3322, 3326, 3329, 3334, 3339-3340, 3350,3355, 3360, 3367, 3369, 3372, 3382, 3387, 3397, 3399, 3401, 3405, 3419, 3429, 3434, 3441, 3458-3459, 3462, 3471,3493, 3498, 3504, 3507, 3512, 3522-3523, 3525, 3527, 3539, 3546, 3552, 3557, 3566, 3573, 3575, 3583-3584, 3587,3592-3593, 3600, 3612, 3619, 3623, 3625, 3629, 3633, 3636-3637, 3639, 3645, 3653, 3655, 3665, 3669, 3673, 3678,3681-3682, 3688, 3708, 3712, 3717, 3722, 3725, 3730, 3737-3738, 3740, 3749, 3752, 3761, 3764, 3766, 3784, 3792,3796, 3806, 3814, 3816, 3820, 3847, 3858, 3862, 3867, 3878-3879, 3920, 3830, 3864, 3869, 3881, 3884, 3893, 3899,3916, 3924, 3926, 3928-3930, 3934, 3936, 3938, 3940, 3944, 3948, 3951, 3955, 3960, 3964, 3966, 3969, 3977-3981,3989-3993, 3996

E K2962 29-1055 05 08 JUL 08 HYDRAULIC POWER-BLUE MAIN HYDRAULICPOWER-IMPROVE MAINTENANCE STATUS OF BLUEHYDRAULIC RESERVOIR

Applicable to: MSN 0002-0038, 0040-0041, 0043-0086, 0089-0102, 0104-0108, 0110-0119, 0121-0131, 0133-0162,0165-0167, 0170-0173, 0176-0178, 0180-0188, 0190-0192, 0194-0209, 0211-0220, 0223-0224, 0226-0229, 0233-0246,0248-0256, 0260-0278, 0281-0282, 0285-0293, 0295-0298, 0300, 0303-0304, 0306-0307, 0310-0312, 0315-0337,0339-0342, 0346, 0348, 0350-0353, 0355-0356, 0358-0363, 0365-0372, 0375, 0377-0384, 0387-0390, 0392-0404,0406, 0408-0410, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0492,0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534, 0537,0539-0540, 0542-0543, 0545-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569,0571-0575, 0577-0580, 0582, 0584-0585, 0587-0590, 0592, 0594, 0596, 0598, 0600-0603, 0605, 0607-0613,




M(1) MODIFICATION Linked SB Incorp. Date Title0615-0619, 0621-0630, 0634-0641, 0643-0651, 0653-0662, 0665, 0667, 0669-0673, 0676, 0678-0679, 0681-0683,0685-0686, 0688-0691, 0693-0698, 0700-0714, 0716-0724, 0726-0730, 0732-0745, 0747-0760, 0762-0764,0766-0770, 0772-0774, 0776, 0778-0780, 0782-0786, 0788-0791, 0793-0795, 0797-0801, 0803-0805, 0807,0809, 0812-0814, 0816-0818, 0820-0822, 0824-0826, 0828-0834, 0836-0840, 0842-0847, 0849-0851, 0853-0854,0856-0863, 0865-0877, 0879-0886, 0888-0890, 0892-0900, 0902-0907, 0909-0914, 0916-0919, 0921-0925,0927-0934, 0936-0939, 0942-0953, 0955, 0957-0958, 0960, 0962, 0964-0967, 0969, 0971-0973, 0975-0982,0984-0986, 0988-0990, 0992, 0994, 0996-1003, 1005, 1007, 1009-1011, 1013-1014, 1016, 1018-1020, 1022,1025-1026, 1028-1041, 1043-1044, 1046-1059, 1061-1079, 1081-1093, 1095-1132, 1134-1143, 1145-1152, 1154-1160,1162-1173, 1175-1184, 1187, 1189-1194, 1196-1198, 1200-1201, 1203, 1205-1206, 1208-1213, 1215-1217, 1221-1226,1228-1232, 1234-1237, 1239-1240, 1242-1249, 1251-1259, 1261-1272, 1274-1275, 1277-1292, 1294-1298, 1300-1306,1308-1332, 1334-1355, 1357-1365, 1367-1398, 1400-1402, 1404-1407, 1409-1411, 1413-1416, 1418-1420, 1422-1424,1426-1427, 1429-1430, 1432, 1434-1435, 1437, 1439-1441, 1443-1446, 1448-1450, 1452-1454, 1456-1457, 1459-1461,1463-1464, 1466-1471, 1473-1475, 1477-1480, 1482-1486, 1488-1491, 1493-1495, 1497-1498, 1500-1502, 1504-1510,1512-1516, 1518, 1520, 1522-1524, 1526-1530, 1532-1535, 1537-1538, 1540-1553, 1555-1571, 1573-1586, 1588-1595,1597-1601, 1603-1606, 1608-1610, 1612-1613, 1615-1618, 1620-1622, 1624-1628, 1630-1631, 1633-1635, 1637,1639-1641, 1643-1650, 1652-1657, 1659-1665, 1667-1669, 1671-1674, 1676-1680, 1682-1689, 1692-1694, 1696-1700,1702-1703, 1705-1706, 1708-1710, 1712, 1714-1715, 1717-1719, 1721-1723, 1725, 1727-1733, 1735-1747, 1749-1762,1764-1771, 1773-1775, 1777-1782, 1784-1787, 1789-1793, 1795-1797, 1799-1806, 1808-1810, 1812-1816, 1818-1835,1837-1842, 1844-1847, 1849, 1851-1858, 1860-1868, 1870-1877, 1879-1880, 1882-1886, 1888-1904, 1906-1920,1922-1925, 1927, 1929-1931, 1933-1940, 1942-1945, 1947-1949, 1951-1952, 1954-1955, 1957-1959, 1961-1965,1968-1969, 1971, 1973, 1975-1976, 1979-1983, 1986-1987, 1989-1993, 1996-2004, 2006-2020, 2022-2040,2042-2044, 2046-2054, 2056-2059, 2061-2063, 2065-2066, 2068-2075, 2077-2079, 2081-2104, 2106, 2108-2109,2112-2114, 2116, 2118-2189, 2191-2207, 2209-2210, 2212-2215, 2217-2219, 2221-2225, 2227-2233, 2235-2246,2248-2254, 2256-2260, 2262-2266, 2268-2269, 2271-2289, 2291-2302, 2304, 2306-2308, 2310-2314, 2316-2319,2321-2322, 2325-2329, 2331-2336, 2338-2341, 2343-2350, 2352-2356, 2358-2362, 2364-2380, 2382-2409,2411-2461, 2463-2471, 2473-2475, 2477-2479, 2481-2487, 2489-2520, 2522-2529, 2531-2535, 2537-2542, 2544-2548,2550-2552, 2554-2562, 2564-2589, 2591-2598, 2600-2609, 2611-2652, 2654-2681, 2683-2686, 2688-2706,2708-2712, 2714-2725, 2727-2729, 2731-2735, 2737-2740, 2742-2755, 2757-2758, 2760-2766, 2768-2792,2794-2798, 2800-2808, 2810-2822, 2824-2861, 2863-2867, 2869-2881, 2883-2894, 2896-2902, 2904-2911,2913-2915, 2917-2918, 2920-2926, 2928-2932, 2934-2935, 2937-2956, 2958-2964, 2966-2970, 2972-2973,2975-2995, 2997-2998, 3000-3004, 3006-3012, 3014, 3016-3021, 3023-3033, 3035-3050, 3052-3066, 3068-3069,3071-3074, 3076-3080, 3082-3097, 3099-3105, 3107-3111, 3113-3119, 3121-3125, 3127-3129, 3131-3145, 3147-3190,3192-3197, 3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228, 3230-3232, 3234, 3236-3240, 3242-3246,3248, 3250, 3252-3253, 3255-3261, 3263-3264, 3266, 3268-3273, 3275-3282, 3284-3289, 3291-3293, 3295-3296,3298-3301, 3303-3306, 3308-3314, 3316-3321, 3323-3325, 3327-3328, 3330-3333, 3335-3338, 3341-3349,3351-3354, 3356-3359, 3361-3366, 3368, 3370-3371, 3373-3381, 3383-3386, 3388-3396, 3398, 3400, 3402-3404,3406-3418, 3420-3428, 3430-3433, 3435-3440, 3442-3457, 3460-3461, 3463-3470, 3472-3492, 3494-3497,3499-3503, 3505-3506, 3508-3511, 3513-3521, 3524, 3526, 3528-3538, 3540-3545, 3547-3551, 3553-3556,3558-3565, 3567-3572, 3574, 3576-3582, 3585-3586, 3588-3591, 3594-3599, 3601-3611, 3613-3618, 3620-3622,3624, 3626-3628, 3630-3632, 3634-3635, 3640-3644, 3646-3652, 3654, 3656-3664, 3666-3668, 3670-3672,3674-3677, 3679-3680, 3683-3687, 3689-3707, 3709-3711, 3713-3716, 3718-3721, 3723-3724, 3726-3729, 3731-3736,3739, 3741-3748, 3750-3751, 3753-3760, 3762-3763, 3765, 3767-3783, 3785-3791, 3793-3795, 3807-3813, 3815,3817-3819, 3863, 3871-3877, 3937, 3638, 3797-3805, 3821-3829, 3831-3846, 3848-3857, 3859-3861, 3865-3866,3868, 3880, 3882-3883, 3885-3892, 3894-3898, 3900-3915, 3917-3919, 3921-3923, 3925, 3927, 3931-3933, 3935,3939, 3941-3943, 3945-3947, 3949-3950, 3952-3954, 3956-3959, 3962, 3965, 3967-3968, 3970-3972, 3983-3984,3995




M(1) MODIFICATION Linked SB Incorp. Date TitleE K3154 08 JUL 08 FUSELAGE - REAR FUSELAGE - ADAPT SECTION 17/19

STRUCTURE TO A319 DEFINITIONApplicable to: MSN 0546, 0572, 0578, 0588, 0598, 0600, 0608-0610, 0612, 0616, 0618, 0621, 0623, 0625, 0627,0629, 0634, 0636-0637, 0639, 0641, 0644, 0646-0647, 0649, 0651, 0654, 0656, 0660, 0670, 0672, 0679, 0682, 0686,0688-0691, 0693-0695, 0697, 0700, 0711, 0713, 0717, 0719, 0721, 0723, 0727-0729, 0732, 0734, 0736, 0738, 0740,0742, 0744, 0748, 0750, 0752, 0755, 0757, 0759, 0763, 0767, 0769, 0773, 0779, 0783, 0785, 0788-0790, 0794,0798, 0800, 0804, 0813, 0817, 0821, 0825, 0829, 0831, 0833, 0837, 0840, 0843, 0845, 0847, 0850, 0853, 0858,0860, 0862, 0867, 0869, 0871, 0873, 0875, 0880, 0882, 0885, 0889-0890, 0893, 0896, 0898, 0904, 0906, 0910,0913, 0917, 0922, 0924, 0929, 0931, 0933, 0938, 0944, 0946, 0948-0949, 0952, 0965, 0972, 0976, 0979-0980, 0985,0989, 0997-0998, 1000, 1002, 1010, 1016, 1018-1020, 1022, 1025, 1029, 1031, 1033-1034, 1036, 1038, 1040, 1043,1046, 1048-1049, 1051, 1053, 1055-1056, 1058, 1062, 1064, 1066, 1068-1069, 1071, 1073-1074, 1077-1078, 1082,1084, 1086, 1088-1092, 1095-1098, 1100, 1102-1103, 1106-1107, 1109, 1111, 1113, 1115-1116, 1118, 1120, 1122, 1124,1126-1127, 1129, 1131, 1135-1136, 1139-1140, 1142, 1145, 1147, 1149, 1151, 1154-1155, 1157, 1159-1160, 1164-1165,1167, 1169-1170, 1172, 1176, 1178, 1180, 1182, 1184, 1190-1191, 1193, 1197, 1201, 1203, 1205, 1209, 1211-1212,1216, 1222-1223, 1225, 1228, 1230, 1232, 1236, 1239, 1243, 1245, 1247, 1249, 1252, 1254, 1256, 1258, 1261, 1263,1265, 1267, 1269, 1271, 1275, 1277-1279, 1281, 1283, 1285, 1287, 1289, 1291, 1295, 1297, 1301, 1303, 1305, 1309,1311, 1313, 1315, 1317, 1319, 1321, 1323-1326, 1328-1329, 1331, 1335-1336, 1338, 1340, 1342, 1344, 1346, 1348,1350, 1352, 1354, 1358, 1360, 1362, 1364, 1369, 1371, 1373-1375, 1377-1378, 1380, 1382, 1384, 1386, 1388-1389,1391-1393, 1395, 1397, 1401, 1404, 1406, 1410, 1414-1415, 1420, 1423, 1426, 1429, 1434, 1440, 1444-1445, 1449,1453, 1456, 1460, 1463, 1466, 1468, 1471, 1474, 1477, 1479, 1483, 1485, 1488, 1490, 1494, 1498, 1501, 1505, 1507,1510, 1513, 1515, 1520, 1522, 1524, 1527, 1529, 1534, 1537, 1541, 1543, 1545, 1547, 1549, 1551-1552, 1556, 1558,1560, 1562-1563, 1565, 1567, 1569-1570, 1573-1577, 1579, 1581-1583, 1585, 1589-1590, 1592, 1594, 1598-1601,1603-1604, 1606, 1608, 1612, 1616, 1618, 1622, 1625, 1627, 1630, 1634, 1640, 1643, 1645, 1647, 1649, 1653-1654,1656, 1659-1660, 1662, 1664, 1668, 1671, 1673, 1677, 1679, 1683-1685, 1688, 1693, 1698-1699, 1703, 1706, 1709,1714, 1718, 1722, 1727, 1729, 1731, 1733, 1737-1738, 1740, 1742-1743, 1745-1746, 1750, 1752-1753, 1756, 1758-1759,1761, 1765-1766, 1768, 1770, 1774, 1778-1779, 1781, 1786, 1790-1791, 1795-1796, 1800-1801, 1803, 1805, 1808,1810, 1815, 1819-1820, 1824, 1826, 1828, 1831, 1833, 1837, 1839, 1841, 1844, 1846, 1851, 1853, 1855, 1863, 1866,1870, 1872, 1875-1876, 1880, 1882, 1884, 1886, 1890, 1893, 1897, 1901, 1908, 1912, 1916, 1923, 1925, 1934, 1936,1938-1939, 1943, 1947, 1952, 1955, 1959, 1962-1963, 1971, 1976, 1980, 1982, 1986, 1990-1991, 1997, 1999-2000,2002, 2004, 2007-2008, 2010, 2012-2013, 2015, 2017, 2019, 2023, 2026, 2028, 2030, 2032-2033, 2035, 2037, 2039,2043, 2047, 2050-2053, 2057, 2059, 2062, 2066, 2069, 2071-2072, 2074, 2078, 2081, 2083, 2086-2087, 2089, 2091,2093, 2095-2096, 2098, 2100-2101, 2103, 2109, 2113, 2119-2120, 2122, 2124, 2126-2127, 2129, 2131, 2170, 2172,2174, 2176, 2179, 2181, 2184, 2186, 2188, 2192, 2194, 2196, 2198, 2200, 2202-2203, 2205, 2209, 2213-2214, 2218,2222, 2224, 2228, 2230, 2232, 2236-2237, 2240-2241, 2243, 2245, 2249, 2251, 2253, 2258, 2260, 2262-2266,2268-2269, 2271, 2273, 2276-2277, 2279, 2281, 2283, 2285, 2287, 2289, 2293, 2295-2296, 2298, 2300, 2302, 2304,2306, 2308, 2311, 2313, 2317-2319, 2321, 2326, 2328, 2332-2333, 2335, 2339, 2341, 2344, 2346, 2348, 2350, 2353,2355, 2358, 2360, 2362, 2365, 2367, 2369-2371, 2373, 2375, 2377-2380, 2382-2383, 2385, 2387, 2389, 2392, 2394,2396, 2398, 2400, 2402, 2404, 2406, 2408, 2412, 2414, 2416, 2418, 2420-2421, 2424, 2426-2427, 2429, 2431, 2433,2435-2436, 2438, 2440, 2442, 2444, 2446, 2448, 2450, 2452, 2454, 2456, 2458, 2460, 2463-2471, 2473-2474, 2477,2481, 2483, 2485, 2487, 2490, 2492, 2494-2495, 2497, 2499-2501, 2503, 2505, 2507-2508, 2510, 2512, 2514, 2516,2518-2519, 2523, 2525, 2527-2528, 2532, 2534, 2538, 2541, 2544-2548, 2550-2552, 2554-2561, 2565, 2567-2568,2570, 2572, 2574-2575, 2578-2579, 2581-2582, 2585-2586, 2588, 2592-2593, 2595, 2597, 2601, 2603, 2605,2607, 2611, 2614-2615, 2617-2618, 2621-2622, 2624-2625, 2628-2629, 2631-2632, 2634, 2636, 2638-2639, 2641,2643-2644, 2646, 2648, 2650, 2652, 2655, 2657, 2659-2660, 2662, 2664, 2666-2667, 2669, 2672-2673, 2675, 2677,2679, 2681, 2684, 2686, 2690-2691, 2693-2694, 2697-2698, 2700, 2702, 2704, 2709, 2711, 2715-2716, 2718, 2720,2723, 2727, 2729, 2733, 2735, 2738-2739, 2742, 2744, 2746, 2748, 2750-2751, 2754, 2757, 2762-2763, 2765, 2769,




M(1) MODIFICATION Linked SB Incorp. Date Title2771, 2773-2774, 2777, 2779-2780, 2782, 2784, 2786, 2788, 2790, 2795, 2797, 2803, 2805-2806, 2811-2813, 2815,2818-2819, 2821, 2825, 2827, 2829, 2831, 2833, 2836-2837, 2839, 2841, 2843, 2845, 2847, 2849-2850, 2852, 2854,2857-2858, 2860, 2864, 2866, 2870, 2872-2873, 2876, 2878-2879, 2884, 2886-2894, 2897-2898, 2901, 2905, 2907,2910, 2913, 2918, 2921, 2923, 2925, 2929, 2931, 2935, 2938, 2940, 2942, 2946, 2948-2949, 2951, 2954-2955,2959, 2961, 2963, 2967, 2969, 2972, 2976, 2978-2979, 2981, 2983, 2985, 2997, 3001, 3003, 3007, 3009, 3011,3017, 3019-3020, 3024, 3026, 3028, 3030, 3032, 3036, 3038, 3041, 3043, 3045-3046, 3049, 3053-3054, 3057, 3059,3061-3062, 3065, 3069, 3073, 3077-3078, 3082, 3084-3085, 3088, 3090, 3092, 3094, 3096, 3100, 3102, 3104, 3108,3110, 3114, 3116, 3118, 3122, 3124, 3128, 3133-3134, 3137, 3139, 3142, 3144, 3163, 3165, 3168-3169, 3171-3172,3175-3176, 3179, 3181, 3184, 3186, 3188, 3193, 3195, 3200, 3202, 3204, 3209, 3214, 3216, 3220, 3225-3226, 3231,3238, 3243, 3245, 3248, 3250, 3252-3253, 3255, 3258, 3260, 3269, 3271, 3276, 3279, 3281, 3285, 3288, 3292,3298, 3300, 3305, 3309, 3311, 3317, 3320, 3324, 3331, 3333, 3336, 3342, 3344, 3346-3347, 3352, 3356, 3358,3363-3364, 3371, 3375, 3377, 3380, 3385, 3388, 3390, 3393, 3395, 3403, 3406-3407, 3411, 3413, 3415, 3417, 3421,3424, 3426, 3428, 3432, 3436, 3438, 3442-3443, 3445, 3447, 3450, 3452, 3454, 3463, 3466-3467, 3469, 3491, 3500,3509, 3513, 3518, 3520, 3530, 3533-3534, 3537, 3542, 3544, 3548, 3551, 3555, 3560-3561, 3564, 3569, 3571, 3578,3580, 3585-3586, 3588-3590, 3595, 3602, 3604, 3606, 3608, 3614-3615, 3617, 3620, 3632, 3634-3635, 3642, 3647,3651, 3657, 3660-3661, 3663, 3671, 3675, 3680, 3683-3687, 3689, 3691, 3694, 3700, 3702, 3704-3705, 3710, 3720,3727-3728, 3733, 3735, 3742, 3744, 3746, 3751, 3754, 3757, 3759, 3763, 3768, 3770, 3772, 3774, 3779, 3788, 3790,3794, 3799, 3801, 3803, 3808, 3810, 3822, 3824, 3828, 3832, 3838-3839, 3841, 3844-3845, 3849, 3851, 3860, 3874,3888, 3890, 3892, 3903, 2706, 2801, 3638, 3818, 3826, 3834, 3836, 3853-3854, 3856, 3865, 3872, 3876, 3886, 3895,3897, 3901, 3905, 3911, 3918, 3932, 3950, 3962, 3970, 3983

ER P2316 22-1015 14 08 JUL 08 AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTIONApplicable to: MSN 0002-0021, 0031-0034, 0039-0042, 0044-0051, 0056-0058, 0061-0063, 0066-0067, 0069-0072,0074-0083, 0085-0090, 0093-0097, 0100-0112, 0115-0118, 0120-0121, 0125, 0128-0139, 0143-0148, 0151-0153,0155-0156, 0158, 0160-0173, 0176-0179, 0181-0182, 0184-0204, 0206-0209, 0211-0220, 0223-0228, 0230, 0234-0241,0243-0247, 0249-0251, 0257-0258, 0262-0264, 0266-0274, 0278, 0280-0282, 0285-0289, 0291-0293, 0297-0298,0300, 0303-0304, 0306-0308, 0312-0315, 0317-0319, 0322-0323, 0325-0329, 0331-0332, 0334-0340, 0343-0347,0351-0352, 0354-0358, 0360, 0364-0367, 0372-0375, 0377, 0380-0383, 0385, 0387-0388, 0393-0396, 0399-0401,0406-0425, 0427-0510, 0512-3996

P3060 08 JUL 08 POWER PLANT - GENERAL - A321 - CFM 56-5B 1/2(30KBLS) - INSTALL ENGINE WITH DOUBLE ANNULARCOMBUSTOR

Applicable to: MSN 0517, 0519-0520, 0522, 0535, 0541, 0552, 0570, 0581, 0642, 0827, 0891, 0987, 1144E P3341 32-1136 02

32-1263 1108 JUL 08 LANDING GEAR - WHEELS AND BRAKES - INSTALL

MESSIER GOODRICH WHEELS AND BRAKES ON A321Applicable to: MSN 0364, 0385, 0412, 0458, 0468, 0473-0474, 0484, 0493, 0498, 0502, 0505, 0509, 0518-0522,0529, 0538, 0541, 0544, 0550, 0555, 0557, 0560, 0563-0564, 0567, 0591, 0595, 0597, 0604, 0606, 0614, 0620,0631-0633, 0652, 0663-0664, 0666, 0668, 0674-0675, 0677, 0680, 0684, 0687, 0692, 0699, 0715, 0725, 0731, 0746,0761, 0771, 0775, 0777, 0781, 0787, 0792, 0796, 0802, 0808, 0811, 0815, 0823, 0841, 0852, 0855, 0864, 0878, 0887,0901, 0908, 0915, 0926, 0954, 0956, 0963, 0970, 0983, 0987, 0991, 0993, 0995, 1004, 1006, 1008, 1012, 1015, 1017,1021, 1023-1024, 1027, 1042, 1045, 1060, 1080, 1094, 1133, 1144, 1153, 1161, 1188, 1195, 1199, 1202, 1204, 1207,1214, 1218-1219, 1227, 1233, 1238, 1250, 1260, 1273, 1276, 1293, 1299, 1307, 1333, 1366, 1399, 1403, 1408, 1412,1417, 1421, 1425, 1428, 1431, 1433, 1436, 1438, 1442, 1447, 1451, 1455, 1462, 1465, 1472, 1476, 1481, 1487, 1492,1496, 1499, 1503, 1517, 1519, 1521, 1525, 1531, 1536, 1539, 1554, 1572, 1587, 1596, 1602, 1607, 1611, 1614, 1619,1623, 1629, 1632, 1638, 1642, 1651, 1658, 1666, 1675, 1681, 1690-1691, 1695, 1701, 1704, 1707, 1711, 1713, 1716,1720, 1724, 1726, 1748, 1763, 1772, 1776, 1783, 1788, 1794, 1798, 1807, 1811, 1817, 1836, 1843, 1848, 1859, 1869,




M(1) MODIFICATION Linked SB Incorp. Date Title1878, 1881, 1887, 1905, 1921, 1928, 1932, 1941, 1946, 1950, 1953, 1956, 1960, 1966-1967, 1970, 1972, 1974, 1977,1984, 1988, 1994-1995, 2005, 2021, 2055, 2060, 2064, 2067, 2076, 2080, 2105, 2107, 2117, 2190, 2211, 2216, 2220,2234, 2255, 2261, 2267, 2270, 2303, 2305, 2309, 2315, 2320, 2323-2324, 2330, 2337, 2342, 2351, 2357, 2363, 2381,2410, 2462, 2476, 2480, 2521, 2530, 2536, 2543, 2549, 2553, 2590, 2599, 2610, 2653, 2682, 2687, 2707, 2713, 2726,2730, 2736, 2741, 2756, 2759, 2767, 2793, 2799, 2809, 2823, 2862, 2868, 2882, 2895, 2903, 2912, 2916, 2919,2927, 2933, 2936, 2957, 2965, 2971, 2974, 2996, 2999, 3005, 3013, 3015, 3022, 3034, 3051, 3067, 3070, 3075, 3081,3098, 3106, 3112, 3120, 3126, 3130, 3146, 3191, 3198, 3207, 3212, 3217, 3222, 3229, 3233, 3235, 3241, 3247, 3249,3251, 3254, 3262, 3265, 3267, 3274, 3283, 3290, 3294, 3302, 3307, 3315, 3322, 3326, 3329, 3334, 3339-3340, 3350,3355, 3360, 3367, 3369, 3372, 3382, 3387, 3397, 3399, 3401, 3405, 3419, 3429, 3434, 3441, 3458-3459, 3462, 3471,3493, 3498, 3504, 3507, 3512, 3522-3523, 3525, 3527, 3539, 3546, 3552, 3557, 3566, 3573, 3575, 3583-3584, 3587,3592-3593, 3600, 3612, 3619, 3623, 3625, 3629, 3633, 3636-3637, 3639, 3645, 3653, 3655, 3665, 3669, 3673, 3678,3681-3682, 3688, 3708, 3712, 3717, 3722, 3725, 3730, 3737-3738, 3740, 3749, 3752, 3761, 3764, 3766, 3784, 3792,3796, 3806, 3814, 3816, 3820, 3847, 3858, 3862, 3867, 3878-3879, 3920, 3830, 3864, 3869, 3881, 3884, 3893, 3899,3916, 3924, 3926, 3928-3930, 3934, 3936, 3938, 3940, 3944, 3948, 3951, 3955, 3960, 3964, 3966, 3969, 3977-3981,3989-3993, 3996

P3345 34-1119 02 08 JUL 08 NAVIGATION - SATELLITE NAVIGATION - INSTALL DUALLITTON GPS

Applicable to: MSN 0364, 0385, 0412, 0458, 0468, 0473-0474, 0484, 0493, 0502, 0505, 0518, 0550, 0557, 0560,0563-0565, 0567, 0573, 0575, 0580, 0582, 0591, 0595, 0597, 0604, 0609-0610, 0614, 0616, 0620, 0623, 0627,0631-0633, 0636, 0641, 0646, 0651-0654, 0657, 0659, 0661, 0663, 0666-0668, 0674-0675, 0679, 0684, 0689, 0692,0694, 0696, 0698-0700, 0704-0706, 0709-0710, 0712, 0717-0718, 0720, 0722-0723, 0729, 0738, 0744-0745, 0761,0775, 0794, 0805, 0808, 0823, 0853, 0860, 0875, 0887, 0901, 0908, 1016

E P3379 08 JUL 08 INDICATING/RECORDING SYSTEMS - GENERAL-DEFINE CPIP3

Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0483-3996P3437 08 JUL 08 AUTO FLIGHT - A320 - INHIBIT ENERGY MANAGEMENT

FUNCTIONS FOR IAE AND CFM ENGINESApplicable to: MSN 0501, 0507, 0511, 0531, 0534, 0549, 0554, 0658, 0669, 0685

P3476 08 JUL 08 INDICATING/RECORDING SYSTEMS - GENERAL -DEFINE PIN PROGRAMMING FOR UA1 VERSION

Applicable to: MSN 0463-0465, 0470, 0472, 0475, 0479E P3511 22-1022 03 08 JUL 08 AUTO FLIGHT - FAC - INSTALL TWO FACS P/N BAM

0509Applicable to: MSN 0002-0010, 0014, 0019-0029, 0039, 0042, 0052-0055, 0061-0067, 0069-0072, 0076-0078,0081-0083, 0085-0088, 0091-0094, 0098-0104, 0109-0111, 0115-0117, 0119-0120, 0123-0124, 0128-0129, 0131-0137,0140, 0142-0143, 0146-0147, 0157-0158, 0161-0162, 0168-0169, 0172-0177, 0179, 0181-0182, 0186-0189, 0193,0195, 0199-0203, 0205, 0207, 0209-0210, 0216-0218, 0220, 0223-0229, 0231-0232, 0240-0241, 0246, 0258,0264, 0266-0269, 0274, 0279, 0283-0289, 0302-0305, 0308-0309, 0312, 0314-0315, 0317, 0322-0323, 0326, 0331,0343-0344, 0346, 0348, 0354, 0356-0357, 0362-0364, 0370, 0376, 0382, 0385-0386, 0390, 0393-0394, 0401-0404,0411-0412, 0415, 0422, 0425, 0430, 0434-0437, 0439, 0442-0443, 0446-0450, 0452, 0454-0457, 0460-0465,0470-0472, 0475, 0477, 0479-0480, 0483-3996

E P3560 22-1059 01 08 JUL 08 AUTO FLIGHT - FMGC - PROVIDE TIME CONSTRAINTAND TEN CHARACTERS RTE IDENT FUNCTIONS

Applicable to: MSN 0087-0088, 0565, 0569, 0575, 0580, 0624, 0626, 0628, 0630, 0659, 0661, 0667, 0677, 0680,0686-0687, 0690, 0696, 0698, 0704-0706, 0709-0710, 0712, 0715, 0718, 0720, 0722, 0725, 0745, 0748, 0759, 0771,




M(1) MODIFICATION Linked SB Incorp. Date Title0781, 0783, 0787-0788, 0792, 0798, 0804, 0806, 0810, 0825, 0835, 0843-0844, 0847, 0849-0850, 0852, 0855,0858-0859, 0861-0864, 0867-0868, 0871, 0873, 0881-0882, 0885, 0890, 0893, 0895-0896, 0898, 0900, 0904, 0908,0910, 0913, 0922, 0929, 0934, 0936, 0941-0942, 0944, 0946-0950, 0952, 0954, 0961, 0965-0966, 0968, 0970,0972, 0974, 0976, 0980, 0989-0990, 0995, 0997, 1002, 1004, 1006, 1010, 1012, 1014, 1017, 1019, 1022, 1026, 1028,1030-1031, 1033, 1035, 1038-1040, 1044-1046, 1048, 1051-1055, 1057, 1060-1061, 1065-1066, 1068-1070, 1073,1077, 1080-1082, 1084, 1086, 1089, 1092, 1094-1097, 1102-1105, 1107, 1109, 1112-1115, 1118, 1121-1125, 1128, 1130,1132-3996

P3605 08 JUL 08 POWER PLANT - GENERAL - A320 - CFM 56-5B -4/2 (26.5 KLBS) - INSTALL ENGINE WITH DOUBLEANNULAR COMBUSTOR

Applicable to: MSN 0533, 0545, 0548, 0553, 0559, 0562, 0566, 0574, 0577, 0585, 0596, 0603, 0635, 0643, 0681,0701, 0703, 0768, 0776, 0782, 0797, 0870, 0942, 0947, 1026, 1054, 1081, 1125, 1132, 1137, 1150, 1162, 1179, 1189,1244, 1259, 1308, 1322, 1370, 1387, 1405, 1413, 1439, 1450, 1470, 1478, 1544, 1588, 1678, 1712, 1735, 1913, 1989,2065, 2146, 2154

E P3686 22-1038 04 08 JUL 08 AUTO FLIGHT-FAC-INTRODUCE FAC P/N BAM 510Applicable to: MSN 0002-0010, 0014, 0019-0029, 0039, 0042, 0052-0055, 0061-0067, 0069-0072, 0076-0078,0081-0083, 0085-0088, 0091-0094, 0098-0104, 0109-0112, 0116-0117, 0119-0120, 0123-0124, 0128-0129, 0131-0137,0140, 0142-0143, 0146-0147, 0157-0158, 0161-0166, 0168-0169, 0172-0179, 0181-0182, 0186-0189, 0193-0195,0198-0203, 0205, 0207, 0209-0210, 0216-0218, 0220, 0223-0229, 0231-0232, 0235, 0240-0241, 0246, 0258, 0264,0266-0269, 0274, 0279, 0283-0289, 0299, 0302-0305, 0308-0309, 0312, 0314-0315, 0317, 0322-0323, 0326, 0331,0343-0344, 0346, 0348-0349, 0351, 0354, 0356-0357, 0362-0364, 0366, 0370-0371, 0376, 0382, 0385-0386,0390-0391, 0393-0394, 0401-0404, 0411-0412, 0415, 0422, 0425, 0427, 0430, 0434-0437, 0439, 0442-0443,0446-0450, 0452, 0454-0458, 0460-0465, 0468, 0470-0475, 0477, 0479-0480, 0483-0500, 0502-3996

E P3924 32-1162 22 08 JUL 08 LANDING GEAR - MLG - MESSIER - INTRODUCEBRAKES P/N C202253

Applicable to: MSN 0002-0029, 0033, 0035-0039, 0042, 0044, 0061-0063, 0069-0072, 0078, 0083, 0085-0088,0093-0094, 0100-0111, 0115-0117, 0119-0120, 0123-0124, 0128-0140, 0142-0148, 0151, 0155-0158, 0161-0170,0172-0182, 0184, 0186-0190, 0193-0196, 0198-0205, 0207, 0209-0212, 0214-0224, 0226-0232, 0235-0241, 0244-0247,0256-0258, 0264, 0266-0270, 0274, 0278, 0283-0289, 0294-0295, 0299-0303, 0305, 0309, 0312-0313, 0316,0322-0323, 0325-0326, 0328, 0331-0332, 0337-0338, 0343-0349, 0351-0352, 0356, 0361-0363, 0365-0366,0369-0371, 0375, 0377, 0382-0383, 0390, 0401-0407, 0409, 0413-0415, 0419-0421, 0424, 0427-0430, 0436-0438,0441, 0444-0445, 0449, 0459, 0466, 0476, 0478, 0482, 0491, 0496-0497, 0501, 0507, 0511, 0525, 0531, 0533-0534,0537, 0540, 0542-0543, 0545, 0548-0549, 0551, 0553-0554, 0556, 0559, 0562, 0566, 0569, 0574, 0577-0579,0585, 0588, 0590, 0594, 0596, 0598, 0600-0603, 0605, 0607-0612, 0615-0619, 0621-0623, 0625, 0627, 0629,0635-0637, 0641, 0643-0648, 0650-0651, 0653-0654, 0657-0658, 0660, 0662, 0665, 0669, 0671, 0673, 0679,0681, 0685, 0689, 0694, 0696, 0698, 0700-0701, 0703-0706, 0709-0710, 0712-0713, 0717-0718, 0720, 0722-0723,0726-0727, 0729, 0734, 0738, 0744-0745, 0750, 0754-0755, 0758, 0760, 0763, 0767-0768, 0772, 0774, 0776, 0782,0790-0791, 0793-0795, 0797, 0809, 0814, 0821-0822, 0833, 0837-0838, 0849, 0853-0854, 0859-0860, 0869-0870,0872, 0875-0876, 0880-0881, 0883-0884, 0886, 0894-0895, 0897, 0899-0900, 0905-0906, 0909-0910, 0913-0914,0917-0919, 0921, 0925, 0927-0928, 0932-0933, 0937-0939, 0942-0943, 0945, 0947, 0950, 0957-0958, 0960,0966-0967, 0969, 0971, 0973, 0975, 0977, 0979, 0982, 0984-0986, 0992, 0994, 0998, 1000, 1002, 1005, 1009, 1013,1016, 1018, 1020, 1025-1026, 1028-1030, 1032, 1034-1036, 1039, 1041, 1047-1048, 1053-1054, 1057, 1059, 1063,1067-1068, 1070, 1072-1074, 1076, 1081-1082, 1085-1087, 1093, 1098-1102, 1106-1108, 1115, 1117-1121, 1123-1125,1127, 1132, 1137, 1142, 1145, 1150-1152, 1154, 1156-1157, 1160, 1162, 1165, 1169, 1172-1173, 1175-1176, 1179-1181,1184, 1187, 1189-1190, 1193, 1196-1198, 1200-1201, 1206, 1208, 1212, 1215-1216, 1221-1222, 1225, 1228-1229,




M(1) MODIFICATION Linked SB Incorp. Date Title1231-1232, 1235-1237, 1239-1240, 1244, 1247, 1252, 1255-1259, 1261-1262, 1267, 1270-1271, 1279-1280, 1283,1285, 1288, 1292, 1295-1296, 1302-1303, 1305, 1308-1309, 1312, 1316, 1318, 1322, 1327, 1329-1330, 1335-1338,1344-1345, 1347, 1349, 1352, 1357, 1361-1362, 1364-1365, 1367, 1370, 1372, 1377, 1379-1381, 1384-1388, 1396,1398, 1402, 1404-1405, 1411, 1413, 1415-1416, 1422-1423, 1429-1430, 1437, 1439-1441, 1444-1446, 1448-1450,1452, 1454, 1457, 1461, 1464, 1466, 1468, 1470-1471, 1473, 1478-1480, 1484-1485, 1489, 1493-1494, 1497, 1502,1504-1506, 1510, 1513, 1516, 1524, 1528-1530, 1532, 1537, 1540-1542, 1544, 1546, 1550-1551, 1553, 1556-1558,1561, 1566, 1574, 1578, 1588-1592, 1594, 1597-1599, 1601, 1603-1604, 1606, 1610, 1612, 1616, 1622, 1625, 1631,1639-1640, 1645, 1648, 1650, 1652, 1654-1657, 1661, 1663, 1665, 1667, 1672, 1674, 1677-1679, 1682, 1686-1687,1689, 1692, 1694, 1696, 1698-1700, 1705-1706, 1708, 1712, 1715, 1717, 1722-1723, 1727, 1729, 1733, 1735-1736,1739-1740, 1744-1745, 1749-1750, 1753-1754, 1757, 1760, 1762, 1767-1771, 1773, 1775, 1778-1780, 1782, 1784-1787,1791, 1793, 1795, 1797, 1799, 1801-1802, 1804, 1806, 1808-1809, 1814, 1816, 1818, 1823, 1825-1827, 1829-1832,1835, 1837-1838, 1846, 1849, 1852, 1855-1857, 1861-1862, 1868, 1871, 1873, 1879-1880, 1883-1885, 1888-1889,1891, 1894-1896, 1898-1901, 1904, 1906-1911, 1913-1920, 1924, 1927, 1931, 1933, 1936-1938, 1942, 1944-1945,1947-1949, 1951, 1954-1955, 1957-1958, 1961, 1964-1965, 1969, 1973, 1975, 1979, 1981, 1983, 1989, 1993, 1996,1998-2001, 2003, 2006-2007, 2009, 2011, 2014-2016, 2020, 2022-2024, 2027, 2031-2036, 2038, 2040, 2042, 2044,2046, 2049, 2054, 2056-2059, 2061, 2063, 2065, 2068, 2070-2071, 2073-2075, 2079, 2081, 2083, 2085-2086, 2088,2090, 2094, 2097-2101, 2104, 2108-2109, 2112-2114, 2121-2125, 2127-2128, 2130-2132, 2134-2143, 2146-2150,2152-2162, 2164-2168, 2171-2174, 2177-2178, 2182-2183, 2186, 2188-2189, 2192, 2194-2195, 2199-2205, 2207,2210, 2212-2213, 2215, 2219, 2221, 2223, 2225, 2227-2228, 2231-2232, 2235, 2237, 2239, 2242, 2244, 2246,2248, 2252, 2254, 2257, 2259, 2262-2264, 2266, 2269, 2273-2275, 2278-2280, 2284-2286, 2288, 2291, 2293,2297-2298, 2306-2307, 2310-2311, 2313-2314, 2317, 2331-2332, 2334, 2336, 2340-2341, 2343-2350, 2352, 2354,2361, 2365-2366, 2368, 2371, 2376, 2382, 2384, 2386, 2388-2391, 2397, 2403, 2407-2408, 2413, 2415-2417,2419, 2421, 2424-2426, 2429, 2433, 2435, 2437, 2439-2440, 2443, 2445, 2447, 2449, 2451, 2454, 2456, 2459,2461, 2466, 2470, 2473, 2478-2479, 2484-2485, 2489-2491, 2493-2494, 2496, 2498-2499, 2502, 2504-2511, 2513,2517, 2519-2520, 2522, 2524-2525, 2529, 2531-2535, 2539-2541, 2545-2547, 2550-2551, 2554-2555, 2557-2562,2564, 2566-2569, 2571, 2574, 2576-2577, 2579-2582, 2584, 2589, 2591-2594, 2596-2598, 2601-2603, 2606-2607,2609, 2611-2612, 2614, 2616-2617, 2619-2624, 2626-2629, 2631-2634, 2637, 2639-2640, 2643-2645, 2647-2650,2652, 2654-2656, 2658-2661, 2663-2665, 2667-2668, 2670-2676, 2678-2680, 2683-2686, 2688-2689, 2692-2699,2701, 2704-2706, 2708, 2710-2712, 2714, 2716, 2718-2725, 2728, 2731-2734, 2737-2740, 2743, 2745-2750,2752-2753, 2755, 2757-2758, 2760-2762, 2764, 2768, 2770, 2772-2776, 2778, 2781, 2783-2785, 2789, 2792,2794, 2796-2798, 2800-2802, 2804-2805, 2807-2808, 2811, 2814-2817, 2819-2820, 2822, 2824-2826, 2828, 2830,2832, 2834-2835, 2853, 2855-2856, 2858-2859, 2861, 2863-2865, 2867, 2869-2872, 2874, 2877-2881, 2883,2885-2894, 2896-2902, 2904-2911, 2913-2915, 2918, 2921-2922, 2924-2926, 2928-2932, 2934-2935, 2937-2945,2948-2956, 2958, 2960-2964, 2966-2970, 2972-2973, 2975, 2977-2978, 2980-2986, 2988-2993, 2995, 2998,3000-3002, 3004, 3006-3010, 3012, 3014, 3016-3021, 3023-3027, 3029-3033, 3035, 3037, 3039-3040, 3043-3044,3046-3047, 3049-3050, 3054-3056, 3058, 3060, 3062, 3064-3066, 3068, 3071-3074, 3076, 3078-3080, 3083,3085-3087, 3089, 3091, 3093-3097, 3099-3102, 3104-3105, 3107-3109, 3111, 3114-3117, 3119, 3121, 3124-3125, 3127,3131-3133, 3135, 3138-3145, 3147-3156, 3158-3162, 3164-3171, 3173-3174, 3177-3183, 3185-3190, 3192, 3194-3197,3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228, 3230-3232, 3234, 3236-3240, 3242-3246, 3250, 3252,3255-3261, 3263-3264, 3266, 3268-3271, 3273, 3275, 3277-3278, 3280, 3282, 3284-3289, 3291-3293, 3295-3296,3299-3301, 3303, 3305-3306, 3308-3314, 3316-3317, 3319-3321, 3323-3325, 3327-3328, 3330-3333, 3335,3337-3338, 3341-3344, 3346-3349, 3351, 3353-3354, 3356-3357, 3359, 3361-3366, 3368, 3370-3371, 3376-3377,3379-3381, 3383-3386, 3388, 3390-3396, 3398, 3400, 3402-3404, 3406-3407, 3409, 3412, 3414-3417, 3420-3425,3427-3428, 3430, 3435-3440, 3443-3449, 3451-3457, 3460-3461, 3464-3465, 3468-3470, 3473, 3475-3486,3488-3490, 3492, 3494, 3496-3497, 3499, 3502-3503, 3505-3506, 3508-3509, 3513-3517, 3519-3521, 3524, 3526,3528-3533, 3535-3536, 3540-3543, 3548-3551, 3553-3554, 3556, 3558-3565, 3567-3568, 3570, 3572, 3576,




M(1) MODIFICATION Linked SB Incorp. Date Title3578-3580, 3582, 3585-3586, 3588-3589, 3594-3599, 3601-3607, 3609-3611, 3613-3618, 3620-3622, 3626, 3628,3630, 3632, 3635, 3641-3643, 3648-3652, 3654, 3656-3663, 3666-3667, 3670-3671, 3674, 3676-3677, 3679-3680,3684-3687, 3689-3690, 3692-3698, 3700-3701, 3703-3704, 3706-3707, 3709-3710, 3713-3716, 3718-3719, 3721,3723-3724, 3726-3729, 3731-3734, 3736, 3739, 3741, 3744-3745, 3747-3748, 3750-3751, 3753, 3755-3760, 3765,3768-3773, 3779-3782, 3785, 3787, 3791, 3793, 3795, 3800-3804, 3807, 3809, 3811-3813, 3815, 3817-3819,3863, 3937, 2837-2851, 3591, 3638, 3775-3777, 3797-3798, 3821-3822, 3825-3829, 3831-3834, 3836-3837, 3840,3846, 3848-3853, 3855-3856, 3859-3861, 3865-3866, 3868, 3872-3877, 3880, 3882-3883, 3885-3887, 3889-3892,3894-3898, 3900-3904, 3906-3908, 3910-3912, 3915, 3918-3919, 3921, 3925, 3927, 3931-3933, 3935, 3939,3941-3943, 3945, 3947, 3949-3950, 3952, 3956-3959, 3962, 3965, 3967-3968, 3970-3972, 3983-3984, 3995

P4085 34-1132 02 08 JUL 08 NAVIGATION-PRIMARY MEANS USING HONEYWELLGPS (HYBRID ARCHITETURE) PROVIDING RAIMFUNCTION (CL)

Applicable to: MSN 0087-0088, 0434, 0477, 0488, 0494-0495, 0513-0517, 0519-0520, 0522, 0524, 0526, 0532-0533,0535, 0541, 0545, 0548, 0553, 0559, 0562, 0566, 0569, 0574, 0576-0578, 0583, 0585-0586, 0588, 0593, 0596, 0599,0603, 0612, 0621, 0629, 0635, 0642-0643, 0664, 0673, 0680-0681, 0687, 0701, 0703, 0713, 0715, 0725, 0727, 0734,0765, 0782, 0819, 0827, 0848, 0870, 0891, 0940, 0951, 0959, 0987, 0999, 1018, 1138, 1144, 1168, 1217, 1220, 1226

E P4089 22-1057 04 08 JUL 08 AUTO FLIGHT-FMGC-REDUCE VAPP FOR A320 CFM/IAE

Applicable to: MSN 0069-0072, 0078, 0083, 0086, 0093-0094, 0104, 0110-0111, 0116-0117, 0135, 0137, 0147,0161-0162, 0172, 0200-0202, 0209, 0216-0218, 0267-0269, 0346, 0382, 0401, 0533, 0545, 0548, 0553, 0559, 0562,0566, 0574, 0577, 0585, 0596, 0603, 0635, 0643, 0673, 0681, 0701, 0703, 0756, 0768, 0774, 0776, 0782, 0784,0793, 0797, 0809, 0812, 0816, 0844, 0861, 0863, 0868, 0870, 0877, 0884, 0894, 0905, 0930, 0934, 0936, 0942,0945, 0947, 0951, 0957, 0960, 0971, 0982, 0999, 1014, 1026, 1028, 1030, 1032, 1035, 1037, 1039, 1041, 1044, 1047,1050, 1052, 1054, 1057, 1059, 1061, 1063, 1065, 1067, 1070, 1072, 1075-1076, 1079, 1081, 1083, 1085, 1087, 1093,1099, 1101, 1104-1105, 1108, 1110, 1112, 1114, 1117, 1119, 1121, 1123, 1125, 1128, 1130, 1132, 1134, 1137-1138, 1141,1143, 1146, 1148, 1150, 1152, 1156, 1158, 1162-1163, 1166, 1168, 1171, 1173, 1175, 1177, 1179, 1181, 1183, 1187,1189, 1192, 1194, 1196, 1198, 1200, 1206, 1208, 1210, 1213, 1215, 1217, 1221, 1224, 1226, 1229, 1231, 1234-1235,1237, 1240, 1242, 1244, 1246, 1248, 1251, 1253, 1255, 1257, 1259, 1262, 1264, 1266, 1268, 1270, 1272, 1274, 1280,1282, 1284, 1286, 1288, 1290, 1292, 1294, 1296, 1298, 1300, 1302, 1304, 1306, 1308, 1310, 1312, 1314, 1316, 1318,1320, 1322, 1327, 1330, 1332, 1334, 1337, 1339, 1341, 1343, 1345, 1347, 1349, 1351, 1353, 1355, 1357, 1359, 1361,1363, 1365, 1367-1368, 1370, 1372, 1376, 1379, 1381, 1383, 1385, 1387, 1390, 1394, 1396, 1398, 1400, 1402, 1405,1407, 1409, 1411, 1413, 1416, 1418-1419, 1422, 1424, 1427, 1430, 1432, 1435, 1437, 1439, 1441, 1443, 1446, 1448,1450, 1452, 1454, 1457, 1459, 1461, 1464, 1467, 1469-1470, 1473, 1475, 1478, 1480, 1482, 1484, 1486, 1489, 1491,1493, 1495, 1497, 1500, 1502, 1504, 1506, 1508-1509, 1512, 1514, 1516, 1518, 1523, 1526, 1528, 1530, 1532-1533,1535, 1538, 1540, 1542, 1544, 1546, 1548, 1550, 1553, 1555, 1557, 1559, 1561, 1564, 1566, 1568, 1571, 1578, 1580,1584, 1586, 1588, 1591, 1593, 1595, 1597, 1605, 1609-1610, 1613, 1615, 1617, 1620-1621, 1624, 1626, 1628, 1631,1633, 1635, 1637, 1639, 1641, 1644, 1646, 1648, 1650, 1652, 1655, 1657, 1661, 1663, 1665, 1667, 1669, 1672, 1674,1676, 1678, 1680, 1682, 1686-1687, 1689, 1692, 1694, 1696-1697, 1700, 1702, 1705, 1708, 1710, 1712, 1715, 1717,1719, 1721, 1723, 1725, 1728, 1730, 1732, 1735-1736, 1739, 1741, 1744, 1747, 1749, 1751, 1754-1755, 1757, 1760,1762, 1764, 1767, 1769, 1771, 1773, 1775, 1777, 1780, 1782, 1784-1785, 1787, 1789, 1792-1793, 1797, 1799, 1802,1804, 1806, 1809, 1812-1814, 1816, 1818, 1821-1823, 1825, 1827, 1829, 1832, 1834-1835, 1838, 1840, 1842, 1845,1847, 1849, 1852, 1854, 1856-1858, 1860-1862, 1864-1865, 1867-1868, 1871, 1873-1874, 1877, 1879, 1883, 1885,1888-1889, 1891-1892, 1894-1896, 1898-1900, 1902-1904, 1906-1907, 1909-1911, 1913-1915, 1917-1920, 1922, 1924,1927, 1929-1931, 1933, 1935, 1937, 1940, 1942, 1944-1945, 1948-1949, 1951, 1954, 1957-1958, 1961, 1964-1965,1968-1969, 1973, 1975, 1979, 1981, 1983, 1987, 1989, 1993, 1996, 1998, 2001, 2003, 2006, 2009, 2011, 2014, 2016,




M(1) MODIFICATION Linked SB Incorp. Date Title2018, 2020, 2022, 2024, 2027, 2029, 2031, 2034, 2036, 2038, 2040, 2042, 2044, 2046, 2048-2049, 2054, 2056,2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2077, 2079, 2082, 2084-2085, 2088, 2090, 2092, 2094, 2097,2099, 2102, 2104, 2106, 2108, 2112, 2114, 2116, 2118, 2121, 2123, 2125, 2128, 2130, 2132-2169, 2171, 2173, 2175,2177-2178, 2180, 2182-2183, 2185, 2187, 2189, 2191, 2193, 2195, 2197, 2199, 2201, 2204, 2206-2207, 2210, 2212,2215, 2217, 2219, 2221, 2223, 2225, 2227, 2229, 2231, 2233, 2235, 2238-2239, 2242, 2244, 2246, 2248, 2250, 2252,2254, 2256-2257, 2259, 2272, 2274-2275, 2278, 2280, 2282, 2284, 2286, 2288, 2291-2292, 2294, 2297, 2299, 2301,2307, 2310, 2312, 2314, 2316, 2322, 2325, 2327, 2329, 2331, 2334, 2336, 2338, 2340, 2343, 2345, 2347, 2349, 2352,2354, 2356, 2359, 2361, 2364, 2366, 2368, 2372, 2374, 2376, 2384, 2386, 2388, 2390-2391, 2393, 2395, 2397,2399, 2401, 2403, 2405, 2407, 2409, 2411, 2413, 2415, 2417, 2419, 2422-2423, 2425, 2428, 2430, 2432, 2434, 2437,2439, 2441, 2443, 2445, 2447, 2449, 2451, 2453, 2455, 2457, 2459, 2461, 2475, 2478-2479, 2482, 2484, 2486, 2489,2491, 2493, 2496, 2498, 2502, 2504, 2506, 2509, 2511, 2513, 2515, 2517, 2520, 2522, 2524, 2526, 2529, 2531, 2533,2535, 2537, 2539-2540, 2542, 2562, 2564, 2566, 2569, 2571, 2573, 2576-2577, 2580, 2583-2584, 2587, 2589, 2591,2594, 2596, 2598, 2600, 2602, 2604, 2606, 2608-2609, 2612-2613, 2616, 2619-2620, 2623, 2626-2627, 2630, 2633,2635, 2637, 2640, 2642, 2645, 2647, 2649, 2651, 2654, 2656, 2658, 2661, 2663, 2665, 2668, 2670-2671, 2674, 2676,2678, 2680, 2683, 2685, 2688-2689, 2692, 2695-2696, 2699, 2701, 2703, 2705, 2708, 2710, 2712, 2714, 2717, 2719,2721, 2724-2725, 2728, 2731-2732, 2734, 2737, 2740, 2743, 2745, 2747, 2749, 2752-2753, 2755, 2758, 2760-2761,2764, 2766, 2768, 2770, 2772, 2775-2776, 2778, 2781, 2783, 2785, 2787, 2789, 2791-2792, 2794, 2796, 2798,2800, 2802, 2804, 2807-2808, 2810, 2814, 2816-2817, 2820, 2822, 2824, 2826, 2828, 2830, 2832, 2834-2835, 2838,2840, 2842, 2844, 2846, 2848, 2851, 2853, 2855-2856, 2859, 2861, 2863, 2865, 2867, 2869, 2871, 2874-2875, 2877,2880-2881, 2883, 2885, 2896, 2899-2900, 2902, 2904, 2906, 2908-2909, 2911, 2914-2915, 2917, 2920, 2922, 2924,2926, 2928, 2930, 2932, 2934, 2937, 2939, 2941, 2943-2945, 2947, 2950, 2952-2953, 2956, 2958, 2960, 2962, 2964,2966, 2968, 2970, 2973, 2975, 2977, 2980, 2982, 2984, 2986-2995, 2998, 3000, 3002, 3004, 3006, 3008, 3010,3012, 3014, 3016, 3018, 3021, 3023, 3025, 3027, 3029, 3031, 3033, 3035, 3037, 3039-3040, 3042, 3044, 3047-3048,3050, 3052, 3055-3056, 3058, 3060, 3063-3064, 3066, 3068, 3071-3072, 3074, 3076, 3079-3080, 3083, 3086-3087,3089, 3091, 3093, 3095, 3097, 3099, 3101, 3103, 3105, 3107, 3109, 3111, 3113, 3115, 3117, 3119, 3121, 3123, 3125,3127, 3129, 3131-3132, 3135-3136, 3138, 3140-3141, 3143, 3145, 3147-3162, 3164, 3166-3167, 3170, 3173-3174,3177-3178, 3180, 3182-3183, 3185, 3187, 3189-3190, 3192, 3194, 3196-3197, 3199, 3201, 3203, 3205-3206, 3208,3210-3211, 3213, 3215, 3218-3219, 3221, 3223-3224, 3227-3228, 3230, 3232, 3234, 3236-3237, 3239-3240, 3242,3244, 3246, 3256-3257, 3259, 3261, 3263-3264, 3266, 3268, 3270, 3272-3273, 3275, 3277-3278, 3280, 3282, 3284,3286-3287, 3289, 3291, 3293, 3295-3296, 3299, 3301, 3303-3304, 3306, 3308, 3310, 3312-3314, 3316, 3318-3319,3321, 3323, 3325, 3327-3328, 3330, 3332, 3335, 3337-3338, 3341, 3343, 3345, 3348-3349, 3351, 3353-3354, 3357,3359, 3361-3362, 3365-3366, 3368, 3370, 3373-3374, 3376, 3378-3379, 3381, 3383-3384, 3386, 3389, 3391-3392,3394, 3396, 3398, 3400, 3402, 3404, 3408-3410, 3412, 3414, 3416, 3418, 3420, 3422-3423, 3425, 3427, 3430-3431,3433, 3435, 3437, 3439-3440, 3444, 3446, 3448-3449, 3451, 3453, 3455-3457, 3460-3461, 3464-3465, 3468, 3470,3472-3490, 3492, 3494-3497, 3499, 3501-3503, 3505-3506, 3508, 3510-3511, 3514-3517, 3519, 3521, 3524, 3526,3528-3529, 3531-3532, 3535-3536, 3538, 3540-3541, 3543, 3545, 3547, 3549-3550, 3553-3554, 3556, 3558-3559,3562-3563, 3565, 3567-3568, 3570, 3572, 3574, 3576-3577, 3579, 3581-3582, 3594, 3596-3599, 3601, 3603,3605, 3607, 3609-3611, 3613, 3616, 3618, 3621-3622, 3624, 3626-3628, 3630-3631, 3640-3641, 3643-3644, 3646,3648-3650, 3652, 3654, 3656, 3658-3659, 3662, 3664, 3666-3668, 3670, 3672, 3674, 3676-3677, 3679, 3690,3692-3693, 3695-3699, 3701, 3703, 3706-3707, 3709, 3711, 3713-3716, 3718-3719, 3721, 3723-3724, 3726, 3729,3731-3732, 3734, 3736, 3739, 3741, 3743, 3745, 3747-3748, 3750, 3753, 3755-3756, 3760, 3762, 3765, 3767, 3769,3771, 3773, 3780-3783, 3785-3787, 3789, 3791, 3793, 3795, 3800, 3802, 3804-3805, 3807, 3809, 3811-3813, 3815,3817, 3823, 3829, 3835, 3843, 3850, 3863, 3871, 3875, 3891, 3904, 3937, 3591, 3758, 3775-3778, 3797-3798, 3819,3821, 3825, 3827, 3831, 3833, 3837, 3840, 3846, 3848, 3852, 3855, 3857, 3859, 3861, 3866, 3868, 3873, 3877, 3880,3882-3883, 3885, 3887, 3889, 3894, 3896, 3898, 3900, 3902, 3906-3910, 3912-3915, 3917, 3919, 3921-3923, 3925,




M(1) MODIFICATION Linked SB Incorp. Date Title3927, 3931, 3933, 3935, 3939, 3941-3943, 3945-3947, 3949, 3952-3954, 3956-3959, 3965, 3967-3968, 3971-3972,3984, 3995

ER P4319 22-1058 43 08 JUL 08 AUTO FLIGHT - FCU - DEFINE FLIGHT DIRECTORENGAGEMENT IN CROSSED BARS AT GO AROUND

Applicable to: MSN 0002-0021, 0033, 0039, 0042, 0044, 0052-0055, 0059-0068, 0073, 0076-0077, 0081-0082,0084, 0087-0088, 0091, 0098-0103, 0108-0109, 0112, 0115, 0120, 0122, 0126-0131, 0133-0134, 0136, 0138-0139,0141, 0143-0146, 0148-0151, 0154-0156, 0158-0159, 0165-0166, 0173-0178, 0181-0188, 0191, 0193-0195, 0198-0199,0203-0204, 0207, 0210-0211, 0214-0215, 0220, 0223-0224, 0226-0228, 0231-0244, 0246, 0248-0251, 0253-0255,0264-0266, 0270, 0274, 0277-0279, 0283-0287, 0289-0290, 0302-0303, 0305, 0309-0312, 0315, 0317, 0323-0325,0330, 0333-0335, 0337, 0341-0342, 0350-0352, 0356, 0359, 0366, 0375, 0377-0378, 0384, 0395, 0403-0404, 0407,0409, 0419, 0421, 0424, 0426-0427, 0429, 0434, 0438, 0440, 0445, 0448, 0453, 0455, 0459, 0466, 0471, 0477, 0480,0488, 0491, 0494-0495, 0497-0498, 0509, 0513-0517, 0519-0522, 0524, 0526-0527, 0529, 0532-0533, 0535-0538,0540-0541, 0543-0548, 0550-0553, 0555-0557, 0559, 0562, 0565-0566, 0570, 0572-0574, 0576-0578, 0581-0586,0588, 0591, 0593, 0596, 0598-0600, 0603, 0606, 0608, 0612, 0618, 0620-0621, 0625, 0629, 0631-0633, 0635, 0637,0640, 0642-0644, 0646-0647, 0653-0654, 0656-0657, 0660-0661, 0663-0664, 0668, 0670, 0672-0676, 0680-0682,0684, 0687-0688, 0691, 0693, 0695-0698, 0701, 0703-0705, 0707-0716, 0718-0722, 0725, 0727-0728, 0730-0736,0740-0742, 0746-0747, 0750, 0752, 0755-0758, 0760-0765, 0768-0771, 0773-0774, 0776-0777, 0779, 0781-0782,0784-0785, 0790-0791, 0793-0797, 0800, 0802-0803, 0805-0806, 0808-0813, 0815-0817, 0819, 0821-0823, 0827,0829, 0831, 0835, 0837, 0839-0841, 0844-0845, 0848-0849, 0855-0856, 0859, 0861, 0863-0864, 0866, 0868, 0870,0872, 0874, 0877-0879, 0881, 0884-0885, 0889-0892, 0894-0896, 0899-0900, 0902, 0904-0906, 0908, 0910, 0912,0915, 0917, 0919-0920, 0922, 0924, 0926-0938, 0940-0943, 0945-0947, 0949-0951, 0953, 0956-0957, 0959-0961,0966, 0968-0974, 0976-0979, 0982-0983, 0985, 0987, 0991-0995, 0997-1000, 1002-1003, 1007, 1010, 1012-1016,1018-1021, 1023-1028, 1030, 1033-1036, 1038-1040, 1043-1057, 1059-1061, 1063-1070, 1073-1075, 1077, 1079-1084,1086-1089, 1092, 1094-1107, 1109-1116, 1118-1125, 1127-1128, 1130, 1132-3996

E P4320 22-1072 03 08 JUL 08 AUTO FLIGHT-GENERAL-ACTIVATE GLOBAL SPEEDPROTECTION AND F/D DISENGAGEMENT UPONSPEED CONSTRAINTS

Applicable to: MSN 0002, 0005-0014, 0019-0020, 0031, 0034, 0040-0041, 0044, 0061-0063, 0069-0072, 0078, 0083,0086, 0093-0094, 0100-0101, 0104-0108, 0110-0111, 0116-0118, 0121, 0125, 0128-0131, 0133, 0135, 0137, 0144-0145,0147, 0152-0153, 0155-0156, 0160-0162, 0165-0166, 0171-0172, 0178, 0184, 0186-0188, 0192, 0194, 0197-0198,0200-0202, 0206, 0208-0209, 0213-0214, 0216-0218, 0226-0228, 0235-0236, 0239, 0258, 0262-0263, 0267-0273,0278, 0281-0282, 0285-0287, 0297-0298, 0306-0307, 0318-0319, 0329, 0337, 0339-0340, 0346, 0351-0352, 0355,0358, 0360, 0366-0367, 0372, 0377, 0380-0382, 0387-0388, 0399-0401, 0408, 0410, 0412, 0417-0418, 0434, 0458,0468, 0473-0474, 0477, 0484, 0488, 0491, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522, 0524, 0526, 0529,0532-0533, 0535, 0541, 0544-0545, 0548, 0550, 0553, 0556, 0559-0560, 0562-0564, 0566-0567, 0573-0574,0576-0578, 0583, 0585-0586, 0588, 0593, 0595-0596, 0598-0600, 0603, 0608-0610, 0612, 0616, 0618, 0621,0623, 0625, 0627, 0629, 0635-0637, 0640-0644, 0646-0647, 0651-0654, 0657, 0660, 0663-0665, 0668, 0673-0674,0676, 0679-0681, 0684, 0686-0687, 0689-0690, 0692, 0694, 0696, 0698-0701, 0703-0710, 0712-0713, 0715-0718,0720, 0722-0725, 0727, 0729-0730, 0733-0735, 0737-0738, 0741, 0744-0745, 0747-0750, 0754-0755, 0760-0761,0763-0767, 0771-0772, 0774, 0777-0778, 0782-0783, 0786, 0788-0790, 0793-0794, 0796, 0798-0799, 0801,0804, 0806-0807, 0809-0810, 0815, 0818-0819, 0821, 0825, 0827-0828, 0830, 0832-0833, 0835, 0837-0838, 0841,0843-0844, 0846-0850, 0853-0855, 0858-0864, 0867-0868, 0870-0876, 0878-0879, 0881-0887, 0889-3996




M(1) MODIFICATION Linked SB Incorp. Date TitleP4391 34-1143 08 08 JUL 08 NAVIGATION - GPS - ACTIVATE A PRIMARY GPS

MEANS OF NAVIGATION USING LITTON GPS (CLASSC1 - HYBRID ARCHITECTURE)

Applicable to: MSN 0364, 0385, 0412, 0458, 0468, 0473-0474, 0484, 0493, 0502, 0505, 0518, 0550, 0557, 0560,0563-0565, 0567, 0573, 0575, 0580, 0582, 0591, 0595, 0597, 0604, 0609-0610, 0614, 0616, 0620, 0623, 0627,0631-0633, 0641, 0646, 0651-0654, 0657, 0659, 0661, 0663, 0666-0668, 0674-0675, 0679, 0684, 0689, 0692, 0694,0696, 0698-0700, 0704-0706, 0709-0710, 0712, 0717-0718, 0720, 0722-0723, 0729, 0738, 0744-0745, 0761, 0775,0794, 0805, 0808, 0823, 0853, 0860, 0875, 0887, 0901, 0908, 1016

P4507 32-1174 01 08 JUL 08 LANDING GEAR - INSTALL ABS A321 WHEELS ANDBRAKES ON A320

Applicable to: MSN 0043, 0113-0114, 0565, 0575, 0580, 0659, 0661, 0667, 0934, 0951, 0990, 0999, 1014, 1138, 1168,1177, 1183, 1217, 1226, 1383, 1407, 1418, 1424, 1459, 1697, 1732, 1987

E P4576 08 JUL 08 LANDING GEAR-ALTERNATE BRAKING- INTRODUCEMODIFIED ALTERNATE BRAKING SYSTEM

Applicable to: MSN 1599, 1660, 1939, 1991, 2017, 2035, 2037, 2043, 2050-2051, 2053, 2059, 2062, 2071, 2081,2100, 2109, 2119-2120, 2129, 2170, 2176, 2181, 2184, 2186, 2189, 2196, 2213-2214, 2218, 2224, 2228, 2230, 2245,2249, 2251, 2257, 2265, 2268, 2271, 2276-2277, 2279, 2281, 2283, 2289, 2291-2292, 2296-2297, 2299-2300, 2306,2308, 2317, 2319, 2322, 2326, 2328-2329, 2332-2333, 2335, 2338, 2344, 2346, 2350, 2353-2355, 2358, 2360-2362,2366-2367, 2370, 2375-2380, 2382-2383, 2385, 2387, 2392, 2394-2396, 2398, 2400-2404, 2406, 2412-2414,2417-2420, 2423-2424, 2427, 2431, 2433-2434, 2436, 2438-2446, 2448, 2450, 2452-2453, 2455-2457, 2460, 2463,2465, 2467-2471, 2473, 2475-2477, 2481, 2483-2485, 2487, 2490, 2492, 2495-2497, 2501-2503, 2506, 2511-2516,2518-2519, 2522-2524, 2526-2529, 2531, 2533, 2537-2541, 2544, 2546, 2548, 2550, 2552-2558, 2560-2561,2564-2567, 2569, 2571-2573, 2575-2576, 2578, 2581-2582, 2584-2588, 2590, 2592-2594, 2596, 2598, 2600-2605,2607-2612, 2616-2617, 2619-2626, 2628-2629, 2631-2634, 2636-2638, 2642, 2644-2646, 2648-2651, 2653-2666,2668, 2670, 2672-2681, 2683-2689, 2691-2709, 2711-2724, 2726-2754, 2756-2774, 2776-2780, 2782-2801,2803-2804, 2806-2813, 2816-2818, 2820-2831, 2833-2838, 2840-2846, 2849-2870, 2872-2879, 2881-2889,2891-2899, 2902-2939, 2941-2944, 2946-2947, 2949-2968, 2971-2976, 2978-2991, 2993-3019, 3021-3028,3030-3038, 3040-3071, 3073-3090, 3092-3103, 3105, 3107-3118, 3120-3143, 3145-3149, 3151-3189, 3191-3194,3196-3199, 3201-3225, 3227, 3229-3249, 3251-3257, 3259-3262, 3264-3268, 3270-3286, 3288-3310, 3312-3341,3343-3347, 3349-3996

E P4808 08 JUL 08 LANDING GEAR-WHEELS AND BRAKES- INTRODUCEBSCU COMMON STD

Applicable to: MSN 1599, 1660, 1752, 1766, 1774, 1785, 1789, 1796, 1800, 1802, 1810, 1812, 1815, 1819-1820,1823-1824, 1827-1828, 1833, 1835, 1839, 1849, 1861, 1868, 1870, 1873, 1875, 1879, 1885, 1891, 1894, 1896-1898,1900, 1904, 1915, 1917, 1923-1924, 1927, 1938-1939, 1948-1949, 1959, 1976, 1982, 1990-1991, 2000, 2002,2006-2007, 2013, 2015, 2017, 2020, 2023, 2026, 2028, 2031-2033, 2035, 2037, 2039, 2042-2043, 2047, 2050-2053,2057, 2059, 2062-2063, 2069, 2071-2072, 2074-2075, 2081-2083, 2085-2087, 2089-2093, 2095-2096, 2098-2101,2103, 2106, 2108-2109, 2112-2113, 2116, 2119-2122, 2124-2125, 2127-2136, 2138-2142, 2144, 2146-2156, 2158-2179,2181-2189, 2191-2207, 2209-2210, 2212-2215, 2217-2219, 2221-2224, 2227-2233, 2235-2241, 2243-2246, 2248-2254,2256-2260, 2262-2266, 2268-2269, 2271-2289, 2291-2302, 2304, 2306-2308, 2310-2314, 2316-2319, 2321-2322,2325-2329, 2331-2336, 2338-2341, 2343-2350, 2352-2356, 2358-2362, 2364-2380, 2382-2409, 2411-2461,2463-2471, 2473-2475, 2477-2479, 2481-2487, 2489-2520, 2522-2529, 2531-2535, 2537-2542, 2544-2548,2550-2552, 2554-2562, 2564-2589, 2591-2598, 2600-2609, 2611-2652, 2654-2681, 2683-2686, 2688-2706,2708-2712, 2714-2725, 2727-2729, 2731-2735, 2737-2740, 2742-2755, 2757-2758, 2760-2766, 2768-2792,2794-2798, 2800-2808, 2810-2822, 2824-2861, 2863-2867, 2869-2881, 2883-2894, 2896-2902, 2904-2911,




M(1) MODIFICATION Linked SB Incorp. Date Title2913-2915, 2917-2918, 2920-2926, 2928-2932, 2934-2935, 2937-2956, 2958-2964, 2966-2970, 2972-2973,2975-2995, 2997-2998, 3000-3004, 3006-3012, 3014, 3016-3021, 3023-3033, 3035-3050, 3052-3066, 3068-3069,3071-3074, 3076-3080, 3082-3097, 3099-3105, 3107-3111, 3113-3119, 3121-3125, 3127-3129, 3131-3145, 3147-3190,3192-3197, 3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228, 3230-3232, 3234, 3236-3240, 3242-3246,3248, 3250, 3252-3253, 3255-3261, 3263-3264, 3266, 3268-3273, 3275-3282, 3284-3289, 3291-3293, 3295-3296,3298-3301, 3303-3306, 3308-3314, 3316-3321, 3323-3325, 3327-3328, 3330-3333, 3335-3338, 3341-3349,3351-3354, 3356-3359, 3361-3366, 3368, 3370-3371, 3373-3381, 3383-3386, 3388-3396, 3398, 3400, 3402-3404,3406-3418, 3420-3428, 3430-3433, 3435-3440, 3442-3457, 3460-3461, 3463-3470, 3472-3492, 3494-3497,3499-3503, 3505-3506, 3508-3511, 3513-3521, 3524, 3526, 3528-3538, 3540-3545, 3547-3551, 3553-3556,3558-3565, 3567-3572, 3574, 3576-3582, 3585-3586, 3588-3591, 3594-3599, 3601-3611, 3613-3618, 3620-3622,3624, 3626-3628, 3630-3632, 3634-3635, 3640-3644, 3646-3652, 3654, 3656-3664, 3666-3668, 3670-3672,3674-3677, 3679-3680, 3683-3687, 3689-3707, 3709-3711, 3713-3716, 3718-3721, 3723-3724, 3726-3729, 3731-3736,3739, 3741-3748, 3750-3751, 3753-3760, 3762-3763, 3765, 3767-3783, 3785-3791, 3793-3795, 3807-3813, 3815,3817-3819, 3863, 3871-3877, 3937, 3638, 3797-3805, 3821-3829, 3831-3846, 3848-3857, 3859-3861, 3865-3866,3868, 3880, 3882-3883, 3885-3892, 3894-3898, 3900-3915, 3917-3919, 3921-3923, 3925, 3927, 3931-3933, 3935,3939, 3941-3943, 3945-3947, 3949-3950, 3952-3954, 3956-3959, 3962, 3965, 3967-3968, 3970-3972, 3983-3984,3995

ER P5168 34-1162 0834-1406 01

08 JUL 08 NAVIGATION - MMR - INSTALL COLLINS MMRPROVIDING ILS AND GPS FUNCTION

Applicable to: MSN 0498, 0509, 0521, 0529, 0544, 0598, 0600, 0608, 0618, 0625, 0633, 0637, 0644, 0647, 0660,0665, 0739, 0743, 0750, 0754-0756, 0758, 0763, 0767, 0777, 0784, 0790, 0796, 0802, 0811-0812, 0815-0816, 0821,0833, 0837-0839, 0841, 0849, 0854, 0859, 0869, 0877, 0880-0881, 0892, 0895, 0897, 0900, 0906, 0908-0910,0917, 0926-0928, 0930, 0932-0933, 0938-0939, 0941, 0943, 0945, 0950, 0956, 0958, 0960-0961, 0963, 0966-0967,0975-0977, 0979, 0982-0986, 0991, 0993, 0998, 1000, 1002, 1008-1010, 1015, 1020, 1023-1025, 1029, 1034, 1036,1039, 1041-1042, 1047, 1053, 1057, 1059, 1063, 1066-1067, 1071, 1073, 1078, 1080, 1082, 1087, 1090-1092, 1094,1096, 1099-1101, 1103, 1106-1107, 1113, 1115, 1118-1121, 1123, 1125-1127, 1130-3996

E P5518 32-1196 0332-1232 0132-1336 01

08 JUL 08 LANDING GEAR-NORMAL BRAKING- INTRODUCE STD8 BSCU (TWIN VERSION)

Applicable to: MSN 0002-0044, 0052-0055, 0059-0073, 0076-0078, 0081-0088, 0091-0094, 0098-0246, 0248-0250,0252-0256, 0258-0395, 0399-0415, 0417-0422, 0424-0430, 0434-0450, 0452-0468, 0470-0485, 0487-0489, 0491,0493-0498, 0500-1156, 1158-3996

P5594 08 JUL 08 ENGINE - GENERAL - INSTALL CFM56-5B3/2P ENGINESAT 33.000 LBS

Applicable to: MSN 0920, 0935, 0941, 0961, 0970, 0995, 1012, 1185, 1241, 1458, 1978, 2208E P5768 24-1096 05 08 JUL 08 ELEC PWR-AC EMERGENCY GENERATION-

ACTIVATE A319/A321 ELECTRICAL EMERGENCYCONFIGURATION ON A320 A/C

Applicable to: MSN 1130, 1138, 1143, 1146, 1148, 1150, 1152, 1156, 1158, 1162-1163, 1166, 1168, 1171, 1173, 1175,1177, 1179, 1181, 1183, 1187, 1189, 1192, 1194, 1196, 1198, 1200, 1206, 1208, 1210, 1213, 1215, 1217, 1221, 1224,1226, 1229, 1231, 1234-1235, 1237, 1240, 1242, 1244, 1246, 1248, 1251, 1253, 1255, 1257, 1259, 1262, 1264, 1266,1268, 1270, 1272, 1274, 1280, 1282, 1284, 1286, 1288, 1290, 1292, 1294, 1296, 1298, 1300, 1302, 1304, 1306,1308, 1310, 1312, 1314, 1316, 1318, 1320, 1322, 1327, 1330, 1332, 1334, 1337, 1339, 1341, 1343, 1345, 1347, 1349,1351, 1353, 1355, 1357, 1359, 1361, 1363, 1365, 1367-1368, 1370, 1372, 1376, 1379, 1381, 1383, 1385, 1387, 1390,1394, 1396, 1398, 1400, 1402, 1405, 1407, 1409, 1411, 1413, 1416, 1418-1419, 1422, 1424, 1427, 1430, 1432, 1435,




M(1) MODIFICATION Linked SB Incorp. Date Title1437, 1439, 1441, 1443, 1446, 1448, 1450, 1452, 1454, 1457, 1459, 1461, 1464, 1467, 1469-1470, 1473, 1475, 1478,1480, 1482, 1484, 1486, 1489, 1491, 1493, 1495, 1497, 1500, 1502, 1504, 1506, 1508-1509, 1512, 1514, 1516, 1518,1523, 1526, 1528, 1530, 1532-1533, 1535, 1538, 1540, 1542, 1544, 1546, 1548, 1550, 1553, 1555, 1557, 1559, 1561,1564, 1566, 1568, 1571, 1578, 1580, 1584, 1586, 1588, 1591, 1593, 1595, 1597, 1605, 1609-1610, 1613, 1615, 1617,1620-1621, 1624, 1626, 1628, 1631, 1633, 1635, 1637, 1639, 1641, 1644, 1646, 1648, 1650, 1652, 1655, 1657, 1661,1663, 1665, 1667, 1669, 1672, 1674, 1676, 1678, 1680, 1682, 1686-1687, 1689, 1692, 1694, 1696-1697, 1700, 1702,1705, 1708, 1710, 1712, 1715, 1717, 1719, 1721, 1723, 1725, 1728, 1730, 1732, 1735-1736, 1739, 1741, 1744, 1747,1749, 1751, 1754-1755, 1757, 1760, 1762, 1764, 1767, 1769, 1771, 1773, 1775, 1777, 1780, 1782, 1784-1785, 1787,1789, 1792-1793, 1797, 1799, 1802, 1804, 1806, 1809, 1812-1814, 1816, 1818, 1821-1823, 1825, 1827, 1829, 1832,1834-1835, 1838, 1840, 1842, 1845, 1847, 1849, 1852, 1854, 1856-1858, 1860-1862, 1864-1865, 1867-1868, 1871,1873-1874, 1877, 1879, 1883, 1885, 1888-1889, 1891-1892, 1894-1896, 1898-1900, 1902-1904, 1906-1907, 1909-1911,1913-1915, 1917-1920, 1922, 1924, 1927, 1929-1931, 1933, 1935, 1937, 1940, 1942, 1944-1945, 1948-1949, 1951,1954, 1957-1958, 1961, 1964-1965, 1968-1969, 1973, 1975, 1979, 1981, 1983, 1987, 1989, 1993, 1996, 1998, 2001,2003, 2006, 2009, 2011, 2014, 2016, 2018, 2020, 2022, 2024, 2027, 2029, 2031, 2034, 2036, 2038, 2040, 2042,2044, 2046, 2048-2049, 2054, 2056, 2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2077, 2079, 2082, 2084-2085,2088, 2090, 2092, 2094, 2097, 2099, 2102, 2104, 2106, 2108, 2112, 2114, 2116, 2118, 2121, 2123, 2125, 2128, 2130,2132-2169, 2171, 2173, 2175, 2177-2178, 2180, 2182-2183, 2185, 2187, 2189, 2191, 2193, 2195, 2197, 2199, 2201,2204, 2206-2207, 2210, 2212, 2215, 2217, 2219, 2221, 2223, 2225, 2227, 2229, 2231, 2233, 2235, 2238-2239, 2242,2244, 2246, 2248, 2250, 2252, 2254, 2256-2257, 2259, 2272, 2274-2275, 2278, 2280, 2282, 2284, 2286, 2288,2291-2292, 2294, 2297, 2299, 2301, 2307, 2310, 2312, 2314, 2316, 2322, 2325, 2327, 2329, 2331, 2334, 2336, 2338,2340, 2343, 2345, 2347, 2349, 2352, 2354, 2356, 2359, 2361, 2364, 2366, 2368, 2372, 2374, 2376, 2384, 2386,2388, 2390-2391, 2393, 2395, 2397, 2399, 2401, 2403, 2405, 2407, 2409, 2411, 2413, 2415, 2417, 2419, 2422-2423,2425, 2428, 2430, 2432, 2434, 2437, 2439, 2441, 2443, 2445, 2447, 2449, 2451, 2453, 2455, 2457, 2459, 2461,2475, 2478-2479, 2482, 2484, 2486, 2489, 2491, 2493, 2496, 2498, 2502, 2504, 2506, 2509, 2511, 2513, 2515, 2517,2520, 2522, 2524, 2526, 2529, 2531, 2533, 2535, 2537, 2539-2540, 2542, 2562, 2564, 2566, 2569, 2571, 2573,2576-2577, 2580, 2583-2584, 2587, 2589, 2591, 2594, 2596, 2598, 2600, 2602, 2604, 2606, 2608-2609, 2612-2613,2616, 2619-2620, 2623, 2626-2627, 2630, 2633, 2635, 2637, 2640, 2642, 2645, 2647, 2649, 2651, 2654, 2656, 2658,2661, 2663, 2665, 2668, 2670-2671, 2674, 2676, 2678, 2680, 2683, 2685, 2688-2689, 2692, 2695-2696, 2699, 2701,2703, 2705, 2708, 2710, 2712, 2714, 2717, 2719, 2721, 2724-2725, 2728, 2731-2732, 2734, 2737, 2740, 2743, 2745,2747, 2749, 2752-2753, 2755, 2758, 2760-2761, 2764, 2766, 2768, 2770, 2772, 2775-2776, 2778, 2781, 2783, 2785,2787, 2789, 2791-2792, 2794, 2796, 2798, 2800, 2802, 2804, 2807-2808, 2810, 2814, 2816-2817, 2820, 2822, 2824,2826, 2828, 2830, 2832, 2834-2835, 2838, 2840, 2842, 2844, 2846, 2848, 2851, 2853, 2855-2856, 2859, 2861, 2863,2865, 2867, 2869, 2871, 2874-2875, 2877, 2880-2881, 2883, 2885, 2896, 2899-2900, 2902, 2904, 2906, 2908-2909,2911, 2914-2915, 2917, 2920, 2922, 2924, 2926, 2928, 2930, 2932, 2934, 2937, 2939, 2941, 2943-2945, 2947, 2950,2952-2953, 2956, 2958, 2960, 2962, 2964, 2966, 2968, 2970, 2973, 2975, 2977, 2980, 2982, 2984, 2986-2995, 2998,3000, 3002, 3004, 3006, 3008, 3010, 3012, 3014, 3016, 3018, 3021, 3023, 3025, 3027, 3029, 3031, 3033, 3035, 3037,3039-3040, 3042, 3044, 3047-3048, 3050, 3052, 3055-3056, 3058, 3060, 3063-3064, 3066, 3068, 3071-3072, 3074,3076, 3079-3080, 3083, 3086-3087, 3089, 3091, 3093, 3095, 3097, 3099, 3101, 3103, 3105, 3107, 3109, 3111, 3113,3115, 3117, 3119, 3121, 3123, 3125, 3127, 3129, 3131-3132, 3135-3136, 3138, 3140-3141, 3143, 3145, 3147-3162,3164, 3166-3167, 3170, 3173-3174, 3177-3178, 3180, 3182-3183, 3185, 3187, 3189-3190, 3192, 3194, 3196-3197,3199, 3201, 3203, 3205-3206, 3208, 3210-3211, 3213, 3215, 3218-3219, 3221, 3223-3224, 3227-3228, 3230, 3232,3234, 3236-3237, 3239-3240, 3242, 3244, 3246, 3256-3257, 3259, 3261, 3263-3264, 3266, 3268, 3270, 3272-3273,3275, 3277-3278, 3280, 3282, 3284, 3286-3287, 3289, 3291, 3293, 3295-3296, 3299, 3301, 3303-3304, 3306, 3308,3310, 3312-3314, 3316, 3318-3319, 3321, 3323, 3325, 3327-3328, 3330, 3332, 3335, 3337-3338, 3341, 3343, 3345,3348-3349, 3351, 3353-3354, 3357, 3359, 3361-3362, 3365-3366, 3368, 3370, 3373-3374, 3376, 3378-3379, 3381,3383-3384, 3386, 3389, 3391-3392, 3394, 3396, 3398, 3400, 3402, 3404, 3408-3410, 3412, 3414, 3416, 3418,




M(1) MODIFICATION Linked SB Incorp. Date Title3420, 3422-3423, 3425, 3427, 3430-3431, 3433, 3435, 3437, 3439-3440, 3444, 3446, 3448-3449, 3451, 3453,3455-3457, 3460-3461, 3464-3465, 3468, 3470, 3472-3490, 3492, 3494-3497, 3499, 3501-3503, 3505-3506, 3508,3510-3511, 3514-3517, 3519, 3521, 3524, 3526, 3528-3529, 3531-3532, 3535-3536, 3538, 3540-3541, 3543, 3545,3547, 3549-3550, 3553-3554, 3556, 3558-3559, 3562-3563, 3565, 3567-3568, 3570, 3572, 3574, 3576-3577, 3579,3581-3582, 3594, 3596-3599, 3601, 3603, 3605, 3607, 3609-3611, 3613, 3616, 3618, 3621-3622, 3624, 3626-3628,3630-3631, 3640-3641, 3643-3644, 3646, 3648-3650, 3652, 3654, 3656, 3658-3659, 3662, 3664, 3666-3668,3670, 3672, 3674, 3676-3677, 3679, 3690, 3692-3693, 3695-3699, 3701, 3703, 3706-3707, 3709, 3711, 3713-3716,3718-3719, 3721, 3723-3724, 3726, 3729, 3731-3732, 3734, 3736, 3739, 3741, 3743, 3745, 3747-3748, 3750, 3753,3755-3756, 3760, 3762, 3765, 3767, 3769, 3771, 3773, 3780-3783, 3785-3787, 3789, 3791, 3793, 3795, 3800, 3802,3804-3805, 3807, 3809, 3811-3813, 3815, 3817, 3823, 3829, 3835, 3843, 3850, 3863, 3871, 3875, 3891, 3904, 3937,3591, 3758, 3775-3778, 3797-3798, 3819, 3821, 3825, 3827, 3831, 3833, 3837, 3840, 3846, 3848, 3852, 3855, 3857,3859, 3861, 3866, 3868, 3873, 3877, 3880, 3882-3883, 3885, 3887, 3889, 3894, 3896, 3898, 3900, 3902, 3906-3910,3912-3915, 3917, 3919, 3921-3923, 3925, 3927, 3931, 3933, 3935, 3939, 3941-3943, 3945-3947, 3949, 3952-3954,3956-3959, 3965, 3967-3968, 3971-3972, 3984, 3995

P5983 08 JUL 08 AUTO FLIGHT - GENERAL - DE-ACTIVATE THE 'SPEEDPROTECTION' PACKAGE (ANTI-MOD OF 26497)

Applicable to: MSN 0963, 1008, 1042, 1204, 1227P6025 22-1077 00 08 JUL 08 AUTOFLIGHT - FMGC - DEACTIVATE THE "REDUCED

VAPP" FUNCTION FOR A320 CFM/IAE VERSIONSApplicable to: MSN 1037, 1047, 1059, 1063, 1067, 1087, 1099, 1101, 1119, 1200, 1208, 1221, 1229, 1255, 1262, 1288,1292, 1318, 1347, 1379, 1396, 1430, 1454, 1461, 1484, 1516, 1530, 1535, 1540, 1550, 1633, 1641, 1646, 1655, 1674,1694, 1736, 1789, 1793, 1809, 1812, 1973, 2054, 2061, 2082, 2092, 2104, 2143, 2225, 2242, 2248, 2347, 2391, 2998,3099, 3147-3148, 3189

ER P6054 34-1186 0534-1232 0134-1425 00

08 JUL 08 NAVIGATION - MMR - ACTIVATE GPS PRIMARYFUNCTION (HYBRID) IN SEXTANT MMR (WITHHONEYWELL OR LITTON ADIRU)

Applicable to: MSN 0552, 0570, 0581, 0591, 0677, 0737, 0749, 0764, 0768, 0771, 0774, 0776, 0781, 0787,0792-0793, 0797, 0806, 0809-0810, 0835, 0844, 0852, 0855, 0861, 0863-0864, 0868, 0872, 0878, 0884-0885, 0890,0894, 0896, 0899, 0904-0905, 0913-0915, 0919-0920, 0922, 0929, 0934-0936, 0942, 0946-0947, 0949, 0954, 0957,0968-0974, 0990, 0995, 0997, 1004-1007, 1012-1014, 1017, 1019, 1026, 1028, 1030-1031, 1033, 1035, 1038, 1040,1044-1046, 1048, 1051-1055, 1060-1061, 1065, 1068-1070, 1072, 1074, 1077, 1080-1082, 1084, 1086, 1089, 1093,1095, 1097-1098, 1102, 1104-1105, 1108-1109, 1112, 1114-1115, 1118, 1121-1122, 1124-1125, 1128, 1130, 1132,1134-1137, 1141-1142, 1145-1148, 1150, 1152-1153, 1155, 1160-1163, 1170-1172, 1174-1175, 1177, 1179, 1182-1184,1188-1189, 1192-1193, 1195-1199, 1203, 1205, 1207, 1209-1211, 1213-1215, 1218-1219, 1222, 1224-1225, 1228,1232-1233, 1236, 1238-1239, 1243-1245, 1248, 1250, 1254, 1258-1261, 1263-1266, 1268-1269, 1272-1273, 1275-1279,1282-1283, 1285-1287, 1289-1291, 1293-1298, 1301, 1303, 1305-1306, 1308, 1310-1315, 1317, 1319-1322, 1326,1328-1331, 1333, 1336-1338, 1340-1343, 1348-1349, 1354, 1356-1361, 1363-1367, 1369-1372, 1377-1378, 1380-1391,1393, 1401-1403, 1406-1410, 1412-1413, 1416-1429, 1431-1433, 1435-1442, 1445, 1447, 1450-1451, 1455, 1458-1460,1462-1463, 1465-1466, 1469, 1472, 1474-1475, 1477-1478, 1481, 1487-1488, 1490, 1492-1497, 1499, 1503-1504,1507-1508, 1510-1511, 1513-1515, 1517, 1519, 1521-1522, 1525, 1527, 1529, 1531-1534, 1536-1539, 1541-1542, 1545,1547, 1551-1553, 1555, 1558-1565, 1569, 1571, 1573-1574, 1576-1577, 1579, 1581, 1583-1586, 1590, 1594, 1596,1600-1607, 1609, 1611, 1614-1615, 1617-1618, 1620-1621, 1623, 1627, 1629-1632, 1634, 1636-1639, 1643-1644,1647, 1649, 1651, 1653-1654, 1660-1661, 1664-1671, 1673, 1679-1680, 1682, 1684, 1687-1690, 1692, 1696-1698,1701-1702, 1704, 1708, 1710-1711, 1715, 1717-1720, 1723-1726, 1728, 1731-1732, 1734, 1737, 1741-1744, 1747-1749,1751, 1753-1757, 1759-1762, 1764-1765, 1769, 1772, 1775-1778, 1781-1783, 1786-1788, 1792, 1797, 1803, 1805-1806,




M(1) MODIFICATION Linked SB Incorp. Date Title1811, 1814, 1821, 1828-1829, 1838, 1840-1845, 1847, 1851-1853, 1860, 1862-1865, 1867, 1869, 1871, 1874, 1876,1878, 1883, 1886, 1890, 1899, 1905-1907, 1910-1911, 1914, 1918-1920, 1929-1931, 1933, 1935, 1937, 1939-1940,1943, 1946-1947, 1953, 1955-1956, 1958, 1963-1964, 1966-1969, 1974-1975, 1977, 1979-1981, 1983, 1987-1988,1991-1998, 2001, 2005, 2009-2010, 2012, 2014, 2017-2019, 2022-2023, 2027, 2029-2030, 2032, 2034, 2036-2038,2040-2041, 2043-2045, 2048-2051, 2053, 2055-2056, 2058, 2062, 2067-2068, 2077, 2080, 2098, 2103, 2108,2110, 2123, 2128, 2131, 2135, 2137, 2139, 2145, 2155-2157, 2164-2165, 2168, 2171, 2174-2175, 2178, 2180, 2182,2187-2188, 2190, 2193-2195, 2198-2199, 2204, 2207, 2209-2210, 2212, 2218-2219, 2221, 2223, 2226, 2235-2236,2239-2241, 2244-2245, 2247, 2249, 2251-2253, 2255, 2258, 2260-2262, 2265, 2267, 2271, 2274, 2276, 2283, 2287,2289-2290, 2300, 2302-2303, 2305-2306, 2309, 2312-2313, 2315, 2318-2320, 2323-2325, 2327-2328, 2331, 2333,2340, 2346, 2348, 2351, 2353, 2358-2360, 2363, 2367, 2370, 2377-2378, 2380, 2385, 2387-2389, 2392, 2394,2397-2398, 2400, 2402, 2405-2407, 2412, 2416-2417, 2420, 2422, 2427, 2429-2430, 2436-2437, 2440-2442, 2446,2448, 2450-2451, 2458-2460, 2462-2463, 2465-2466, 2471, 2477-2483, 2492-2495, 2497-2498, 2503, 2510, 2512,2514, 2517-2518, 2521, 2523, 2527-2530, 2534, 2536, 2538-2540, 2543-2544, 2547-2549, 2552, 2562, 2565-2566,2568, 2570, 2575, 2578, 2589, 2591, 2593, 2595-2597, 2602, 2605-2607, 2613, 2615, 2619-2620, 2623-2624,2627-2630, 2632, 2636, 2639, 2646, 2652-2654, 2658, 2662, 2668-2669, 2672, 2677-2678, 2681-2682, 2684-2685,2690-2691, 2693-2697, 2700, 2702, 2709, 2713, 2715, 2720, 2727, 2729, 2732, 2735, 2741-2742, 2744-2745, 2749,2751, 2754, 2757, 2759, 2761-2763, 2765, 2767, 2769, 2774-2775, 2777, 2779, 2782, 2785, 2794-2795, 2798-2799,2803-2804, 2806, 2808-2809, 2812-2813, 2818, 2820, 2825, 2827, 2829, 2833, 2835-2836, 2840-2841, 2844, 2846,2853-2854, 2857, 2860, 2863, 2865-2867, 2873, 2878-2879, 2882-2884, 2895, 2902, 2905, 2907, 2909, 2911, 2913,2923, 2925, 2935-2936, 2939, 2943, 2946, 2954, 2958-2959, 2962, 2968, 2971, 2973-2976, 2980-2981, 2988,2990-2991, 3003-3006, 3011, 3013-3014, 3019, 3021-3025, 3027-3028, 3036, 3038, 3040-3041, 3046, 3049-3050,3053, 3055, 3059, 3061, 3067, 3071, 3075, 3081-3084, 3086-3088, 3090, 3092-3093, 3095, 3104, 3106-3108,3110, 3112, 3114, 3116, 3118, 3121-3125, 3128, 3130-3132, 3134, 3137, 3139, 3146, 3149, 3152-3153, 3158-3160,3163-3164, 3167-3168, 3170, 3172, 3176, 3184, 3186-3188, 3192-3193, 3196-3198, 3202, 3205-3206, 3210, 3212,3215, 3221, 3224, 3227, 3233-3236, 3238, 3242-3247, 3249, 3252, 3254, 3259-3260, 3262, 3268, 3271, 3273-3274,3286, 3288-3290, 3293, 3297, 3300-3301, 3304-3305, 3308, 3310, 3312, 3314-3315, 3317, 3321, 3326, 3335, 3337,3340, 3344, 3346, 3351-3352, 3355-3358, 3361, 3366-3369, 3374-3375, 3383, 3386, 3389, 3396-3397, 3407, 3411,3413-3415, 3422, 3425-3426, 3431-3432, 3435, 3437, 3440, 3442, 3447, 3449, 3453, 3455-3457, 3461, 3466, 3468,3471, 3475, 3480-3481, 3483, 3485, 3496-3500, 3504, 3506, 3508, 3512, 3514, 3516, 3528-3530, 3534, 3537,3541, 3544, 3550-3551, 3553, 3555, 3557, 3559, 3569-3571, 3573, 3579, 3583-3584, 3586, 3593, 3596, 3599-3601,3604-3605, 3607-3608, 3611-3613, 3615, 3618-3620, 3629, 3633-3634, 3636, 3639, 3641, 3649-3650, 3652, 3657,3661, 3667, 3669, 3675-3677, 3680, 3682-3683, 3687, 3689-3690, 3692, 3696-3698, 3700, 3702-3704, 3706, 3708,3712, 3716, 3720-3721, 3723, 3726, 3728, 3730-3731, 3735, 3737, 3740, 3742, 3746, 3749, 3752, 3754, 3756,3763, 3774-3775, 3780, 3782, 3787-3788, 3790, 3792-3793, 3796-3797, 3799, 3805, 3808-3810, 3817, 3824, 3839,3841-3845, 3854-3855, 3858, 3862-3863, 3871, 3904-3905, 3937, 3943-3946, 3591, 3758, 3821-3822, 3830, 3833,3848, 3852, 3865, 3868, 3873-3874, 3879, 3881, 3886-3889, 3893-3894, 3898, 3909, 3912-3913, 3918, 3922, 3924,3926, 3928, 3932-3933, 3935, 3953, 3955, 3960-3967, 3970-3971, 3977, 3984-3996

E P6183 34-1232 01 08 JUL 08 NAVIGATION - MMR - REMOVE COLLINS MMRPROVIDING ILS (FM IMMUNE) AND GPS PRIMARYFUNCTION (PREVIOUS SPEC.)

Applicable to: MSN 1053, 1080, 1082, 1115, 1118, 1121, 1125, 1130, 1132, 1134-1138, 1141-1142, 1144-1150,1152-1153, 1155, 1160-1164, 1166-1168, 1170-1172, 1174-1175, 1177-1179, 1182-1184, 1188-1189, 1191-1193,1195-1199, 1203, 1205, 1207, 1209-1211, 1213-1215, 1217-1220, 1222-1226, 1228, 1230, 1232-1234, 1236, 1238-1239,1243-1245, 1248-1250, 1254, 1258-1261, 1263-1266, 1268-1269, 1272-1279, 1281-1287, 1289-1291, 1293-1298, 1301,1303, 1305-1306, 1308, 1310-1315, 1317, 1319-1326, 1328-1331, 1333, 1336-1338, 1340-1343, 1346, 1348-1350,




M(1) MODIFICATION Linked SB Incorp. Date Title1354, 1356-1361, 1363-1367, 1369-1375, 1377-1378, 1380-1393, 1395, 1397, 1401-1403, 1406-1410, 1412-1414,1416-1429, 1431-1442, 1445, 1447, 1450-1451, 1453, 1455-1456, 1458-1460, 1462-1463, 1465-1466, 1469, 1472,1474-1475, 1477-1478, 1481, 1483, 1487-1488, 1490, 1492-1499, 1501, 1503-1504, 1507-1508, 1510-1511, 1513-1515,1517, 1519-1522, 1525, 1527, 1529, 1531-1539, 1541-1543, 1545, 1547, 1549, 1551-1553, 1555, 1558-1565, 1567,1569-1571, 1573-1574, 1576-1577, 1579, 1581-1586, 1590, 1594, 1596, 1600-1607, 1609, 1611, 1614-1615, 1617-1618,1620-1621, 1623, 1627, 1629-1634, 1636-1639, 1641, 1643-1644, 1646-1647, 1649, 1651, 1653-1654, 1659-1662,1664-1671, 1673, 1679-1680, 1682-1685, 1687-1690, 1692-1693, 1696-1698, 1701-1702, 1704, 1708-1711, 1714-1715,1717-1720, 1723-1726, 1728, 1731-1732, 1734, 1737-1738, 1741-1744, 1746-1749, 1751-1757, 1759-1762, 1764-1766,1769, 1772, 1774-1778, 1781-1783, 1786-1789, 1792, 1796-1797, 1800, 1803, 1805-1806, 1810-1815, 1819-1821,1824, 1828-1829, 1833, 1838-1845, 1847, 1851-1853, 1860, 1862-1865, 1867, 1869-1871, 1874-1876, 1878, 1883,1886, 1890, 1897, 1899, 1905-1907, 1910-1911, 1914, 1918-1920, 1923, 1929-1931, 1933, 1935, 1937, 1939-1940,1943, 1946-1947, 1953, 1955-1956, 1958-1959, 1963-1964, 1966-1969, 1974-1977, 1979-1983, 1987-1988, 1990-1998,2001-2002, 2005, 2009-2010, 2012-2014, 2017-2019, 2022-2023, 2026-2030, 2032, 2034, 2036-2041, 2043-2045,2047-2051, 2053, 2055-2056, 2058, 2062, 2067-2068, 2077, 2080, 2082, 2087, 2092, 2095, 2098, 2103, 2108,2110, 2123, 2128, 2131, 2135, 2137, 2139, 2145, 2155-2157, 2164-2165, 2168, 2171, 2174-2175, 2178, 2180, 2182,2187-2188, 2190, 2193-2195, 2198-2199, 2204, 2207, 2209-2210, 2212, 2218-2219, 2221, 2223, 2226, 2235-2236,2239-2241, 2244-2245, 2247, 2249, 2251-2253, 2255, 2258, 2260-2262, 2265, 2267, 2271, 2274, 2276, 2283, 2287,2289-2290, 2300, 2302-2303, 2305-2306, 2309, 2312-2313, 2315, 2318-2320, 2323-2325, 2327-2328, 2331, 2333,2340, 2346, 2348, 2351, 2353, 2358-2360, 2363, 2367, 2369-2370, 2373, 2377-2378, 2380, 2385, 2387-2389, 2392,2394, 2397-2398, 2400, 2402, 2405-2407, 2412, 2416-2417, 2420, 2422, 2427, 2429-2430, 2436-2437, 2440-2442,2446, 2448, 2450-2451, 2458-2460, 2462-2466, 2471, 2474, 2477-2483, 2492-2495, 2497-2498, 2503, 2510, 2512,2514, 2517-2518, 2521, 2523, 2527-2530, 2534, 2536, 2538-2540, 2543-2544, 2547-2549, 2552, 2562, 2565-2566,2568, 2570, 2575, 2578, 2589, 2591, 2593, 2595-2597, 2602, 2605-2607, 2613, 2615, 2618-2620, 2623-2624,2627-2630, 2632, 2636, 2639, 2641, 2646, 2652-2654, 2658, 2662, 2668-2669, 2672, 2677-2678, 2681-2682,2684-2685, 2690-2691, 2693-2697, 2700, 2702, 2709, 2713, 2715, 2720, 2727, 2729, 2732, 2735, 2741-2742,2744-2745, 2749, 2751, 2754, 2757, 2759, 2761-2763, 2765, 2767, 2769, 2774-2775, 2777, 2779, 2782, 2785,2794-2795, 2798-2799, 2803-2804, 2806, 2808-2809, 2812-2813, 2818, 2820, 2825, 2827, 2829, 2833, 2835-2836,2840-2841, 2844, 2846, 2853-2854, 2857, 2860, 2863, 2865-2867, 2873, 2878-2879, 2882-2884, 2895, 2902, 2905,2907, 2909, 2911, 2913, 2923, 2925, 2935-2936, 2939, 2943, 2946, 2954, 2958-2959, 2962, 2968, 2971, 2973-2976,2980-2981, 2988, 2990-2991, 3003-3006, 3011, 3013-3014, 3019, 3021-3025, 3027-3028, 3036, 3038, 3040-3041,3046, 3049-3050, 3053, 3055, 3059, 3061, 3067, 3071, 3075, 3081-3084, 3086-3088, 3090, 3092-3093, 3095, 3104,3106-3108, 3110, 3112, 3114, 3116, 3118, 3121-3125, 3128, 3130-3132, 3134, 3137, 3139, 3146, 3149, 3152-3153,3158-3160, 3163-3164, 3167-3168, 3170, 3172, 3176, 3184, 3186-3188, 3192-3193, 3196-3198, 3202, 3205-3206,3210, 3212, 3215, 3221, 3224, 3227, 3233-3236, 3238, 3242-3247, 3249, 3252, 3254, 3259-3260, 3262, 3268, 3271,3273-3274, 3286, 3288-3290, 3293, 3297, 3300-3301, 3304-3305, 3308, 3310, 3312, 3314-3315, 3317, 3321, 3326,3335, 3337, 3340, 3344, 3346, 3351-3352, 3355-3358, 3361, 3366-3369, 3374-3375, 3383, 3386, 3389, 3396-3397,3407, 3411, 3413-3415, 3422, 3425-3426, 3431-3432, 3435, 3437, 3440, 3442, 3447, 3449, 3453, 3455-3457, 3461,3466, 3468, 3471, 3475, 3480-3481, 3483, 3485, 3496-3500, 3504, 3506, 3508, 3512, 3514, 3516, 3528-3530,3534, 3537, 3541, 3544, 3550-3551, 3553, 3555, 3557, 3559, 3569-3571, 3573, 3579, 3583-3584, 3586, 3593, 3596,3599-3601, 3604-3605, 3607-3608, 3611-3613, 3615, 3618-3620, 3629, 3633-3634, 3636, 3639, 3641, 3649-3650,3652, 3657, 3661, 3667, 3669, 3675-3677, 3680, 3682-3683, 3687, 3689-3690, 3692, 3696-3698, 3700, 3702-3704,3706, 3708, 3712, 3716, 3720-3721, 3723, 3726, 3728, 3730-3731, 3735, 3737, 3740, 3742, 3746, 3749, 3752, 3754,3756, 3763, 3774-3775, 3780, 3782, 3787-3788, 3790, 3792-3793, 3796-3797, 3799, 3805, 3808-3810, 3817, 3824,3839, 3841-3845, 3854-3855, 3858, 3862-3863, 3871, 3904-3905, 3937, 3943-3946, 3591, 3758, 3821-3822, 3830,3833, 3848, 3852, 3865, 3868, 3873-3874, 3879, 3881, 3886-3889, 3893-3894, 3898, 3909, 3912-3913, 3918, 3922,3924, 3926, 3928, 3932-3933, 3935, 3953, 3955, 3960-3967, 3970-3971, 3977, 3984-3996




M(1) MODIFICATION Linked SB Incorp. Date TitleP6193 08 JUL 08 AUTOFLIGHT - FMS - DEACTIVATE BATCH 1 OPTION

OF FMS (PREVIOUS SPEC.)Applicable to: MSN 1144, 1149, 1154, 1164-1167, 1178, 1180-1181, 1187, 1191, 1194, 1196, 1200, 1202, 1204,1206, 1208, 1221, 1223, 1227-1231, 1234, 1247, 1249, 1255, 1262, 1274, 1281, 1284, 1288, 1292, 1307, 1316, 1318,1323-1325, 1345-1347, 1350, 1362, 1373-1375, 1379, 1392, 1395-1397, 1399, 1414, 1422, 1430, 1434, 1453-1454,1456, 1461, 1479, 1483-1484, 1498, 1501, 1516, 1520, 1530, 1535, 1540, 1543, 1549-1550, 1554, 1561, 1567, 1570,1572, 1582, 1633, 1635, 1641, 1646, 1655, 1659, 1662, 1674, 1681, 1683, 1685, 1693-1694, 1698, 1700, 1709,1713-1714, 1716, 1736, 1738, 1746, 1752, 1766, 1774, 1789, 1793, 1796, 1800, 1809-1810, 1812, 1815, 1819-1820,1824, 1828, 1833-1834, 1836, 1839, 1870, 1875, 1892, 1897, 1902, 1923, 1959, 1976, 1982, 1990, 2002, 2013, 2026,2028, 2039, 2047, 2058, 2082, 2087, 2092, 2095, 2104, 2115, 2143, 2220, 2225, 2242, 2248, 2252, 2270, 2347, 2357,2369, 2373, 2381, 2391, 2464, 2472, 2474, 2488, 2517, 2563, 2568, 2599, 2618, 2641, 2775, 3104

P6197 08 JUL 08 AUTOFLIGHT - FCU - DEACTIVATE FUNCTION "FD"ENGAGEMENT IN CROSSED BARS "GOAROUND"FROM FCU (PREVIOUS SPEC.)

Applicable to: MSN 1149, 1164-1165, 1167, 1187, 1191, 1194-1196, 1199, 1204, 1218, 1227, 1230, 1249, 1316,1324-1325, 1345-1346, 1392, 1408, 1414, 1421, 1434, 1438, 1453, 1456, 1459, 1479, 1483, 1487, 1498, 1501, 1520,1535, 1543, 1549, 1567, 1570, 1582, 1633, 1641, 1646, 1659, 1662, 1683, 1685, 1693, 1700, 1709, 1714, 1738, 1746,1752, 1766, 1774, 1789, 1796, 1800, 1810, 1812, 1815, 1819-1820, 1824, 1828, 1833, 1839, 1870, 1875, 1897, 1923,1959, 1976, 1982, 1990, 2002, 2013, 2026, 2028, 2039, 2047, 2082, 2087, 2092, 2095, 2369, 2373, 2464, 2474, 2618,2641

P6310 08 JUL 08 ENGINE - GENERAL - INSTALL PW 6100 ENGINE RATEDAT 22.100 IBF ON A318

Applicable to: MSN 3001, 3030, 3062, 3214, 3216, 3371, 3390, 3438, 3469, 3509, 3585, 3602, 3606, 3635, 3642E P6375 32-1201 04 08 JUL 08 LANDING GEAR-PARKING/ULTIMATE EMERGENCY

BRAKING-INTRODUCE A PRESSURE SWITCHApplicable to: MSN 0002-0019, 0035-0039, 0043-0051, 0053-0054, 0056-0058, 0061-0063, 0066-0080, 0083-0102,0104-0140, 0142-0148, 0151-0157, 0161-0163, 0165-0170, 0172-0175, 0177-0188, 0191-0192, 0194-0203, 0205-0209,0211-0230, 0233-0243, 0245-0248, 0250-0254, 0256-0258, 0261-0262, 0264-0270, 0274-0276, 0278-0280, 0282,0285-0287, 0289, 0291-0296, 0299-0301, 0303, 0308, 0314-0317, 0319-0323, 0325-0329, 0331-0332, 0334-0338,0344, 0346-0349, 0351-0354, 0357-0358, 0361-0362, 0365-0366, 0369, 0373-0377, 0379, 0382-0386, 0389-0390,0392-0393, 0395-0398, 0400-0401, 0403, 0405-0407, 0409, 0411-0413, 0415-0416, 0422-0423, 0425-0428,0430-0435, 0437-0440, 0442, 0444-0447, 0450-0470, 0472-0520, 0522-0523, 0525-0541, 0543-0545, 0548-0552,0554-0557, 0559-0560, 0562-0571, 0573, 0575-0585, 0587, 0589-0621, 0623-0628, 0630-0633, 0636-0638,0640-0642, 0644-0652, 0654-0655, 0658-0661, 0666-0671, 0674-0676, 0678-0681, 0683-0695, 0698-0718,0720-0725, 0727, 0729-0735, 0737-0741, 0743-0748, 0750-0754, 0756, 0758-0761, 0763-0765, 0767-0768,0771-0772, 0775-0777, 0780-0784, 0787-0788, 0791-0792, 0794-0797, 0799, 0802, 0804-0806, 0808, 0811-0816,0819-0822, 0824-0828, 0833-0837, 0839-0842, 0844-0845, 0847-0849, 0851-0853, 0855-0872, 0874-0881, 0883,0885-0893, 0895-0902, 0906, 0908-0915, 0917-0921, 0925-0928, 0930, 0932-0933, 0935-0937, 0939-0945, 0947,0950-0952, 0954-0955, 0958-0961, 0963-0970, 0972-0974, 0976, 0980-1001, 1004-1005, 1007-1021, 1023-1033,1035-1039, 1041-1042, 1044-1046, 1048, 1050-1053, 1055, 1057, 1060-1061, 1063-1085, 1088-1091, 1093-1095,1097-1113, 1115-1121, 1123, 1125-1138, 1140-1143, 1145-1148, 1150, 1152-1156, 1158-1166, 1168-1170, 1172-1179,1181-1182, 1184-1185, 1188-1190, 1192-1194, 1196-1201, 1203-1204, 1206-1209, 1212-1218, 1220-1225, 1227-1228,1231-1237, 1239, 1241-1242, 1244, 1247, 1252-1256, 1258-1262, 1264-1268, 1270-1271, 1273, 1275, 1277-1280,1282-1283, 1285-1286, 1288, 1290-1296, 1298-1300, 1303, 1305-1310, 1312, 1314, 1316-1322, 1324-1326, 1328-1331,1334-1336, 1340-1348, 1350, 1352, 1354, 1356-1365, 1367-3996




M(1) MODIFICATION Linked SB Incorp. Date TitleP6387 08 JUL 08 ELECTRICAL POWER-AC EMERGENCY GENERATION-

REINSTALL A320 ELECTRICAL EMERGENCYCONFIGURATION

Applicable to: MSN 1146, 1163, 1166, 1187, 1200, 1208, 1221, 1229, 1234, 1237, 1255, 1262, 1274, 1288, 1292, 1296,1316, 1318, 1337, 1345, 1347, 1365, 1367, 1379, 1396, 1430, 1454, 1461, 1484, 1516, 1530, 1535, 1540, 1550, 1633,1641, 1646, 1655, 1674, 1694, 1700, 1736, 1789, 1793, 1809, 1812, 2082, 2092, 2104, 2143, 2225, 2242, 2248, 2347,2391

ER P7372 22-1124 0222-1161 0022-1209 0122-1240 00

08 JUL 08 AUTOFLIGHT - FMGC DEFINE AND INSTALL FMGC IAEC13043BA01 THALES(EQUIPPED WITH FMS2 THALES/SMITH)

Applicable to: MSN 1080, 1161, 1214, 1260, 1273, 1500, 1656, 1893, 1912, 1922, 1926, 1928, 1935, 1962, 1996,2016, 2023, 2029, 2032, 2041, 2045, 2070, 2073, 2077, 2079, 2088, 2094, 2097, 2107, 2110, 2121, 2135, 2138-2139,2156, 2161, 2164, 2190, 2193, 2195, 2204, 2211, 2216, 2226, 2247, 2254-2255, 2261, 2267, 2277, 2288, 2290,2296, 2302-2303, 2305, 2310, 2312-2313, 2320, 2323-2324, 2331, 2335, 2340-2341, 2348, 2351, 2359, 2362-2363,2366, 2376, 2383, 2389, 2396-2397, 2404-2405, 2410, 2414, 2417, 2422, 2429-2431, 2441, 2452, 2458-2459, 2462,2466-2468, 2480, 2482, 2509-2510, 2517, 2524, 2534, 2536, 2564, 2566, 2568, 2570, 2595, 2597, 2613, 2615,2630-2631, 2639, 2645, 2648, 2653, 2655, 2660, 2669, 2676, 2682, 2690, 2694, 2697, 2720, 2731-2732, 2738-2739,2747, 2753, 2775, 2799, 2808, 2813, 2828, 2833, 2840, 2844, 2863, 2874, 2883, 2908, 2911, 2914, 2922, 2943,2958, 2974, 2976, 2981, 2990, 2997, 3001, 3004-3005, 3011-3013, 3022, 3030, 3033, 3049-3050, 3062, 3066, 3071,3074, 3081, 3086, 3104, 3106, 3114, 3116, 3124, 3128, 3142, 3158-3159, 3162, 3167, 3172, 3183, 3192-3193, 3196,3198, 3210, 3214, 3216, 3219, 3227, 3235, 3244, 3252, 3254, 3259, 3264-3265, 3274, 3290, 3297, 3301, 3308,3314-3317, 3330, 3335, 3339, 3351-3352, 3355, 3357-3358, 3360, 3365, 3369, 3371, 3375, 3379, 3382, 3386-3387,3390, 3392, 3397, 3402, 3414, 3421, 3423-3424, 3434, 3437-3439, 3449, 3453-3454, 3457, 3462, 3468-3469, 3478,3481, 3483-3484, 3496-3497, 3499-3500, 3509, 3512, 3519-3520, 3524, 3526-3527, 3534, 3541, 3543, 3546, 3548,3550, 3561, 3570, 3575, 3578, 3580, 3583, 3585, 3600, 3602, 3606-3607, 3613-3614, 3618, 3621, 3625, 3635-3636,3641-3642, 3649-3650, 3669, 3676-3677, 3680, 3692, 3694, 3697, 3703, 3709, 3712, 3714, 3716, 3721, 3726, 3730,3737, 3740, 3745, 3753, 3759, 3768, 3773, 3782, 3785, 3793, 3796-3797, 3820-3821, 3829, 3839, 3841, 3849-3851,3858, 3862-3864, 3878, 3904, 3943-3944, 3591-3592, 3638, 3775, 3836, 3873, 3876, 3881, 3893, 3897, 3901,3911-3912, 3924, 3926, 3935-3937, 3960-3966, 3969, 3977, 3989-3996

E P7373 22-1130 0122-1176 0022-1193 0122-1217 03

08 JUL 08 AUTOFLIGHT - FMGC DEFINE AND INSTALL FMGC CFMC13043AA01 THALES(EQUIPPED WITH FMS2 THALES/SMITH)

Applicable to: MSN 0994, 1132, 1160, 1162, 1172, 1336-1337, 1388, 1660, 1766, 1774, 1796, 1800, 1810, 1812,1815, 1819-1820, 1824, 1828, 1833, 1839, 1841, 1851, 1853, 1859, 1863, 1870, 1875-1876, 1879, 1884, 1890, 1894,1897, 1901, 1923, 1938-1939, 1943, 1959, 1963, 1976, 1980, 1982, 1990-1991, 1997, 2002, 2010, 2012-2013, 2017,2019, 2026, 2028, 2030, 2033, 2035, 2039, 2047, 2051, 2057, 2059, 2064, 2071, 2074, 2076, 2081-2083, 2086-2087,2092, 2095, 2100-2101, 2103, 2109, 2113, 2122, 2127, 2140, 2142, 2158, 2166, 2186, 2189, 2198, 2207, 2209, 2213,2218, 2228, 2236, 2240-2241, 2253, 2258, 2260, 2276, 2278-2279, 2287, 2291, 2306, 2317-2318, 2332, 2344, 2346,2349-2350, 2369, 2373, 2382, 2390, 2392, 2400, 2406, 2425, 2448, 2456, 2464-2465, 2474, 2483, 2497, 2518,2529, 2539, 2557, 2561, 2581-2582, 2593, 2601, 2607, 2611-2612, 2617-2619, 2624, 2628-2629, 2632-2633, 2641,2644, 2654, 2656, 2662, 2665, 2668, 2672, 2683-2686, 2696, 2699-2700, 2705, 2707, 2712, 2716, 2721, 2726,2733, 2746, 2749-2751, 2760, 2762-2764, 2768, 2774, 2806, 2816, 2820, 2826, 2835-2836, 2841-2842, 2846, 2849,2853, 2857, 2865, 2867, 2869, 2878-2879, 2881-2882, 2885, 2891, 2895, 2902, 2905, 2907, 2909-2910, 2913, 2918,




M(1) MODIFICATION Linked SB Incorp. Date Title2925-2926, 2930-2932, 2935, 2937-2939, 2944, 2951, 2954-2956, 2961, 2964, 2966-2968, 2972-2973, 2975, 2980,2985, 2989, 2991, 2995, 3000, 3006, 3008-3009, 3014, 3018-3019, 3021, 3023-3024, 3027-3028, 3038, 3044, 3046,3051, 3055-3056, 3064-3065, 3068, 3070, 3076, 3079-3080, 3087, 3092-3093, 3096, 3098, 3100, 3107-3108, 3110,3115, 3117, 3121, 3130-3132, 3138-3140, 3146, 3149, 3153-3154, 3160-3161, 3163-3164, 3170-3171, 3173, 3178, 3182,3187-3188, 3194, 3197, 3199, 3201-3202, 3205-3206, 3212-3213, 3215, 3218, 3220-3221, 3223-3225, 3232-3234,3236, 3238, 3242-3243, 3245, 3247, 3249, 3256, 3260-3262, 3268, 3271, 3273, 3277, 3282, 3285-3286, 3288-3289,3291, 3295, 3299-3300, 3305-3307, 3309-3310, 3312, 3323, 3326-3329, 3331, 3337-3338, 3340, 3343-3344, 3346,3353, 3356, 3362-3364, 3366-3368, 3370, 3372, 3383, 3385, 3388-3389, 3394, 3399, 3401, 3403-3404, 3407, 3412,3415, 3419-3420, 3422, 3427, 3431, 3435, 3440-3441, 3444, 3446-3448, 3455-3456, 3461, 3464, 3470-3471, 3473,3476-3477, 3480, 3482, 3485-3486, 3489-3490, 3492, 3494, 3498, 3502, 3504-3506, 3508, 3514-3516, 3521, 3523,3528, 3530, 3532-3533, 3536, 3549, 3551, 3553, 3557, 3559-3560, 3563-3564, 3568, 3573, 3576, 3579, 3582,3584, 3586, 3589, 3593, 3596-3599, 3601, 3604-3605, 3609-3612, 3615-3616, 3619-3620, 3623, 3626, 3628-3629,3633, 3639, 3643, 3648, 3652-3653, 3655, 3657, 3661, 3665-3667, 3678-3679, 3682, 3687, 3689-3690, 3695-3696,3700-3701, 3704, 3706, 3708, 3715, 3722-3723, 3725, 3728-3729, 3731-3732, 3739, 3749, 3751-3752, 3756,3765-3766, 3769, 3776-3777, 3791-3792, 3795, 3798, 3802, 3806, 3809, 3813-3815, 3822, 3874-3875, 3883-3887,3891, 3903, 3698, 3758, 3818, 3825, 3827-3828, 3830-3831, 3833-3834, 3840, 3846, 3848, 3852-3853, 3855, 3859,3865-3866, 3872, 3879-3880, 3895-3896, 3898, 3900, 3906-3907, 3915, 3918, 3921, 3925, 3928-3932, 3940, 3945,3949-3950, 3955-3956, 3967, 3970-3971, 3983-3984

E P7519 22-1089 1022-1163 0022-1233 00

08 JUL 08 AUTOFLIGHT-FMGC-INSTALL FMGC CFM C13042AA01(EQUIPPED WITH FMS2) HONEYWELL

Applicable to: MSN 0134, 0136, 0143, 0146, 0158, 0173, 0176-0177, 0196, 0199, 0207, 0219, 0223-0224, 0240-0241,0264, 0274, 0300, 0312, 0323, 0328, 0365, 0383, 0501, 0507, 0531, 0658, 0669, 0685, 0941, 0961, 0992, 1002, 1021,1027, 1047, 1059, 1067, 1073, 1087, 1099, 1101, 1107, 1119, 1125, 1130, 1132, 1137, 1150, 1152, 1157, 1160, 1162,1172, 1179, 1184-1185, 1189, 1198, 1200, 1208, 1213, 1219, 1221, 1229, 1233, 1238, 1241-1242, 1244, 1250, 1255,1259, 1262, 1285, 1288, 1292, 1303, 1306, 1308-1309, 1318, 1320, 1322, 1336-1337, 1352, 1364-1365, 1367, 1377,1381, 1385-1387, 1390, 1394, 1396, 1402, 1405, 1413, 1416, 1429-1430, 1437, 1441, 1443, 1451, 1454, 1458, 1461,1467, 1470, 1478, 1484-1485, 1493, 1503-1504, 1516, 1530, 1540-1541, 1544, 1550-1551, 1553-1554, 1556, 1562,1564, 1571-1572, 1577-1578, 1588, 1592, 1597-1599, 1601-1603, 1605, 1607, 1611-1612, 1615, 1618, 1623, 1625,1629-1630, 1632, 1634, 1637-1638, 1657, 1660, 1668, 1673, 1678, 1686, 1706, 1712, 1717-1720, 1725-1726, 1735,1742, 1747-1748, 1750-1751, 1753, 1756-1757, 1762, 1765-1767, 1769, 1772, 1774-1775, 1777-1778, 1780, 1783,1786-1787, 1791, 1795-1797, 1800, 1805-1806, 1808, 1810-1812, 1815, 1819-1820, 1824, 1828, 1833, 1838-1839, 1841,1846, 1851-1853, 1859-1860, 1863-1864, 1866-1867, 1870, 1872, 1874-1876, 1879, 1881-1882, 1884, 1886-1887,1889-1890, 1894, 1897, 1901, 1905-1906, 1908, 1911, 1913, 1916, 1920-1921, 1923-1925, 1929-1932, 1936-1940,1942-1943, 1949, 1951, 1954, 1959-1961, 1963-1966, 1968, 1972-1973, 1975-1976, 1978, 1980-1983, 1988-1991,1994, 1997, 1999, 2001-2003, 2005, 2009-2013, 2017-2019, 2022, 2024-2026, 2028, 2030, 2033-2037, 2039, 2043,2046-2054, 2056-2057, 2059-2062, 2064-2066, 2068-2069, 2071-2072, 2074, 2076, 2078, 2081-2083, 2086-2087,2091-2093, 2095, 2100-2101, 2103-2104, 2106, 2109, 2113-2117, 2119-2120, 2122-2124, 2126-2127, 2129, 2131,2133-2134, 2140, 2142-2146, 2151, 2154-2155, 2158, 2162-2163, 2165-2166, 2170-2171, 2174-2176, 2178-2184,2186-2187, 2189, 2191, 2196, 2198-2199, 2206-2209, 2212-2214, 2217-2222, 2224-2225, 2227-2228, 2230, 2233,2235-2237, 2239-2245, 2248-2251, 2253, 2256, 2258, 2260, 2262, 2264-2266, 2269-2272, 2274, 2276, 2278-2279,2283, 2285, 2287, 2289, 2291, 2293-2294, 2298, 2300, 2306, 2309, 2311, 2315, 2317-2319, 2325, 2327-2328,2330, 2332-2333, 2337, 2342, 2344, 2346-2347, 2349-2350, 2353-2354, 2357-2358, 2360-2361, 2364-2365, 2367,2369-2370, 2373-2374, 2377-2378, 2380-2382, 2385, 2387-2388, 2390-2392, 2394, 2398-2400, 2402, 2406-2407,2409, 2411-2412, 2416, 2419-2420, 2425, 2427, 2432, 2436-2437, 2439-2440, 2442, 2446, 2448, 2450-2451,




M(1) MODIFICATION Linked SB Incorp. Date Title2456, 2460, 2463-2465, 2471-2472, 2474, 2477-2478, 2481, 2483-2484, 2486-2488, 2492-2495, 2497-2499, 2503,2506-2508, 2511-2512, 2514, 2516, 2518-2519, 2523, 2525, 2527-2529, 2532, 2538-2552, 2554-2558, 2561-2563,2565, 2569, 2575, 2578, 2581-2584, 2586, 2588, 2591-2593, 2596, 2599, 2601, 2605-2607, 2611-2612, 2616-2620,2623-2625, 2627-2629, 2632-2633, 2635-2638, 2641, 2644, 2646, 2652, 2654, 2656, 2658, 2662, 2665, 2668, 2672,2674-2675, 2677-2678, 2681, 2683-2686, 2691, 2693, 2695-2696, 2699-2700, 2702, 2705-2709, 2712, 2715-2716,2719, 2721, 2726-2727, 2729, 2733, 2735-2736, 2740, 2742-2746, 2748-2751, 2754, 2756-2758, 2760-2765,2768-2770, 2773-2774, 2776-2779, 2782, 2785-2786, 2788-2790, 2792, 2794-2796, 2798, 2800-2801, 2803,2805-2807, 2810-2812, 2816, 2818-2822, 2824-2827, 2829-2831, 2834-2837, 2839, 2841-2843, 2846-2847, 2849,2851-2855, 2857, 2860-2861, 2865-2867, 2869-2870, 2873, 2875-2879, 2881-2882, 2884-2885, 2889-2891, 2895,2897, 2899, 2902-2903, 2905, 2907, 2909-2910, 2912-2913, 2915, 2918, 2920-2921, 2923-2926, 2930-2932, 2935,2937-2939, 2944, 2946-2947, 2949-2951, 2954-2957, 2959-2962, 2964-2968, 2972-2973, 2975, 2980, 2985-2986,2988-2989, 2991, 2993-2996, 2998, 3000, 3002-3003, 3006, 3008-3009, 3014, 3016, 3018-3019, 3021, 3023-3025,3027-3028, 3031, 3035-3038, 3040-3041, 3043-3044, 3046-3048, 3051-3056, 3058-3061, 3063-3065, 3068,3070, 3073, 3076, 3078-3080, 3082-3085, 3087-3088, 3090, 3092-3102, 3107-3111, 3115, 3117-3118, 3121-3123,3129-3140, 3145-3149, 3151-3155, 3157, 3160-3161, 3163-3164, 3168-3171, 3173-3174, 3176, 3178-3182, 3184,3186-3189, 3191, 3194, 3197, 3199, 3201-3206, 3209, 3211-3213, 3215, 3218, 3220-3221, 3223-3226, 3230,3232-3234, 3236-3238, 3240, 3242-3243, 3245-3247, 3249-3250, 3255-3256, 3260-3262, 3266-3268, 3271-3273,3277-3278, 3281-3282, 3284-3286, 3288-3289, 3291, 3293, 3295, 3298-3300, 3304-3307, 3309-3310, 3312-3313,3318, 3320-3321, 3323-3329, 3331, 3333-3334, 3336-3338, 3340, 3343-3347, 3349, 3353, 3356, 3359, 3361-3364,3366-3368, 3370, 3372-3374, 3376-3377, 3380, 3383, 3385, 3388-3389, 3391, 3394, 3396, 3398-3401, 3403-3404,3406-3408, 3410-3413, 3415, 3417, 3419-3420, 3422, 3425-3427, 3431-3433, 3435-3436, 3440-3448, 3452,3455-3456, 3460-3461, 3464-3467, 3470-3473, 3475-3477, 3480, 3482, 3485-3487, 3489-3490, 3492, 3494, 3498,3501-3506, 3508, 3511, 3513-3516, 3518, 3521, 3523, 3528-3530, 3532-3533, 3536-3537, 3540, 3542, 3544-3545,3549, 3551, 3553, 3555, 3557, 3559-3560, 3563-3565, 3568-3569, 3571, 3573-3574, 3576, 3579, 3582, 3584, 3586,3589, 3593-3594, 3596-3599, 3601, 3604-3605, 3608-3612, 3615-3617, 3619-3620, 3623, 3626-3634, 3639-3640,3643-3644, 3646-3648, 3651-3653, 3655-3658, 3660-3662, 3664-3667, 3670, 3675, 3678-3679, 3682-3684,3686-3687, 3689-3691, 3695-3696, 3704, 3706, 3708, 3711, 3715, 3720, 3722-3723, 3725, 3727-3729, 3731-3733,3735, 3739, 3742, 3744, 3746-3747, 3749-3752, 3754-3756, 3762-3763, 3765-3767, 3769, 3774, 3776-3778,3780-3781, 3786-3792, 3794-3795, 3798-3799, 3802, 3805-3806, 3808-3810, 3813-3815, 3817-3819, 3822-3828,3838, 3843-3846, 3871-3872, 3874-3875, 3891-3892, 3903, 3698-3702, 3758, 3830-3831, 3833-3835, 3840, 3848,3852-3857, 3859, 3861, 3865-3866, 3868, 3879-3880, 3882-3889, 3894-3896, 3898, 3900, 3905-3909, 3913-3915,3918-3919, 3921-3923, 3925, 3928-3933, 3939-3940, 3945-3946, 3949-3950, 3952-3956, 3967, 3970-3972,3983-3984

E P7520 22-1090 1122-1235 01

08 JUL 08 AUTOFLIGHT-FMGC-INSTALL FMGC IAE C13042BA01(EQUIPPED WITH FMS2 HONEYWELL)

Applicable to: MSN 0910, 0913, 0976, 1010, 1053, 1066, 1080, 1092, 1096, 1103, 1113, 1123, 1139-1140, 1143, 1156,1158-1159, 1161, 1173, 1183, 1188, 1195, 1212, 1214, 1235, 1240, 1246, 1251, 1253, 1256-1257, 1260, 1270, 1273,1276, 1280, 1300, 1302, 1304, 1327, 1332-1335, 1339, 1349, 1351, 1353, 1355, 1366, 1368, 1376, 1383, 1398, 1400,1407-1408, 1411, 1438, 1446, 1452, 1464, 1468, 1482, 1486, 1491, 1497, 1500, 1506, 1509, 1512, 1518, 1523, 1526,1528, 1546, 1548, 1557, 1568, 1575, 1580, 1587, 1589, 1591, 1593, 1595-1596, 1608, 1610, 1613-1614, 1619, 1624,1626, 1628, 1631, 1642, 1650, 1652, 1656, 1663, 1672, 1675-1676, 1682, 1695, 1703, 1705, 1707, 1721, 1727, 1730,1739, 1749, 1763, 1771, 1776, 1784-1785, 1788, 1794, 1798, 1801-1802, 1804, 1807, 1817-1818, 1823, 1825-1827,1831-1832, 1835, 1837, 1843, 1848-1849, 1854-1858, 1861-1862, 1868-1869, 1877-1878, 1880, 1888, 1891, 1893,1896, 1898-1899, 1902-1904, 1907, 1909-1910, 1912, 1914-1915, 1917-1918, 1922, 1926-1928, 1933-1935, 1941,1944-1948, 1950, 1952-1953, 1955-1958, 1962, 1967, 1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996,




M(1) MODIFICATION Linked SB Incorp. Date Title1998, 2000, 2004, 2006-2008, 2014-2016, 2020-2021, 2023, 2027, 2029, 2031-2032, 2038, 2040-2042, 2044-2045,2055, 2058, 2063, 2067, 2070, 2073, 2075, 2077, 2079-2080, 2084-2085, 2088-2090, 2094, 2096-2099, 2102, 2105,2107-2108, 2110-2112, 2118, 2121, 2125, 2128, 2130, 2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157,2159-2161, 2164, 2167-2169, 2172-2173, 2177, 2185, 2188, 2190, 2192-2195, 2197, 2200-2205, 2210-2211, 2215-2216,2223, 2226, 2229, 2231-2232, 2234, 2238, 2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263, 2267-2268,2273, 2275, 2277, 2280-2282, 2284, 2286, 2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310,2312-2314, 2316, 2320-2324, 2326, 2329, 2331, 2334-2336, 2338-2341, 2343, 2345, 2348, 2351-2352, 2355-2356,2359, 2362-2363, 2366, 2368, 2371-2372, 2375-2376, 2379, 2383-2384, 2386, 2389, 2393, 2395-2397, 2401,2403-2405, 2408, 2410, 2413-2415, 2417-2418, 2421-2424, 2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445,2447, 2449, 2452-2455, 2457-2459, 2461-2462, 2466-2470, 2473, 2475-2476, 2479-2480, 2482, 2485, 2489-2491,2496, 2501-2502, 2504-2505, 2509-2510, 2513, 2515, 2517, 2520-2522, 2524, 2526, 2530-2531, 2533-2537, 2553,2559-2560, 2564, 2566-2568, 2570-2574, 2576-2577, 2579-2580, 2585, 2587, 2589-2590, 2594-2595, 2597-2598,2600, 2602-2604, 2608-2610, 2613-2615, 2621-2622, 2626, 2630-2631, 2634, 2639-2640, 2642-2643, 2645,2647-2651, 2653, 2655, 2657, 2659-2661, 2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682,2687-2690, 2692, 2694, 2697-2698, 2701, 2703-2704, 2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728,2730-2732, 2734, 2737-2739, 2741, 2747, 2752-2753, 2755, 2759, 2766-2767, 2771-2772, 2775, 2780-2781,2783-2784, 2787, 2791, 2793, 2797, 2799, 2802, 2804, 2808-2809, 2813-2815, 2817, 2823, 2828, 2832-2833, 2838,2840, 2844-2845, 2848, 2850, 2856, 2858-2859, 2862-2864, 2868, 2871-2872, 2874, 2880, 2883, 2886-2888,2892-2894, 2896, 2898, 2900-2901, 2904, 2906, 2908, 2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934,2936, 2940-2943, 2945, 2948, 2952-2953, 2958, 2963, 2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992,2997, 2999, 3001, 3004-3005, 3007, 3010-3013, 3015, 3017, 3020, 3022, 3026, 3029-3030, 3032-3034, 3039, 3042,3045, 3049-3050, 3057, 3062, 3066-3067, 3069, 3071-3072, 3074-3075, 3077, 3081, 3086, 3089, 3091, 3103-3106,3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159, 3162, 3165-3167, 3172, 3175, 3177,3183, 3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3214, 3216-3217, 3219, 3222, 3227-3229,3231, 3235, 3239, 3241, 3244, 3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270, 3274-3276, 3279-3280, 3283,3287, 3290, 3292, 3294, 3296-3297, 3301-3303, 3308, 3311, 3314-3317, 3319, 3322, 3330, 3332, 3335, 3339,3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365, 3369, 3371, 3375, 3378-3379, 3381-3382, 3384,3386-3387, 3390, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424, 3428-3430, 3434,3437-3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468-3469, 3474, 3478-3479, 3481, 3483-3484, 3488,3491, 3493, 3495-3497, 3499-3500, 3507, 3509-3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531, 3534-3535,3538-3539, 3541, 3543, 3546-3548, 3550, 3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572, 3575,3577-3578, 3580-3581, 3583, 3585, 3587-3588, 3590-3592, 3595, 3600, 3602-3603, 3606-3607, 3613-3614, 3618,3621-3622, 3624-3625, 3635-3638, 3641-3642, 3645, 3649-3650, 3654, 3659, 3663, 3668-3669, 3671-3674,3676-3677, 3680-3681, 3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721,3724, 3726, 3730, 3734, 3736-3738, 3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773,3779, 3782-3785, 3793, 3796-3797, 3800-3801, 3803-3804, 3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839,3841, 3847, 3849-3851, 3858, 3860, 3862-3864, 3867, 3890, 3904, 3920, 3775, 3836-3837, 3869, 3873, 3876-3878,3881, 3893, 3897, 3899, 3901-3902, 3910-3912, 3916-3917, 3924, 3926-3927, 3934-3938, 3941-3944, 3947-3948,3951, 3959-3966, 3968-3969, 3977-3981, 3989-3996




M(1) MODIFICATION Linked SB Incorp. Date TitleER P7666 22-1103 04

22-1116 0422-1124 0222-1130 0122-1152 0322-1153 0122-1161 0022-1176 0022-1180 0022-1193 0122-1197 0222-1209 0122-1217 0322-1218 0122-1219 0122-1240 00

08 JUL 08 AUTO FLIGHT - FMGC DEVELOP FMS 2NDGENERATION THALES/SMITH REV 1 STANDARD

Applicable to: MSN 0002-0021, 0031-0034, 0040-0041, 0044, 0052-0055, 0061-0067, 0076-0077, 0081-0082, 0091,0098-0102, 0108, 0112, 0115, 0118-0119, 0121, 0123-0125, 0128-0131, 0133, 0144-0145, 0152-0153, 0155-0156,0160, 0165-0166, 0171, 0178, 0184, 0186-0188, 0192, 0194, 0197-0198, 0203-0206, 0208, 0211, 0213-0215, 0220,0226-0228, 0235-0239, 0244, 0262-0263, 0270-0273, 0278, 0281-0282, 0285-0287, 0297-0299, 0306-0307,0317-0319, 0322, 0329, 0337, 0339-0340, 0351-0352, 0355, 0358, 0360, 0366-0367, 0370, 0372, 0377, 0380-0381,0387-0388, 0390, 0399-0400, 0402, 0408, 0410, 0417-0418, 0448, 0455, 0471, 0491, 0498, 0509, 0511, 0521, 0527,0529, 0544, 0584, 0598, 0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0680, 0687, 0715, 0725, 0764, 0766,0777-0778, 0786, 0796, 0801-0802, 0807, 0818, 0830, 0832, 0844, 0846, 0861, 0863, 0868-0869, 0880, 0885, 0890,0896, 0903-0904, 0907, 0911, 0922-0923, 0929, 0938, 0958, 0962, 0964, 0972, 0975, 0981, 0985, 0988, 0994,0996-0998, 1000, 1011, 1019-1020, 1025, 1033, 1036-1038, 1040, 1042, 1044, 1046, 1048, 1051-1052, 1055, 1058,1061-1062, 1065, 1069, 1071, 1077-1078, 1080, 1082, 1084, 1089-1091, 1095, 1097, 1102, 1109, 1112, 1114-1115,1118, 1121-1122, 1126, 1129, 1131-1136, 1141-1142, 1147-1149, 1151, 1155, 1160-1162, 1164, 1167, 1169-1170, 1172,1175-1176, 1182, 1187, 1190-1191, 1193-1194, 1197, 1201, 1203-1205, 1214-1216, 1222, 1224-1225, 1227, 1230,1232, 1236, 1239, 1245, 1249, 1254, 1258, 1260-1261, 1264-1265, 1267-1269, 1271, 1273, 1275, 1277-1279, 1283,1287, 1289, 1294-1295, 1297-1299, 1301, 1305, 1310-1311, 1313-1315, 1317, 1319, 1324-1326, 1328-1329, 1331,1336-1338, 1340, 1342, 1344, 1346, 1348, 1354, 1356, 1358, 1360, 1369, 1371, 1378, 1380, 1382, 1384, 1388-1389,1391-1393, 1403-1404, 1406, 1410, 1412, 1414-1415, 1417, 1419, 1423, 1425, 1428, 1431, 1433-1434, 1436, 1440,1442, 1444-1445, 1447, 1449, 1453, 1455-1456, 1462-1463, 1465-1466, 1471-1472, 1476, 1479, 1481, 1483, 1488,1490, 1492, 1494, 1496, 1498-1502, 1505, 1510-1511, 1513, 1515, 1517, 1519-1521, 1524-1525, 1527, 1529, 1531,1534-1537, 1539, 1543, 1547, 1549, 1552, 1558, 1560, 1563, 1565-1567, 1570, 1574, 1576, 1579, 1582-1583, 1590,1594, 1604, 1606, 1616, 1621-1622, 1633, 1636, 1640-1641, 1643-1646, 1648, 1651, 1656, 1658-1662, 1665-1666,1670, 1677, 1683-1685, 1687, 1689-1691, 1693, 1696, 1699-1701, 1704, 1708-1711, 1714-1715, 1722-1724, 1733-1734,1738, 1740, 1743-1746, 1752, 1754, 1758-1761, 1764, 1766, 1770, 1773-1774, 1779, 1781-1782, 1789-1790, 1792,1796, 1800, 1803, 1810, 1812-1815, 1819-1820, 1824, 1828-1829, 1833, 1839, 1841, 1844, 1850-1851, 1853, 1859,1863, 1869-1871, 1873, 1875-1876, 1879, 1883-1885, 1890, 1893-1895, 1897, 1899-1901, 1907, 1910, 1912, 1918,1922-1924, 1926, 1928, 1935, 1938-1939, 1943, 1949, 1957-1959, 1962-1963, 1969, 1976, 1980, 1982, 1990-1993,1996-1997, 2002, 2010, 2012-2013, 2016-2017, 2019, 2023, 2026, 2028-2030, 2032-2033, 2035, 2038-2041, 2045,2047, 2051, 2057, 2059, 2064, 2070-2071, 2073-2074, 2076-2077, 2079, 2081-2083, 2086-2088, 2092, 2094-2095,2097-2098, 2100-2101, 2103, 2107, 2109-2110, 2113, 2121-2122, 2127, 2135, 2137-2140, 2142, 2156-2158, 2161, 2164,2166, 2186, 2188-2190, 2193-2195, 2198, 2204, 2207, 2209, 2211, 2213, 2216, 2218, 2226, 2228, 2236, 2240-2241,




M(1) MODIFICATION Linked SB Incorp. Date Title2247, 2253-2255, 2258, 2260-2261, 2267, 2276-2279, 2287-2288, 2290-2291, 2296, 2302-2303, 2305-2306, 2310,2312-2313, 2317-2318, 2320, 2323-2324, 2331-2332, 2335, 2340-2341, 2344, 2346, 2348-2351, 2359, 2362-2363,2366, 2369, 2373, 2376, 2382-2383, 2389-2390, 2392, 2396-2397, 2400, 2404-2406, 2410, 2414, 2417, 2422,2425, 2429-2431, 2441, 2448, 2452, 2456, 2458-2459, 2462, 2464-2468, 2474, 2480, 2482-2483, 2497, 2509-2510,2517-2518, 2524, 2529, 2534, 2536, 2539, 2557, 2561, 2564, 2566, 2568, 2570, 2581-2582, 2593, 2595, 2597,2601, 2607, 2611-2613, 2615, 2617-2619, 2624, 2628-2633, 2639, 2641, 2644-2645, 2648, 2653-2656, 2660, 2662,2665, 2668-2669, 2672, 2676, 2682-2686, 2690, 2694, 2696-2697, 2699-2700, 2705, 2707, 2712, 2716, 2720-2721,2726, 2731-2733, 2738-2739, 2746-2747, 2749-2751, 2753, 2760, 2762-2764, 2768, 2774-2775, 2799, 2806, 2808,2813, 2816, 2820, 2826, 2828, 2833, 2835-2836, 2840-2842, 2844, 2846, 2849, 2853, 2857, 2863, 2865, 2867,2869, 2874, 2878-2879, 2881-2883, 2885, 2891, 2895, 2902, 2905, 2907-2911, 2913-2914, 2918, 2922, 2925-2926,2930-2932, 2935, 2937-2939, 2943-2944, 2951, 2954-2956, 2958, 2961, 2964, 2966-2968, 2972-2976, 2980-2981,2985, 2989-2991, 2995, 2997, 3000-3001, 3004-3006, 3008-3009, 3011-3014, 3018-3019, 3021-3024, 3027-3028,3030, 3033, 3038, 3044, 3046, 3049-3051, 3055-3056, 3062, 3064-3066, 3068, 3070-3071, 3074, 3076, 3079-3081,3086-3087, 3092-3093, 3096, 3098, 3100, 3104, 3106-3108, 3110, 3114-3117, 3121, 3124, 3128, 3130-3132, 3138-3140,3142, 3146, 3149, 3153-3154, 3158-3164, 3167, 3170-3173, 3178, 3182-3183, 3187-3188, 3192-3194, 3196-3199,3201-3202, 3205-3206, 3210, 3212-3216, 3218-3221, 3223-3225, 3227, 3232-3236, 3238, 3242-3245, 3247, 3249,3252, 3254, 3256, 3259-3262, 3264-3265, 3268, 3271, 3273-3274, 3277, 3282, 3285-3286, 3288-3291, 3295,3297, 3299-3301, 3305-3310, 3312, 3314-3317, 3323, 3326-3331, 3335, 3337-3340, 3343-3344, 3346, 3351-3353,3355-3358, 3360, 3362-3372, 3375, 3379, 3382-3383, 3385-3390, 3392, 3394, 3397, 3399, 3401-3404, 3407,3412, 3414-3415, 3419-3424, 3427, 3431, 3434-3435, 3437-3441, 3444, 3446-3449, 3453-3457, 3461-3462, 3464,3468-3471, 3473, 3476-3478, 3480-3486, 3489-3490, 3492, 3494, 3496-3500, 3502, 3504-3506, 3508-3509,3512, 3514-3516, 3519-3521, 3523-3524, 3526-3528, 3530, 3532-3534, 3536, 3541, 3543, 3546, 3548-3551, 3553,3557, 3559-3561, 3563-3564, 3568, 3570, 3573, 3575-3576, 3578-3580, 3582-3586, 3589, 3596-3602, 3604-3607,3609-3616, 3618-3621, 3623, 3625-3626, 3628-3629, 3633, 3635-3636, 3641-3643, 3648-3650, 3652-3653, 3655,3657, 3661, 3665-3667, 3669, 3676-3680, 3682, 3687, 3689-3690, 3692, 3694-3698, 3700-3701, 3703-3704, 3706,3708-3709, 3712, 3714-3716, 3721-3723, 3725-3726, 3728-3732, 3737, 3739-3740, 3745, 3749, 3751-3753, 3756,3765-3766, 3768-3769, 3773, 3782, 3785, 3791-3793, 3795-3798, 3802, 3806, 3809, 3813-3815, 3820-3822,3839-3841, 3858-3859, 3862-3866, 3878-3881, 3883-3887, 3891, 3903-3904, 3943-3945, 3591-3593, 3638-3639,3758-3759, 3775-3777, 3818, 3825, 3827-3831, 3833-3834, 3836, 3846, 3848-3853, 3855, 3872-3876, 3893,3895-3898, 3900-3901, 3906-3907, 3911-3912, 3915, 3918, 3921, 3924-3926, 3928-3932, 3935-3937, 3940,3949-3950, 3955-3956, 3960-3967, 3969-3971, 3977, 3983-3996

ER P7706 22-1109 00 08 JUL 08 AUTOFLIGHT-FMGC-RE-INSTALL FMS1 CFM P/NB546CAM0103 (ANTI MOD 31896) (CFM GPS+ACARS)

Applicable to: MSN 1753, 1924, 1949, 2104, 2115, 2143P7707 08 JUL 08 AUTOFLIGHT-FMGC-RE-INSTALL FMS1 IAE P/N

B546CCM0105 (ANTI MOD 31897) (IAE GPS+ACARS)Applicable to: MSN 1869, 1899, 1902, 1907, 1910, 1918, 1957-1958, 1969, 1987, 1993, 2038, 2040, 2058, 2098, 2137,2157, 2188, 2194, 2252

E P7721 32-1247 02 08 JUL 08 LANDING GEAR-WHEELS AND BRAKES-CANCELMIXABILITY BETWEEN GOODRICH BRAKES 2-1600-2AND -3 AUTHOR. WITH MOD 31803

Applicable to: MSN 0031, 0034, 0040-0041, 0052-0055, 0059, 0064-0068, 0073, 0076-0077, 0081-0082, 0084,0091, 0098-0099, 0118, 0121-0122, 0125-0127, 0141, 0149-0150, 0152-0154, 0159-0160, 0171, 0183, 0185, 0192,0197, 0206, 0208, 0213, 0233, 0242, 0248, 0252-0255, 0259-0263, 0265, 0272-0273, 0275-0277, 0279-0282,0290, 0296-0298, 0306-0307, 0310-0311, 0317-0321, 0324, 0329-0330, 0333, 0339-0342, 0347, 0350, 0353-0355,




M(1) MODIFICATION Linked SB Incorp. Date Title0357-0360, 0367-0368, 0372, 0378, 0380-0381, 0384, 0387-0388, 0393, 0399-0400, 0408, 0410-0411, 0417-0418,0422, 0426, 0428, 0435, 0439, 0442, 0448, 0450, 0452, 0454-0457, 0460-0465, 0467, 0470-0472, 0475, 0479-0480,0483, 0485, 0487, 0489, 0500, 0503-0504, 0506, 0508, 0510, 0512, 0523, 0527-0528, 0530, 0539, 0546, 0558,0561, 0568, 0571-0572, 0584, 0587, 0589, 0592, 0613, 0624, 0626, 0628, 0630, 0634, 0638-0639, 0649, 0655-0656,0670, 0672, 0678, 0682-0683, 0686, 0688, 0690-0691, 0693, 0695, 0697, 0702, 0711, 0714, 0716, 0719, 0721, 0728,0730, 0732-0733, 0735-0736, 0739-0743, 0747-0748, 0751-0752, 0756-0757, 0759, 0762, 0764, 0766, 0769-0770,0773, 0778-0780, 0783-0786, 0788, 0798, 0800-0801, 0803-0805, 0807, 0812-0813, 0816-0818, 0820, 0824-0826,0829-0832, 0834, 0836, 0840, 0842-0847, 0850-0851, 0856, 0858, 0861-0863, 0865-0868, 0871, 0873-0874, 0877,0882, 0885, 0889-0890, 0893, 0896, 0898, 0902-0904, 0907, 0911-0912, 0922-0924, 0929-0931, 0936, 0944, 0946,0948-0949, 0952-0953, 0955, 0962, 0964-0965, 0972, 0978, 0980-0981, 0988-0989, 0996-0997, 1001, 1003, 1011,1019, 1022, 1031, 1033, 1037-1038, 1040, 1043-1044, 1046, 1049-1052, 1055-1056, 1058, 1061-1062, 1064-1066,1069, 1071, 1075, 1077-1079, 1083-1084, 1088-1091, 1095, 1097, 1104-1105, 1109-1114, 1116, 1122, 1126, 1128-1129,1131, 1134-1136, 1140-1141, 1146-1149, 1155, 1159, 1163-1164, 1166-1167, 1170-1171, 1178, 1182, 1191-1192, 1194,1203, 1205, 1209-1211, 1213, 1223-1224, 1230, 1234, 1242-1243, 1245, 1248-1249, 1253-1254, 1263-1266, 1268-1269,1272, 1274-1275, 1277, 1281-1282, 1284, 1286-1287, 1289-1291, 1294, 1297-1298, 1300-1301, 1304, 1306, 1310-1311,1313-1315, 1317, 1319-1321, 1323-1326, 1328, 1331-1332, 1334, 1339-1343, 1346, 1348, 1350-1351, 1353-1355,1358-1360, 1363, 1369, 1371, 1373-1375, 1378, 1382, 1389, 1391-1395, 1397, 1400-1401, 1406, 1409-1410, 1414,1419-1420, 1426-1427, 1432, 1434-1435, 1443, 1453, 1456, 1460, 1463, 1467, 1469, 1474-1475, 1477, 1482-1483,1488, 1490-1491, 1495, 1498, 1500-1501, 1507-1509, 1512, 1514-1515, 1520, 1522-1523, 1526-1527, 1533-1535, 1538,1543, 1545, 1547-1549, 1552, 1555, 1559-1560, 1562-1565, 1567, 1569-1571, 1573, 1575-1577, 1579, 1581-1586,1600, 1605, 1609, 1615, 1617-1618, 1620, 1624, 1627, 1630, 1633-1634, 1637, 1641, 1646-1647, 1649, 1653, 1659,1662, 1664, 1668-1669, 1671, 1673, 1676, 1680, 1683-1685, 1688, 1693, 1702, 1709, 1714, 1718-1719, 1721, 1725,1728, 1730-1731, 1737-1738, 1741-1743, 1746-1747, 1751-1752, 1755-1756, 1758-1759, 1761, 1765-1766, 1774,1777, 1781, 1789-1790, 1796, 1800, 1803, 1805, 1810, 1812, 1815, 1819-1821, 1824, 1828, 1833, 1839-1842, 1845,1847, 1851, 1853, 1860, 1863-1867, 1870, 1872, 1874-1876, 1882, 1886, 1890, 1893, 1897, 1912, 1922-1923, 1925,1929, 1934-1935, 1940, 1943, 1952, 1959, 1962-1963, 1968, 1971, 1976, 1980, 1982, 1986, 1990, 1997, 2002, 2004,2008, 2010, 2012-2013, 2018-2019, 2026, 2028-2030, 2037, 2039, 2043, 2047-2048, 2050, 2052-2053, 2062, 2066,2069, 2072, 2077-2078, 2082, 2084, 2087, 2089, 2091-2093, 2095-2096, 2102-2103, 2106, 2116, 2118-2120, 2126,2129, 2133, 2144-2145, 2151, 2163, 2169-2170, 2175-2176, 2179-2181, 2184-2185, 2187, 2191, 2193, 2196-2198,2206, 2209, 2214, 2217, 2222, 2224, 2229-2230, 2233, 2236, 2238, 2240-2241, 2243, 2245, 2249-2251, 2253, 2256,2258, 2260, 2265, 2268, 2271-2272, 2276-2277, 2281-2283, 2287, 2289, 2292, 2294-2296, 2299-2302, 2304, 2308,2312, 2316, 2318-2319, 2321-2322, 2325-2329, 2333, 2335, 2338, 2353, 2355-2356, 2358-2360, 2362, 2364, 2367,2369-2370, 2372-2375, 2377-2380, 2383, 2385, 2387, 2392-2396, 2398-2402, 2404-2406, 2409, 2411-2412, 2414,2418, 2420, 2422-2423, 2427-2428, 2430-2432, 2434, 2436, 2438, 2441-2442, 2444, 2446, 2448, 2450, 2452-2453,2455, 2457-2458, 2460, 2463-2465, 2467-2469, 2471, 2474-2475, 2477, 2481-2483, 2486-2487, 2492, 2495, 2497,2501, 2503, 2512, 2514-2516, 2518, 2523, 2526-2528, 2537-2538, 2542, 2544, 2548, 2552, 2556, 2565, 2570,2572-2573, 2575, 2578, 2583, 2585-2588, 2595, 2600, 2604-2605, 2608, 2613, 2615, 2618, 2625, 2630, 2635-2636,2638, 2641-2642, 2646, 2651, 2657, 2662, 2666, 2669, 2677, 2681, 2690-2691, 2700, 2702-2703, 2709, 2715, 2717,2727, 2729, 2735, 2742, 2744, 2751, 2754, 2763, 2765-2766, 2769, 2771, 2777, 2779-2780, 2782, 2786-2788,2790-2791, 2795, 2803, 2806, 2810, 2812-2813, 2818, 2821, 2827, 2829, 2831, 2833, 2836, 2852, 2854, 2857, 2860,2866, 2873, 2875-2876, 2884, 2917, 2920, 2923, 2946-2947, 2959, 2976, 2979, 2987, 2994, 2997, 3003, 3011, 3028,3036, 3038, 3041-3042, 3045, 3048, 3052-3053, 3057, 3059, 3061, 3063, 3069, 3077, 3082, 3084, 3088, 3090, 3092,3103, 3110, 3113, 3118, 3122-3123, 3128-3129, 3134, 3136-3137, 3157, 3163, 3172, 3175-3176, 3184, 3193, 3248,3253, 3272, 3276, 3279, 3281, 3298, 3304, 3318, 3336, 3345, 3352, 3358, 3373-3375, 3378, 3389, 3408, 3410-3411,3413, 3418, 3426, 3431-3433, 3442, 3450, 3463, 3466-3467, 3472, 3474, 3487, 3491, 3495, 3500-3501, 3510-3511,3518, 3534, 3537-3538, 3544-3545, 3547, 3555, 3569, 3571, 3574, 3577, 3581, 3590, 3608, 3624, 3627, 3631, 3634,




M(1) MODIFICATION Linked SB Incorp. Date Title3640, 3644, 3646-3647, 3664, 3668, 3672, 3675, 3683, 3691, 3699, 3702, 3705, 3711, 3720, 3735, 3742-3743,3746, 3754, 3762-3763, 3767, 3774, 3778, 3783, 3786, 3788-3790, 3794, 3799, 3805, 3808, 3810, 3823-3824, 3835,3838-3839, 3841-3845, 3854, 3871, 3888, 3857, 3905, 3909, 3913, 3917, 3922-3923, 3946, 3953-3954

E P7790 22-1123 05 08 JUL 08 AUTO FLIGHT - FLIGHT MANAGEMENT AND GUIDANCESYSTEM - ACTIVATE FMA ENHANCEMENT FUNCTION

Applicable to: MSN 0002-0021, 0033, 0044, 0061-0063, 0100-0102, 0108, 0115, 0128-0131, 0133, 0144-0145,0155-0156, 0184, 0186-0188, 0203, 0214-0215, 0220, 0226-0228, 0235-0239, 0244, 0270, 0278, 0285-0287, 0337,0352, 0377, 0491, 0498, 0509, 0521, 0529, 0544, 0598, 0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0777, 0796,0938, 0985, 0998, 1000, 1020, 1025, 1036, 1133, 1137, 1150-1151, 1189-1190, 1201, 1216, 1267, 1271, 1299, 1344,1387, 1404, 1415, 1444, 1449, 1458, 1471, 1476, 1478, 1502, 1505, 1524, 1599, 1616, 1622, 1640, 1645, 1658, 1660,1677, 1691, 1699, 1733, 1794, 1859, 1873, 1878-1879, 1885, 1894, 1900, 1924, 1928, 1938-1939, 1949, 1951-1953,1956, 1967, 1977, 1991, 2015, 2017, 2019, 2021, 2023-2026, 2028, 2030, 2032-2033, 2035, 2037, 2039, 2041,2043, 2045, 2047, 2050-2053, 2055, 2057, 2059-2060, 2062, 2064, 2066-2067, 2069, 2071-2072, 2074, 2076-2103,2105-2136, 2138-2142, 2144-2156, 2158-2224, 2226-2241, 2243-2247, 2249-2251, 2253-2310, 2312-2380, 2382-2390,2392-2471, 2473-2487, 2489-2562, 2564-2598, 2600-3996

E P7876 73-1075 01 08 JUL 08 ENGINE FUEL AND CONTROL - CONTROLLING -INTRODUCE EEC SOFTWARE STANDARD "SCN17" ONV2500-A5 ENGINES

Applicable to: MSN 0364, 0385, 0412, 0425, 0435, 0439, 0442, 0448, 0450, 0452-0458, 0460-0465, 0468,0470-0475, 0479, 0483-0485, 0487, 0489, 0493, 0496, 0500, 0502-0506, 0508, 0510, 0512, 0518, 0523, 0527, 0530,0538-0540, 0542-0543, 0550-0551, 0555-0558, 0560-0561, 0563-0565, 0567-0568, 0571, 0573, 0575, 0580, 0582,0584, 0587, 0589, 0591-0592, 0595, 0597, 0604, 0606, 0613-0614, 0620, 0631-0633, 0638, 0640, 0652, 0655,0659, 0661, 0663, 0667-0668, 0676, 0678, 0680, 0683, 0686-0687, 0690, 0692, 0696, 0698-0699, 0702, 0704-0705,0709-0710, 0712, 0715, 0718, 0720, 0722, 0725, 0731, 0733, 0739, 0741, 0743, 0746-0748, 0751, 0756, 0758-0760,0762, 0770-0771, 0780, 0783-0784, 0787-0788, 0791-0792, 0798, 0802-0806, 0810-0812, 0816, 0820, 0822,0824-0826, 0834-0836, 0839, 0842-0843, 0847, 0849-0851, 0855-0859, 0862, 0864-0867, 0871-0874, 0877-0878,0881-0882, 0886-0887, 0889, 0892-0893, 0895, 0898-0902, 0908, 0910, 0912-0913, 0915-0916, 0918-0919,0924, 0927-0928, 0930-0932, 0934, 0943-0944, 0948, 0950, 0952-0955, 0963, 0965-0966, 0968-0969, 0974,0976-0977, 0980, 0983, 0989-0990, 0993, 1001, 1003-1004, 1007-1008, 1010, 1013-1015, 1022, 1024, 1031-1032,1035, 1039, 1042-1043, 1045, 1049-1050, 1053, 1056-1057, 1060, 1064, 1066, 1074-1076, 1079-1080, 1082-1083,1085, 1088, 1092, 1096, 1098, 1103-1105, 1110-1111, 1113, 1115-1118, 1123, 1128, 1139-1140, 1142-1143, 1146,1153, 1156, 1158-1159, 1161, 1163, 1166, 1173-1174, 1177-1178, 1183, 1188, 1192-1197, 1199, 1202, 1204, 1207,1211-1212, 1214-1215, 1218, 1222-1223, 1225, 1227-1228, 1232, 1234-1236, 1239-1240, 1243, 1246, 1248, 1251,1253, 1256-1258, 1260-1261, 1266, 1270, 1272-1274, 1276, 1279-1282, 1284, 1290-1291, 1293, 1295, 1300, 1302,1304, 1321, 1323, 1327, 1329, 1332-1335, 1338-1339, 1341, 1343, 1349-1351, 1353, 1355-1356, 1359, 1363, 1366,1368, 1373-1376, 1380, 1383-1384, 1395, 1397-1398, 1400-1401, 1406-1411, 1418-1424, 1426-1428, 1432-1433,1435, 1438, 1440, 1445-1446, 1452, 1459-1460, 1463-1464, 1466, 1468-1469, 1474-1475, 1477, 1482, 1486-1487,1490-1491, 1495, 1497, 1500, 1506-1514, 1518, 1522-1523, 1526-1529, 1533-1534, 1537-1538, 1545-1548, 1552,1555, 1557-1559, 1561, 1563, 1565-1566, 1568-1569, 1573-1576, 1580-1581, 1584-1587, 1589-1591, 1593-1596, 1600,1604, 1606, 1608-1610, 1613-1614, 1617, 1619-1621, 1624, 1626-1628, 1631, 1635-1636, 1642-1644, 1647-1650,1652-1653, 1656, 1661, 1663-1665, 1669-1672, 1675-1676, 1680, 1682, 1687-1690, 1695-1698, 1702-1703, 1705,1707-1708, 1710-1711, 1715, 1721, 1723, 1727-1732, 1734, 1737, 1739, 1741, 1749, 1754-1755, 1758, 1760, 1763-1764,1768, 1771, 1773, 1776, 1782, 1784-1785, 1788, 1790, 1792, 1794, 1798, 1801-1802, 1804, 1807, 1814, 1817-1818,1821-1823, 1825-1827, 1829-1832, 1834-1835, 1837, 1840, 1842-1845, 1847-1850, 1854-1858, 1861-1862, 1865,1868-1869, 1871, 1877-1878, 1880, 1883, 1888, 1891-1893, 1895-1896, 1898-1899, 1902-1904, 1907, 1909-1910,




M(1) MODIFICATION Linked SB Incorp. Date Title1912, 1914-1915, 1917-1918, 1922, 1926-1928, 1933-1935, 1941, 1944-1948, 1950, 1952-1953, 1955-1958, 1962, 1967,1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996, 1998, 2000, 2004, 2006-2008, 2014-2016, 2020-2021,2023, 2027, 2029, 2031-2032, 2038, 2040-2042, 2044-2045, 2055, 2058, 2063, 2067, 2070, 2073, 2075, 2077,2079-2080, 2084-2085, 2088-2090, 2094, 2096-2099, 2102, 2105, 2107-2108, 2110-2112, 2118, 2121, 2125, 2128,2130, 2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157, 2159-2161, 2164, 2167-2169, 2172-2173, 2177,2185, 2188, 2190, 2192-2195, 2197, 2200-2205, 2210-2211, 2215-2216, 2223, 2226, 2229, 2231-2232, 2234, 2238,2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263, 2267-2268, 2273, 2275, 2277, 2280-2282, 2284, 2286,2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310, 2312-2314, 2316, 2320-2324, 2326, 2329, 2331,2334-2336, 2338-2341, 2343, 2345, 2348, 2351-2352, 2355-2356, 2359, 2362-2363, 2366, 2368, 2371-2372,2375-2376, 2379, 2383-2384, 2386, 2389, 2393, 2395-2397, 2401, 2403-2405, 2408, 2410, 2413-2415, 2417-2418,2421-2424, 2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445, 2447, 2449, 2452-2455, 2457-2459, 2461-2462,2466-2470, 2473, 2475-2476, 2479-2480, 2482, 2485, 2489-2491, 2496, 2501-2502, 2504-2505, 2509-2510, 2513,2515, 2517, 2520-2522, 2524, 2526, 2530-2531, 2533-2537, 2553, 2559-2560, 2564, 2566-2568, 2570-2574,2576-2577, 2579-2580, 2585, 2587, 2589-2590, 2594-2595, 2597-2598, 2600, 2602-2604, 2608-2610, 2613-2615,2621-2622, 2626, 2630-2631, 2634, 2639-2640, 2642-2643, 2645, 2647-2651, 2653, 2655, 2657, 2659-2661,2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682, 2687-2690, 2692, 2694, 2697-2698, 2701,2703-2704, 2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728, 2730-2732, 2734, 2737-2739, 2741, 2747,2752-2753, 2755, 2759, 2766-2767, 2771-2772, 2775, 2780-2781, 2783-2784, 2787, 2791, 2793, 2797, 2799, 2802,2804, 2808-2809, 2813-2815, 2817, 2823, 2828, 2832-2833, 2838, 2840, 2844-2845, 2848, 2850, 2856, 2858-2859,2862-2864, 2868, 2871-2872, 2874, 2880, 2883, 2886-2888, 2892-2894, 2896, 2898, 2900-2901, 2904, 2906, 2908,2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934, 2936, 2940-2943, 2945, 2948, 2952-2953, 2958, 2963,2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992, 2997, 2999, 3004-3005, 3007, 3010-3013, 3015, 3017,3020, 3022, 3026, 3029, 3032-3034, 3039, 3042, 3045, 3049-3050, 3057, 3066-3067, 3069, 3071-3072, 3074-3075,3077, 3081, 3086, 3089, 3091, 3103-3106, 3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159,3162, 3165-3167, 3172, 3175, 3177, 3183, 3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3217,3219, 3222, 3227-3229, 3231, 3235, 3239, 3241, 3244, 3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270,3274-3276, 3279-3280, 3283, 3287, 3290, 3292, 3294, 3296-3297, 3301-3303, 3308, 3311, 3314-3317, 3319, 3322,3330, 3332, 3335, 3339, 3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365, 3369, 3375, 3378-3379,3381-3382, 3384, 3386-3387, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424,3428-3430, 3434, 3437, 3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468, 3474, 3478-3479, 3481,3483-3484, 3488, 3491, 3493, 3495-3497, 3499-3500, 3507, 3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531,3534-3535, 3538-3539, 3541, 3543, 3546-3548, 3550, 3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572,3575, 3577-3578, 3580-3581, 3583, 3587-3588, 3590-3592, 3595, 3600, 3603, 3607, 3613-3614, 3618, 3621-3622,3624-3625, 3636-3638, 3641, 3645, 3649-3650, 3654, 3659, 3663, 3668-3669, 3671-3674, 3676-3677, 3680-3681,3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721, 3724, 3726, 3730, 3734,3736-3738, 3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773, 3779, 3782-3785, 3793,3796-3797, 3800-3801, 3803-3804, 3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839, 3841, 3847, 3849-3851,3858, 3860, 3862-3864, 3867, 3890, 3904, 3920, 3775, 3836-3837, 3869, 3873, 3876-3878, 3881, 3893, 3897,3899, 3901-3902, 3910-3912, 3916-3917, 3924, 3926-3927, 3934-3938, 3941-3944, 3947-3948, 3951, 3959-3966,3968-3969, 3977-3981, 3989-3996

E P7929 34-1334 0734-1348 0134-1416 01

08 JUL 08 NAVIGATION-WEATHER RADAR SYSTEM-INSTALLCOLLINS DUAL CONTROL PANEL TO ACTIVATEMULTISCAN FUNCTION

Applicable to: MSN 2085, 2090, 2112, 2130, 2148, 2153, 2254, 2257, 2297, 2306, 2309-2310, 2313, 2315, 2334,2343, 2345-2346, 2348, 2354, 2361, 2396, 2403, 2424, 2429, 2431, 2433-2434, 2444, 2470, 2473, 2476, 2484-2485,




M(1) MODIFICATION Linked SB Incorp. Date Title2490, 2499, 2506, 2508-2511, 2519, 2525, 2529, 2532-2534, 2541, 2543, 2545-2546, 2549, 2551, 2554-2555, 2558,2560, 2566-2567, 2569, 2584, 2590, 2594, 2597, 2603, 2610, 2622, 2637, 2639, 2648-2649, 2654, 2656-2657,2659-2661, 2663, 2666, 2668, 2672-2673, 2679-2680, 2683-2685, 2687-2689, 2692-2694, 2696-2699, 2701, 2704,2708, 2711, 2714, 2716, 2718-2720, 2723, 2730, 2733-2734, 2737, 2743, 2746, 2749, 2757-2758, 2760, 2768,2770-2772, 2780, 2784, 2789, 2791-2793, 2796-2797, 2805, 2810, 2813, 2816, 2819-2820, 2822, 2824-2826, 2828,2833-2835, 2838-2839, 2841-2842, 2844, 2846-2847, 2849, 2853, 2855, 2859, 2861-2863, 2865, 2867, 2869, 2877,2879, 2881-2883, 2885, 2890-2891, 2893, 2895-2896, 2898-2899, 2902, 2904-2905, 2907, 2909, 2911, 2913, 2915,2917, 2924, 2926, 2929, 2931-2932, 2935, 2937, 2942, 2944, 2950, 2953, 2955-2956, 2958, 2960, 2963, 2966,2968, 2973-2976, 2978-2981, 2983, 2985-2987, 2989-2991, 2995, 3000, 3002, 3004-3007, 3011, 3013, 3016-3019,3021-3022, 3026-3027, 3031-3033, 3035, 3042-3043, 3045-3047, 3049-3050, 3055-3058, 3060, 3064-3066,3068-3069, 3071, 3074, 3076-3077, 3079-3080, 3085-3086, 3093-3094, 3097, 3103, 3111, 3113-3117, 3121, 3124,3128-3129, 3131-3132, 3136, 3139-3142, 3153-3154, 3156, 3158-3159, 3165, 3167-3168, 3170-3173, 3175, 3178, 3180,3182, 3186, 3188, 3192-3202, 3206, 3210-3211, 3213, 3217-3218, 3220, 3222-3223, 3225-3227, 3229, 3232-3234,3240-3243, 3245, 3247-3251, 3253, 3256, 3259-3262, 3264-3266, 3268, 3274, 3276-3279, 3282, 3284-3285, 3289,3291, 3294-3295, 3299, 3306-3309, 3313, 3315, 3318, 3323, 3325, 3327-3331, 3335, 3338-3339, 3343, 3345-3346,3349, 3352-3353, 3355, 3357-3358, 3360, 3362, 3364-3366, 3368-3370, 3375, 3378, 3382-3383, 3385-3388,3391-3395, 3397, 3403-3404, 3406-3408, 3412, 3414-3415, 3418, 3421, 3423-3424, 3427-3428, 3434-3436,3439-3440, 3444, 3446-3450, 3452-3454, 3456-3459, 3462-3464, 3467, 3471, 3473, 3476-3478, 3482, 3484-3486,3489-3491, 3493-3494, 3497, 3500-3502, 3504-3505, 3507, 3510, 3515, 3518-3523, 3526-3528, 3532-3534, 3536,3538, 3540-3541, 3546, 3548-3549, 3552, 3559-3561, 3563-3566, 3568, 3570, 3575-3578, 3580-3584, 3586-3600,3604-3605, 3609-3612, 3614, 3616, 3618, 3623-3626, 3628-3630, 3633, 3636, 3643, 3645, 3647-3648, 3653,3655-3656, 3658, 3660-3662, 3664-3666, 3669-3670, 3672, 3676, 3678-3682, 3685, 3689, 3691, 3694-3696,3700-3701, 3704-3705, 3708-3710, 3712, 3714-3715, 3722-3723, 3725, 3727-3730, 3732-3733, 3737, 3739-3740,3745, 3749-3750, 3753, 3756, 3761, 3764-3766, 3768-3769, 3773, 3776, 3782, 3784-3785, 3791, 3796, 3798,3802-3803, 3806, 3813, 3815-3816, 3820-3821, 3839-3841, 3860-3867, 3875, 3878-3881, 3883, 3890, 3892-3893,3903, 2801, 3638-3639, 3698, 3758-3759, 3818, 3827-3833, 3846-3853, 3855, 3857-3858, 3869, 3872, 3885-3887,3895-3898, 3900, 3906-3908, 3910-3911, 3915, 3919-3921, 3924-3925, 3928, 3931-3932, 3934-3936, 3938-3945,3949-3951, 3956-3964, 3966-3967, 3969, 3971-3996

E P8161 08 JUL 08 AUTO FLIGHT-FMS- ACTIVATE LOC BACK-BEAMAPPROACH & BACK COURSE TAKE OFF OPTION ONTHALES & HONEYWELL FMS2

Applicable to: MSN 2612, 2633, 2656, 2683, 2699, 2719, 2758, 2760, 2789, 2816, 2826, 2842, 2881, 2885, 2926,2944, 2956, 2989, 3000, 3018, 3031, 3043, 3060, 3064, 3085, 3094, 3097, 3117, 3140, 3154, 3173, 3182, 3194, 3201,3223, 3232, 3261, 3277, 3291, 3299, 3327, 3338, 3353, 3370, 3394, 3404, 3406, 3427, 3436, 3448, 3452, 3477, 3486,3489, 3505, 3521, 3536, 3549, 3568, 3576, 3582, 3610, 3628, 3648, 3660, 3679, 3701, 3715, 3729, 3765, 3776, 3813,3875, 3892, 2801

E P8194 34-1346 02 08 JUL 08 NAVIGATION - ADIRS ACTIVATE ALIGNMENTIMPROVEMENT FUNCTION ON ADIRU

Applicable to: MSN 0910, 2211, 2216, 2277, 2288, 2296, 2335, 2341, 2362, 2383, 2396, 2404, 2410, 2414, 2431,2452, 2467-2468, 2719, 2736, 2756, 2758, 2776, 2789, 2807, 2813, 2833, 2843, 2845, 2858, 2864, 2870, 2872,2886-2887, 2889, 2892, 2894, 2897, 2907, 2924, 2931, 2955, 2976, 2996-2997, 3001-3002, 3011, 3016, 3030-3033,3035, 3043, 3047, 3054, 3058, 3060, 3062, 3066, 3071-3072, 3074, 3078, 3085, 3091, 3094, 3097, 3102, 3106, 3109,3111, 3119, 3127-3128, 3130, 3138, 3142-3143, 3145-3146, 3149-3151, 3156, 3160-3161, 3166, 3169, 3171-3172,3174, 3177, 3179-3180, 3190, 3193, 3203, 3209, 3211-3212, 3214, 3216-3217, 3220, 3222, 3224-3225, 3228-3229,3236-3237, 3240-3241, 3251-3252, 3255-3256, 3263, 3266, 3271, 3278, 3280, 3284, 3286-3288, 3294, 3300,




M(1) MODIFICATION Linked SB Incorp. Date Title3305-3307, 3309, 3312-3313, 3317, 3319-3320, 3325-3326, 3329, 3331, 3340, 3344, 3348-3349, 3352, 3354, 3358,3364-3365, 3367, 3371, 3375-3377, 3380-3382, 3384-3385, 3388, 3390-3392, 3400, 3403, 3406, 3408-3409, 3416,3423, 3430, 3433, 3436, 3438-3439, 3443, 3446, 3451-3452, 3459, 3462, 3467, 3469, 3472-3473, 3478-3479,3487-3488, 3490, 3492-3494, 3498, 3500, 3507-3509, 3514, 3517-3518, 3523, 3526-3527, 3531, 3533-3535, 3540,3546, 3551-3552, 3554, 3556-3557, 3560, 3562, 3564-3566, 3572-3573, 3575, 3585, 3587-3589, 3594-3595,3597, 3602, 3605-3606, 3615-3616, 3619-3620, 3622-3624, 3630, 3635, 3642, 3645-3647, 3651, 3653, 3655-3660,3662-3665, 3667, 3670-3672, 3678, 3681, 3687, 3690-3691, 3693, 3707, 3709-3710, 3713-3714, 3722, 3724-3725,3727, 3733, 3736, 3739, 3741, 3744-3745, 3747, 3750, 3752-3753, 3755, 3757-3758, 3760-3762, 3764, 3766-3767,3769-3773, 3779, 3781, 3784-3785, 3791-3792, 3798, 3800-3801, 3804, 3806-3807, 3811, 3816, 3822, 3839, 3841,3847, 3850, 3860-3861, 3874, 3890, 3892, 2801, 3818-3820, 3827-3829, 3834, 3836-3837, 3853, 3866-3867, 3869,3872, 3876-3878, 3880, 3882-3883, 3886, 3895, 3900-3903, 3907-3908, 3910, 3915, 3918-3920, 3927, 3934,3938-3941, 3947, 3950-3952, 3955, 3959, 3967-3970, 3972, 3981-3983

E P8233 34-1316 04 08 JUL 08 NAVIGATION - WEATHER RADAR SYSTEM - INSTALLHONEYWELL DUAL CONTROL UNIT CAPABLE OFAUTO-TILT FUNCTION

Applicable to: MSN 1773, 1878, 1953, 1956, 1967, 2055, 2064, 2076, 2091, 2097, 2288, 2308, 2326, 2330, 2337,2341-2342, 2355, 2375, 2379, 2418-2419, 2421, 2438-2439, 2441, 2469, 2501, 2540, 2596, 2609, 2616, 2623, 2626,2653, 2662, 2674, 2678, 2726, 2736, 2740, 2748, 2756, 2761-2762, 2773, 2776, 2778, 2785, 2794, 2798-2800,2807, 2811, 2823, 2830, 2843, 2851, 2868, 2870, 2875, 2878, 2889, 2897, 2903, 2912, 2920, 2925, 2928, 2934,2941, 2947, 2954, 2957, 2962, 2965, 2984, 2988, 2993, 2996-2997, 2999, 3010, 3015, 3024, 3037, 3040, 3052, 3054,3063, 3070, 3078, 3081, 3083, 3087, 3095, 3101-3102, 3107-3109, 3126-3127, 3130, 3135, 3138, 3143, 3145-3146,3151-3152, 3155, 3157, 3161, 3166, 3169, 3174, 3177, 3179, 3181, 3185, 3187, 3191, 3203-3205, 3207-3209, 3212,3215, 3221, 3230, 3235, 3237, 3239, 3246, 3252, 3254-3255, 3257, 3267, 3271, 3273, 3281, 3283, 3288, 3290, 3293,3298, 3300-3301, 3303, 3305, 3310, 3314, 3317, 3320-3321, 3324, 3326, 3334, 3336-3337, 3340-3341, 3344, 3347,3350-3351, 3354, 3359, 3361, 3367, 3373, 3376-3377, 3380, 3384, 3396, 3398, 3400, 3405, 3409-3410, 3417, 3422,3425, 3429-3430, 3433, 3443, 3445, 3455, 3460-3461, 3465, 3468, 3472, 3475, 3480-3481, 3487, 3492, 3498-3499,3503, 3506, 3511-3512, 3516, 3525, 3529, 3531, 3539, 3545, 3550-3551, 3553, 3557-3558, 3562, 3567, 3573-3574,3579, 3601, 3603, 3607, 3613, 3619-3620, 3627, 3631, 3640, 3644, 3646, 3649-3652, 3654, 3677, 3684, 3686-3687,3692-3693, 3697, 3699, 3703, 3706, 3711, 3713, 3716, 3718-3719, 3721, 3726, 3731, 3736, 3741, 3744, 3747, 3752,3755, 3762, 3767, 3771, 3778, 3781, 3786-3787, 3789, 3792-3794, 3804, 3807, 3809, 3817, 3822-3823, 3874, 3904,3937, 3775, 3797, 3819, 3834-3835, 3837-3838, 3877, 3882, 3894, 3899, 3902, 3912, 3916, 3918, 3923, 3926-3927,3947-3948, 3952, 3954-3955, 3965, 3968, 3970, 3984

E P8440 32-1291 01 08 JUL 08 LANDING GEAR - WHEELS AND BRAKES INTRODUCEGOODRICH DURACARB CARBON BRAKES WITH ANTI- OXYDAN "M1"

Applicable to: MSN 0052-0055, 0064-0067, 0076-0077, 0081-0082, 0091, 0098-0099, 0252, 0259-0261, 0275-0276,0280, 0291-0292, 0296, 0317, 0320-0321, 0332, 0347, 0353, 0357, 0361, 0368-0369, 0373, 0405, 0415, 0427-0428,0447-0448, 0455, 0467, 0471, 0527, 0543, 0565, 0584, 0661, 0733, 0747, 0762, 0770, 0803, 0856, 0866, 0889,0924, 0931, 0953, 1003, 1043, 1049-1050, 1056, 1064, 1075, 1079, 1083, 1088, 1110-1111, 1113, 1116, 1152, 1166,1178, 1196, 1198, 1223, 1234, 1274, 1281, 1284, 1323, 1339, 1350, 1353, 1373-1375, 1395, 1397, 1400, 1406, 1410,1419, 1429, 1463, 1482, 1490, 1500, 1509, 1527, 1534, 1547, 1552, 1563, 1565, 1576, 1598, 1612, 1615, 1618,1624-1625, 1634, 1676, 1706, 1725, 1730, 1750, 1764, 1792, 1844, 1866-1867, 1872, 1882, 1925, 1934-1935, 1952,2029, 2066, 2077-2078, 2118, 2126, 2175, 2187, 2193, 2277, 2296, 2301-2302, 2312, 2325, 2327-2328, 2333, 2335,2339, 2358-2359, 2362, 2367, 2377, 2383, 2394, 2396, 2399, 2402, 2404-2405, 2409, 2411-2412, 2414, 2420, 2422,2427, 2430-2432, 2434, 2436, 2438, 2441-2442, 2444, 2446, 2448, 2450, 2452, 2455, 2458, 2460, 2463-2465,




M(1) MODIFICATION Linked SB Incorp. Date Title2467-2469, 2471, 2474-2475, 2477, 2481-2483, 2486-2487, 2492, 2495, 2497, 2501, 2503, 2512, 2514-2516, 2518,2523, 2526-2528, 2537-2538, 2542, 2544, 2548, 2552, 2556, 2565, 2570, 2572-2573, 2575, 2578, 2583, 2585-2588,2595, 2600, 2604-2605, 2608, 2613, 2615, 2618, 2625, 2630, 2635-2636, 2638, 2641-2642, 2646, 2651, 2657, 2662,2666, 2669, 2677, 2681, 2690-2691, 2700, 2702-2703, 2709, 2715, 2717, 2727, 2729, 2735, 2742, 2744, 2751, 2754,2763, 2765-2766, 2769, 2771, 2777, 2779-2780, 2782, 2786-2788, 2790-2791, 2795, 2803, 2806, 2810, 2812-2813,2818, 2821, 2827, 2829, 2831, 2833, 2836, 2852, 2854, 2857, 2860, 2866, 2873, 2875-2876, 2884, 2917, 2920, 2923,2946-2947, 2959, 2976, 2979, 2987, 2994, 2997, 3003, 3011, 3028, 3036, 3038, 3041-3042, 3045, 3048, 3052-3053,3057, 3059, 3061, 3063, 3069, 3077, 3082, 3084, 3088, 3090, 3092, 3103, 3110, 3113, 3118, 3122-3123, 3128-3129,3134, 3136-3137, 3157, 3163, 3172, 3175-3176, 3184, 3193, 3248, 3253, 3272, 3276, 3279, 3281, 3298, 3304, 3318,3336, 3345, 3352, 3358, 3373-3375, 3378, 3389, 3408, 3410-3411, 3413, 3418, 3426, 3431-3433, 3442, 3450, 3463,3466-3467, 3472, 3474, 3487, 3491, 3495, 3500-3501, 3510-3511, 3518, 3534, 3537-3538, 3544-3545, 3547, 3555,3569, 3571, 3574, 3577, 3581, 3590, 3608, 3624, 3627, 3631, 3634, 3640, 3644, 3646-3647, 3664, 3668, 3672, 3675,3683, 3691, 3699, 3702, 3705, 3711, 3720, 3735, 3742-3743, 3746, 3754, 3762-3763, 3767, 3774, 3778, 3783, 3786,3788-3790, 3794, 3799, 3805, 3808, 3810, 3823-3824, 3835, 3838-3839, 3841-3845, 3854, 3871, 3888, 3857, 3905,3909, 3913, 3917, 3922-3923, 3946, 3953-3954

E P9032 08 JUL 08 FLIGHT CONTROLS - CONTROL INPUTS INTERFACEAND POWER SUPPLY - ACTIVATE "STEEP APPROACH"CAPABILITY ON A318 A/C

Applicable to: MSN 3617, 3932E P9171 08 JUL 08 NAVIGATION-AIR DATA/INERTIAL REFERENCE SYSTEM

(ADIRS) - INTRODUCE AIR DATA MONITORINGFUNCTION

Applicable to: MSN 3606, 3609, 3617, 3635, 3642-3643, 3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886,3897, 3906, 3921, 3932, 3956

N P9355 09 JAN 09 NAVIGATION - WEATHER RADAR SYSTEM - REMOVEWXR TRANSCEIVER COLLINS -623 AND DEACTIVATEPWS (ANTI-MOD 32740/26560)

Applicable to: MSN 2645-2647, 2650-2653, 2658, 2662, 2664, 2667, 2670-2671, 2674, 2676-2678, 2681-2682, 2691,2695, 2700, 2702-2703, 2707, 2709-2710, 2713, 2715, 2717, 2724-2729, 2731, 2735-2736, 2740-2742, 2744-2745,2747-2748, 2751, 2753-2756, 2759, 2761-2763, 2765-2767, 2769, 2773-2779, 2781-2782, 2785-2787, 2790,2794-2795, 2798-2800, 2802-2804, 2806-2809, 2811-2812, 2814-2815, 2817-2818, 2821, 2823, 2827, 2829-2832,2836, 2840, 2843, 2848, 2850-2852, 2854, 2856-2857, 2860, 2866, 2868, 2870-2871, 2873-2876, 2878, 2880,2884, 2888-2889, 2897, 2900-2901, 2903, 2906, 2908, 2912, 2914, 2916, 2919-2920, 2922-2923, 2925, 2927-2928,2933-2934, 2936, 2939-2941, 2943, 2945-2948, 2952, 2954, 2957, 2959, 2962, 2965, 2969-2971, 2977, 2982,2984, 2988, 2992-2994, 2996-2999, 3003, 3010, 3012, 3014-3015, 3020, 3023-3025, 3028-3029, 3034, 3036-3037,3039-3041, 3048, 3052-3054, 3059, 3061, 3063, 3067, 3070, 3072, 3075, 3078, 3081-3084, 3087-3091, 3095-3096,3099, 3101-3102, 3104-3109, 3112, 3118-3120, 3122, 3125-3127, 3130, 3134-3135, 3137-3138, 3143-3152, 3155, 3157,3160-3162, 3164, 3166, 3169, 3174, 3176-3177, 3179, 3181, 3183-3185, 3187, 3189-3191, 3203-3205, 3207-3209,3212, 3215, 3219, 3221, 3224, 3228, 3230-3231, 3235-3237, 3239, 3244, 3246, 3252, 3254-3255, 3257-3258,3263, 3267, 3269-3273, 3275, 3281, 3283, 3286-3288, 3290, 3292-3293, 3296-3298, 3300-3303, 3305, 3310-3312,3314, 3316-3317, 3320-3322, 3324, 3326, 3332, 3334, 3336-3337, 3340-3342, 3344, 3347-3348, 3350-3351, 3354,3356, 3359, 3361, 3367, 3373, 3376-3377, 3379-3381, 3384, 3389, 3396, 3398, 3400, 3402, 3405, 3409-3411,3413, 3416-3417, 3422, 3425-3426, 3429-3433, 3437, 3442-3443, 3445, 3451, 3455, 3460-3461, 3465-3466, 3468,3472, 3474-3475, 3479-3481, 3483, 3487-3488, 3492, 3495-3496, 3498-3499, 3503, 3506, 3508, 3511-3512, 3514,3516-3517, 3524-3525, 3529, 3531, 3537, 3539, 3543-3545, 3547, 3550-3551, 3553-3555, 3557-3558, 3562, 3567,




M(1) MODIFICATION Linked SB Incorp. Date Title3569, 3571-3574, 3579, 3601, 3603, 3607-3608, 3613, 3615, 3619-3622, 3627, 3631, 3634, 3637, 3640-3641, 3644,3646, 3649-3652, 3654, 3657, 3659, 3667-3668, 3673-3675, 3677, 3683-3684, 3686-3688, 3690, 3692-3693, 3697,3699, 3702-3703, 3706-3707, 3711, 3713, 3716-3721, 3724, 3726, 3731, 3734-3736, 3738, 3741-3744, 3746-3748,3752, 3754-3755, 3757, 3760, 3762-3763, 3767, 3771, 3774-3775, 3778, 3780-3781, 3783, 3786-3789, 3792-3794,3799-3801, 3804-3805, 3807-3812, 3817, 3822-3824, 3843-3845, 3854, 3871, 3888-3889, 3904, 3937, 3797, 3819,3834-3835, 3837-3838, 3868, 3873-3874, 3877, 3882, 3894, 3899, 3902, 3909, 3912-3913, 3916-3918, 3922-3923,3926-3927, 3933, 3946-3948, 3952-3955, 3965, 3968, 3970, 3984

E P9907 08 JUL 08 INDICATING RECORDING SYSTEM - FLIGHT WARNINGCOMPUTER (FWC)- INSTALL FWC STANDARD H2-F4

Applicable to: MSN 3001, 3030, 3062, 3100, 3213-3214, 3216, 3238, 3243, 3295, 3309, 3328, 3331, 3333, 3343,3362-3363, 3371, 3385, 3388, 3390, 3412, 3438, 3464, 3469, 3482, 3502, 3509, 3515, 3530, 3532, 3563-3564, 3585,3598, 3602, 3606, 3609, 3617, 3635, 3642-3643, 3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886, 3897, 3906,3921, 3932, 3956

E 22-1026 16 08 JUL 08 AUTO FLIGHT - IAE/CFM ENGINES - PROVIDE PINPROGRAMMING FOR ENERGY MANAGEMENTRETROFIT.

Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0111,0115-0118, 0120-0122, 0125-0137, 0140-0147, 0149-0150, 0152-0162, 0171-0177, 0183-0188, 0191-0192, 0197,0199-0204, 0206-0211, 0213-0218, 0220, 0223-0224, 0226-0229, 0231-0242, 0244, 0246, 0248, 0252-0255,0259-0288, 0290-0292, 0296-0298, 0302-0303, 0305-0307, 0309-0313, 0318-0321, 0323-0325, 0329-0333, 0337,0339-0342, 0345-0347, 0350, 0352-0353, 0355-0356, 0358-0361, 0367-0369, 0372-0375, 0377-0378, 0380-0382,0384, 0387-0388, 0395, 0399-0401, 0403-0405, 0407-0410, 0415, 0417-0421, 0426-0428, 0435-0436, 0438-0439,0442, 0445, 0449-0450, 0452, 0454, 0456-0457, 0459, 0462, 0466-0467

E 22-1052 00 08 JUL 08 AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER(FAC) - INSTALL WINDSHEAR-2 FAC (AAM0509 ANDCAM0101).

Applicable to: MSN 0003, 0010-0013, 0016, 0033, 0035-0038, 0044, 0052-0054, 0059, 0064, 0068, 0073, 0076,0081-0082, 0084-0085, 0098, 0108, 0112, 0115, 0119, 0122-0124, 0126-0127, 0130, 0138-0139, 0141, 0144-0145,0148-0151, 0154-0156, 0159, 0163-0164, 0167-0170, 0174-0175, 0179-0180, 0183-0184, 0189-0190, 0193, 0196,0204-0205, 0210-0212, 0214-0215, 0219, 0231-0233, 0235-0239, 0242-0245, 0248-0251, 0253-0257, 0265, 0270,0277-0280, 0283-0284, 0289-0293, 0295, 0300, 0302, 0304-0305, 0308-0311, 0313-0316, 0324, 0327-0328, 0330,0333-0337, 0341-0343, 0348, 0350, 0352, 0359, 0362-0363, 0365, 0370, 0376-0379, 0383-0384, 0386, 0389-0394,0402-0405, 0413-0415, 0420-0422, 0424-0426, 0428-0430, 0436-0438, 0440, 0443-0449, 0453, 0459, 0466, 0476,0482, 0511

E 31-1068 21 08 JUL 08 INDICATING/RECORDING SYSTEMS - GENERAL -DEFINE PIN PROGRAMMING FOR CPIP3 RETROFIT.

Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112,0115-0162, 0167, 0170-0177, 0183-0188, 0191-0192, 0196-0197, 0199-0220, 0222-0224, 0226-0229, 0231, 0233-0242,0244-0246, 0248, 0253-0255, 0258, 0262-0274, 0277-0279, 0281-0288, 0290, 0293, 0297-0303, 0305-0307,0309-0313, 0315, 0318-0319, 0323-0325, 0328-0331, 0333, 0337, 0339-0342, 0344-0346, 0348, 0350, 0352,0355-0356, 0358-0360, 0365, 0367, 0370, 0372, 0375, 0377-0378, 0380-0384, 0387-0390, 0395, 0399-0404,0407-0410, 0413, 0417-0421, 0426-0427, 0435-0436, 0438-0439, 0442, 0445, 0450, 0452, 0454, 0456-0457,0459-0460, 0462, 0466, 0482, 0511




M(1) MODIFICATION Linked SB Incorp. Date Title32-1188 03 08 JUL 08 LANDING GEAR - MLG - REPLACE BF GOODRICH

WHEELS AND BRAKES BY MESSIER BUGATTI WHEELSAND BRAKES (SEPCARB III).

Applicable to: MSN 0225, 0308, 0314, 0737, 0749, 0799, 0828, 0879, 0888, 0976, 1010, 1092, 1096, 1103, 113932-1242 07 08 JUL 08 LANDING GEAR - WHEELS AND BRAKES - REPLACE

A321 TYPE ABS WHEELS AND BRAKES BY MESSIERWHEELS AND "SEPCARB III PLUS" BRAKES OR"SEPCARB III PLUS OR" BRAKES

Applicable to: MSN 0580, 0667, 0934, 0951, 0990, 0999, 1014, 1138, 1168, 1177, 1183, 1217, 1226, 1383, 1459, 1697,1732, 1987

N 32-1244 36 09 JAN 09 LANDING GEAR - WHEELS AND BRAKES - INSTALLMESSIER WHEELS AND "SEPCARB III PLUS" OR"SEPCARB III PLUS OR" BRAKES

Applicable to: MSN 0112, 0191, 0234, 0243, 0249-0251, 0279, 0293, 0304, 0315, 0327, 0334-0336, 0354, 0376,0379, 0386, 0389, 0391-0395, 0400, 0411, 0425, 0440, 0443, 0446, 0453, 0530, 0558, 0561, 0573, 0582, 0640,0676, 0707, 0716, 0724, 0733, 0739, 0743, 0747, 0758, 0760, 0816, 0839, 0857, 0874, 0892, 0902, 0912, 0916, 0936,0946, 0949, 0978, 1007, 1071, 1078, 1090-1091, 1126, 1129-1130, 1143, 1158, 1164, 1171, 1194, 1210, 1213, 1246,1251, 1263, 1286, 1304, 1306, 1332, 1351, 1355, 1368, 1376, 1390, 1486, 1491, 1500, 1512, 1518, 1526, 1548, 1568,1575, 1580, 1593, 1595, 1608, 1613, 1626, 1628, 1635, 1703, 1751, 1756, 1765, 1834, 1853-1854, 1858, 1877, 1892,1902-1903, 1922, 1929, 1963, 2028, 2089, 2096, 2295-2296, 2304, 2321, 2335, 2369, 2372-2373, 2383, 2393, 2396,2431, 2441, 2467-2468, 2474, 2572, 2585, 2700, 2987

32-1245 02 08 JUL 08 LANDING GEAR - MAIN GEAR - REPLACE MESSIERWHEELS AND SEPCARB III (PLUS) BRAKES BY LATESTSTANDARD OF GOODRICH WHEELS & SEPCARB IIIBRAKES.

Applicable to: MSN 0332, 0361, 0369, 0405, 0415, 0427-0428, 1152, 1198, 161232-1276 00 08 JUL 08 LANDING GEAR - WHEELS AND BRAKES - CHANGE

ABS MLG WHEELS AND BRAKES TO GOODRICHApplicable to: MSN 0565, 0661

E 34-1155 04 08 JUL 08 NAVIGATION - INSTRUMENT LANDING SYSTEM -INSTALL THALES MMR PROVIDING ILS (FM IMMUNE)AND GPS PRIMARY FUNCTION (AUTONOMOUSARCHITECTURE)

Applicable to: MSN 0043, 0113-0114, 0325, 0348, 0375, 0409, 0459, 0466, 0497, 0537, 0615, 0622, 066234-1167 01 08 JUL 08 NAVIGATION - INSTALL LITTON ADIRS (4MCU) INSTEAD

OF HONEYWELL ADIRS (4MCU) - FOR RETROFITONLY.

Applicable to: MSN 0756, 078434-1207 00 08 JUL 08 NAVIGATION - INSTALL COLLINS MMR PROVIDING ILS

(FM IMMUNE) AND GPS PRIMARY FUNCTION INSTEADOF SEXTANT MMR.

Applicable to: MSN 0877, 0992, 0994, 1021, 1027




M(1) MODIFICATION Linked SB Incorp. Date TitleE 34-1208 07 08 JUL 08 NAVIGATION - ILS - INSTALL COLLINS MMR PROVIDING

ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION(AUTONOMOUS ARCHITECTURE)

Applicable to: MSN 0002-0021, 0033, 0044, 0061-0063, 0100-0102, 0108, 0115, 0128-0131, 0133-0134, 0136,0143-0146, 0155-0156, 0158, 0170, 0173, 0176-0177, 0184, 0186-0188, 0196, 0199, 0203-0204, 0207, 0211-0212,0214-0215, 0219-0220, 0223-0224, 0226-0228, 0235-0241, 0244-0246, 0264, 0266, 0270, 0274, 0278, 0285-0287,0300, 0303, 0312, 0323, 0328, 0337, 0352, 0356, 0365, 0377, 0383, 0400, 0413, 0491, 0501, 0507, 0530-0531, 0534,0549, 0554, 0658, 0669, 0685

34-1395 00 08 JUL 08 NAVIGATION - WEATHER RADAR SYSTEM - INSTALLHONEYWELL SINGLE CONTROL PANEL CAPABLE OFTHE AUTOTILT AND PWS FUNCTIONS.

Applicable to: MSN 0764N 34-1424 00 09 JAN 09 NAVIGATION - MMR - INSTALL THALES MMR

TLS755-01-0102A (AUTONOMOUS ARCHITECTURE).Applicable to: MSN 0213, 0988

73-1065 00 08 JUL 08 ENGINE FUEL AND CONTROL - FADEC SYSTEM -INTRODUCE V2500-A1 FADEC A1-SCN14/R.

Applicable to: MSN 0043, 0091, 0113-0114, 0165-0166, 0178, 0194, 0198, 0225, 0243, 0249-0252, 0259-0261,0275-0276, 0280, 0291-0292, 0296, 0320-0322, 0326, 0332, 0334-0335, 0338, 0344, 0347, 0351, 0353, 0357, 0361,0366, 0368-0369, 0373, 0376, 0386, 0393, 0405-0406, 0415, 0428-0430, 0437, 0440-0441, 0447, 0467, 0478, 0480

(1) Evolution code

INTRODUCTION


INTRODUCTIONPRELIMINARY PAGES

TABLE OF CONTENTS

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IN-010. GENERAL INTRODUCTIONFOREWORD.............................................................................................................................................................1/2COMMENT - QUESTIONS - SUGGESTIONS........................................................................................................ 1/2

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SUMMARY OF HIGHLIGHTS

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IN-010COMMENT - QUESTIONS -SUGGESTIONS

1/2 1 Update of the e-mail address to be used for any questions andsuggestions about the FCTM.





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ENV A318/A319/A320/A321 FLEET IN-010. P 1/2FCTM 09 JAN 09

FOREWORDIdent.: IN-010-00005422.0001001 / 12 MAR 08Criteria: SA�Applicable to: ALL

The Flight Crew Training Manual (FCTM) is published as a supplement to the Flight Crew OperatingManual (FCOM) and is designed to provide pilots with practical information on how to operate theAirbus aircraft. It should be read in conjunction with the FCOM. In the case of any conflict, the FCOMis the over-riding authority.Airline training policy may differ in certain areas. Should this be the case, the airline training policy isthe over-riding authority.

COMMENT - QUESTIONS - SUGGESTIONSIdent.: IN-010-00005423.0001001 / 09 DEC 08Criteria: SA�Applicable to: ALL

1 FCTM holders and users are encouraged to submit questions and suggestions regarding this manualto:[email protected], rond point Maurice BELLONTE31707 BLAGNAC CEDEX- FRANCEATTN: Flight Operations Support – STLS


INTRODUCTIONGENERAL INTRODUCTION


ENV A318/A319/A320/A321 FLEET IN-010. P 2/2FCTM 09 JAN 09

OPERATIONAL PHILOSOPHY


OPERATIONAL PHILOSOPHYPRELIMINARY PAGES

TABLE OF CONTENTS

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OP-010. INTRODUCTIONINTRODUCTION...................................................................................................................................................... 1/2OPERATIONAL GOLDEN RULES...........................................................................................................................1/2

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OP-020. FLIGHT CONTROLSINTRODUCTION.................................................................................................................................................... 1/20NORMAL LAW....................................................................................................................................................... 1/20ALTERNATE LAW.................................................................................................................................................. 5/20DIRECT LAW......................................................................................................................................................... 5/20INDICATIONS......................................................................................................................................................... 6/20PROTECTIONS...................................................................................................................................................... 7/20MECHANICAL BACKUP ..................................................................................................................................... 17/20ABNORMAL ATTITUDES.....................................................................................................................................18/20SIDESTICK AND TAKEOVER P/B.......................................................................................................................18/20

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OP-030. AP / FD / ATHRAUTOPILOT/FLIGHT DIRECTOR.......................................................................................................................... 1/24AUTOTHRUST (A/THR)......................................................................................................................................... 4/24AP, FD, A/THR MODE CHANGES AND REVERSIONS..................................................................................... 15/24TRIPLE CLICK..................................................................................................................................................... 22/24

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OP-040. ECAMPURPOSE OF THE ECAM....................................................................................................................................1/10MAIN principles...................................................................................................................................................... 1/10ECAM HANDLING..................................................................................................................................................2/10use of summaries...................................................................................................................................................8/10

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LocalizationTitle

Page ID Reason

OP-020PROTECTIONS

7/20 1 Solution actual effectivity changed: 0299,0371 removed

OP-020PROTECTIONS

12/20 2 Solution actual effectivity changed:0005,0299,0371,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removedDuring the approach, with the A/THR active, Airbusrecommended to set the thrust levers above the CL detent(but below the MCT detent), in exceptional circumstances,if the speed significantly dropped below Vapp. Howeverthis procedure is not trained and proved to have modedrawbacks than advantages. Therefore, Airbus does nolonger recommend to use this procedure. The procedure isdeleted from the operational documentation. If the A/THRperformance is not satisfactory, the flight should manually takeover, and control the thrust manually.

OP-030AUTOTHRUST (A/THR)

4/24 1

Deleted part insideOP-030AUTOTHRUST (A/THR)

9/24 2 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removedDuring the approach, with the A/THR active, Airbusrecommended to set the thrust levers above the CL detent(but below the MCT detent), in exceptional circumstances,if the speed significantly dropped below Vapp. Howeverthis procedure is not trained and proved to have modedrawbacks than advantages. Therefore, Airbus does nolonger recommend to use this procedure. The procedure isdeleted from the operational documentation. If the A/THRperformance is not satisfactory, the flight should manually takeover, and control the thrust manually.

OP-030AUTOTHRUST (A/THR)

9/24 3

Deleted part insideOP-030AP, FD, A/THR MODE CHANGESAND REVERSIONS

15/24 4 Solution actual effectivity changed: 0768,0776,0797 added,0002,0004,0006,0007,0010,0012,0013,0014,0017,0019,0020,0036,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491,0550,0573,0674,0684,0763removed

OP-030AP, FD, A/THR MODE CHANGESAND REVERSIONS

19/24 5 Solution actual effectivity changed:0002,0005,0007,0010,0012,0013,0014,0019,0020,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491,0550,0573,0674,0684,0763,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0768,0776,0797,1374,2500 removed

OP-030TRIPLE CLICK

22/24 6 Solution actual effectivity changed:0005,1951,2024,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,2500 removed





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OPERATIONAL PHILOSOPHYINTRODUCTION

ENV A318/A319/A320/A321 FLEET OP-010. P 1/2FCTM 08 JUL 08

INTRODUCTIONIdent.: OP-010-00005425.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The Airbus cockpit is designed to achieve pilot operational needs throughout the aircraft operatingenvironment, while ensuring maximum commonality within the Fly by Wire family.

The cockpit design objectives are driven by three criteria:• Reinforce the safety of flight• Improve efficiency of flight• Answer pilot requirements in a continuously changing environment

Airbus operational rules result from the design concept, more particularly from the following systems:• The Fly by wire system with its control laws and protections, commanded through the side stick,• An integrated Auto Flight System (AFS) comprising:

‐ The FMS interfaced through the MCDU,‐ The AP/FD interfaced through the FCU,‐ The A/THR interfaced through the non back driven thrust levers,‐ The FMA, providing Guidance targets and Information, to monitor the AFS

• A set of Display units (DU) providing information and parameters required by the crew‐ To operate and to navigate the aircraft (the EFIS)‐ To communicate (the DCDU)‐ To manage the aircraft systems (the ECAM)‐ FMA interface to provide Guidance targets and information to monitor the AFS/FD

• A Forward Facing Cockpit Layout with "Lights out" or "Dark Cockpit" concept assisting the crew toproperly control the various aircraft systems.

The operational rules applicable to these specific features are given in the other sections of thischapter.

OPERATIONAL GOLDEN RULESIdent.: OP-010-00005426.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

1. The aircraft can be flown like any other aircraft2. Fly, navigate, communicate - in that order3. One head up at all times4. Cross check the accuracy of the FMS5. Know your FMA at all times6. When things don’t go as expected - take over


OPERATIONAL PHILOSOPHYINTRODUCTION


7. Use the proper level of automation for the task8. Practice task sharing and back-up each other


OPERATIONAL PHILOSOPHYFLIGHT CONTROLS

ENV A318/A319/A320/A321 FLEET OP-020. P 1/20FCTM 09 JAN 09

INTRODUCTIONIdent.: OP-020-00005427.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The relationship between the Pilot Flying’s (PF’s) input on the sidestick, and the aircraft’s response, isreferred to as control law. This relationship determines the handling characteristics of the aircraft.There are three sets of control laws, and they are provided according to the status of the: Computers,peripherals, and hydraulic generation.

The three sets of control laws are:• Normal law• Alternate law• Direct law.

NORMAL LAWIdent.: OP-020-00005428.0001001 / 08 JAN 09Criteria: SA�Applicable to: ALL

OBJECTIVES

The aim of normal law is to provide the following handling characteristics within the normal flightenvelope (regardless of aircraft speed, altitude, gross weight and CG):• Aircraft must be stable and maneuverable• The same response must be consistently obtained from the aircraft• The Actions on the sidestick must be balanced in pitch and in roll.

The normal law handling characteristics, at the flight envelope limit are:• The PF has full authority to achieve Maximum aircraft Performance• The PF can have instinctive/immediate reaction, in the event of an emergency• There is a reduced possibility of overcontrolling or overstressing the aircraft.

Normal Law is the law that is most commonly available, and it handles single failures.

CHARACTERISTICS IN PITCH

IN FLIGHT

When the PF performs sidestick inputs, a constant G-load maneuver is ordered, and the aircraftresponds with a G-Load/Pitch rate. Therefore, the PF’s order is consistent with the response thatis "naturally" expected from the aircraft: Pitch rate at low speed; Flight Path Rate or G, at highspeed.




So, if there is no input on the stick:• The aircraft maintains the flight path, even in case of speed changes• In case of configuration changes or thrust variations, the aircraft compensates for the pitching

moment effects• In turbulence, small deviations occur on the flight path. However, the aircraft tends to regain a

steady condition.

AIRBUS PITCH CHARACTERISTIC

Operational Recommendation:

From the moment the aircraft is stable and auto-trimmed, the PF needs to perform minorcorrections on the sidestick, if the aircraft deviates from its intended flight path.The PF should not force the sidestick, or overcontrol it. If the PF suspects an overcontrol, theyshould release the sidestick.

AT TAKEOFF AND LANDING

The above-mentioned pitch law is not the most appropriate for takeoff and flare, because thestable flight path is not what the PF naturally expects.

Therefore, the computers automatically adapt the control laws to the flight phases:• GROUND LAW: The control law is direct law• FLARE LAW: The control law is a pitch demand law.


Takeoff and landing maneuvers are naturally achieved. For example, a flare requires the PF toapply permanent aft pressure on the sidestick, in order to achieve a progressive flare. Whereas,derotation consists of smoothly flying the nose gear down, by applying slight aft pressure on thesidestick.




LATERAL CHARACTERISTICS

NORMAL CONDITIONS

When the PF performs a lateral input on the sidestick, a roll rate is ordered and naturallyobtained.Therefore, at a bank angle of less than 33 °, with no input on the sidestick, a zero roll rate isordered, and the current bank angle is maintained. Consequently, the aircraft is laterally stable,and no aileron trim is required.

However, lateral law is also a mixture of roll and yaw demand with:‐ Automatic turn coordination‐ Automatic yaw damping‐ Initial yaw damper response to a major aircraft assymetry.

In addition, if the bank angle is less than 33 °, pitch compensation is provided.If the bank angle is greater than 33 °, spiral stability is reintroduced and pitch compensation is nolonger available. This is because, in normal situations, there is no operational reason to fly withsuch high bank angles for a long period of time.

AIRBUS LATERAL CHARACTERISTIC


During a normal turn (bank angle less than 33 °), in level flight:• The PF moves the sidestick laterally (the more the sidestick is moved laterally, the greater

the resulting roll rate - e.g. 15 °/s at max deflection)• It is not necessary to make a pitch correction• It is not necessary to use the rudder.

In the case of steep turns (bank angle greater than 33 °), the PF must apply:• Lateral pressure on the sidestick to maintain bank• Aft pressure on the sidestick to maintain level flight.




ENGINE FAILURE

In flight, if an engine failure occurs, and no input is applied on the sidestick, lateral normal lawcontrols the natural tendency of the aircraft to roll and yaw.If no input is applied on the sidestick, the aircraft will reach an approximate 5 ° constant bankangle, a constant sideslip, and a slowly-diverging heading rate.The lateral behavior of aircraft is safe.However, the PF is best suited to adapt the lateral trimming technique, when necessary. Froma performance standpoint, the most effective flying technique, in the event of an engine failureat takeoff, is to fly a constant heading with roll surfaces retracted. This technique dictates theamount of rudder that is required, and the resulting residual sideslip.As a result, to indicate the amount of rudder that is required to correctly fly with an engine-outat takeoff, the measured sideslip index is shifted on the PFD by the computed, residual-sideslipvalue. This index appears in blue, instead of in yellow, and is referred to as the beta target. If therudder pedal is pressed to center the beta target index, the PF will fly with the residual slip, asrequired by the engine-out condition. Therefore, the aircraft will fly at a constant heading withailerons and spoilers close to neutral position.

BETA TARGET ON PFD


In the case of an engine failure at takeoff, the PF must:• Smoothly adjust pitch to maintain a safe speed (as per SRS guidance)• Center the Beta target (there is no hurry, because the aircraft is laterally safe)• When appropriate, trim the aircraft laterally using the rudder trim• Apply small lateral sidestick inputs, so that the aircraft flies the appropriate heading.

AVAILABLE PROTECTIONS

Normal Law provides five different protections (Refer to the "Protections" paragraph):• High angle-of-attack protection• Load factor protection• High pitch attitude protection• Bank angle protection• High speed protection.




ALTERNATE LAWIdent.: OP-020-00005429.0001001 / 29 MAY 08Criteria: SA�Applicable to: ALL

In some double failure cases, the integrity and redundancy of the computers and of the peripherals arenot sufficient to achieve normal law and associated protections. System degradation is progressive,and will evolve according to the availability of remaining peripherals or computers.

Alternate law characteristics (usually triggered in case of a dual failure):‐ In pitch: same as in normal law with FLARE in DIRECT‐ In roll: Roll DIRECT‐ Most protections are lost, except Load factor protection.

At the flight envelope limit, the aircraft is not protected, i.e.:‐ In high speed, natural aircraft static stability is restored with an overspeed warning‐ In low speed (at a speed threshold that is below VLS), the automatic pitch trim stops and natural

longitudinal static stability is restored, with a stall warning at 1.03 VS1G.

In certain failure cases, such as the loss of VS1G computation or the loss of two ADRs, thelongitudinal static stability cannot be restored at low speed. In the case of a loss of three ADRs, itcannot be restored at high speed.In alternate law, VMO setting is reduced to 320 kt, and α FLOOR is inhibited. (On A318, MMO settingis also reduced to M 0.77.)

OPERATIONAL RECOMMENDATION:

The handling characteristics within the normal flight envelope, are identical in pitch with normal law.Outside the normal flight envelope, the PF must take appropriate preventive actions to avoid losingcontrol, and/or avoid high speed excursions. These actions are the same as those that would beapplied in any case where non protected aircraft (e.g. in case of stall warning: add thrust, reducepitch, check speedbrakes retracted).

DIRECT LAWIdent.: OP-020-00005430.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

In most triple failure cases, direct law triggers.

When this occurs:• Elevator deflection is proportional to stick deflection. Maximum deflection depends on the

configuration and on the CG




• Aileron and spoiler deflections are proportional to stick deflection, but vary with the aircraftconfiguration

• Pitch trim is commanded manually

Handling characteristics are natural, of high-quality aircraft, almost independent of the configurationand of the CG. Therefore, the aircraft obviously has no protections, no automatic pitch trim, butoverspeed or stall warnings.


The PF must avoid performing large thrust changes, or sudden speedbrake movements, particularlyif the center of gravity is aft. If the speedbrakes are out, and the aircraft has been re-trimmed, thePF must gently retract the speedbrakes, to give time to retrim, and thereby avoid a large, nose-downtrim change.

INDICATIONSIdent.: OP-020-00005431.0001001 / 27 JUN 08Criteria: SA�Applicable to: ALL

The ECAM and PFD indicate any control law degradation.

ON THE ECAM

In ALTN Law:FLT CTL ALTN LAW (PROT LOST)MAX SPEED 320 kt(320 kt/M 0.77 on A318)In Direct Law:FLT CTL DIRECT LAW (PROT LOST)MAX SPEED 320 kt/M 0.77MAN PITCH TRIM USE

ON THE PFD

The PFD enhances the PF’s awarness of the status of flight controls.Specific symbols (= in green), and specific formatting of low speed information on the speed scale innormal law, indicate which protections are available.When protections are lost, amber crosses (X) appear, instead of the green protection symbols (=).When automatic pitch trim is no longer available, the PFD indicates this with an amber “USE MANPITCH TRIM” message below the FMA.




Fly-by-Wire Status Awareness via the PFD

Therefore, by simply looking at this main instrument (PFD), the flight crew is immediately aware ofthe status of flight controls, and the operational consequences.

PROTECTIONSIdent.: OP-020-00005434.0001001 / 27 JUN 08Criteria: SA�

1 Applicable to: MSN 0031, 0034, 0040-0041, 0043, 0045-0051, 0056-0058, 0074-0075, 0080, 0089-0090, 0095-0097, 0113-0114, 0118,0121, 0125, 0152-0153, 0160, 0171, 0185, 0191-0192, 0197, 0206, 0208, 0213, 0221-0222, 0230, 0234, 0247, 0252, 0259-0263, 0272-0273,0275-0276, 0281-0282, 0294, 0296-0298, 0301, 0306-0307, 0318-0321, 0325, 0329, 0332, 0338-0340, 0345, 0347, 0353, 0355, 0358,0360-0361, 0367-0369, 0372-0375, 0380-0381, 0387-0388, 0395-0400, 0406-0410, 0416-0419, 0423, 0431-0432, 0441, 0451, 0467, 0469, 0478

OBJECTIVES

One of the PF's primary tasks is to maintain the aircraft within the limits of the normal flightenvelope. However, some circumstances, due to extreme situations or aircraft mishandling, mayprovoke the violation of these limits.Despite system protections, the PF must not deliberately exceed the normal flight envelope. Inaddition, these protections are not designed to be structural limit protections (e.g. opposite rudderpedal inputs). Rather, they are designed to assist the PF in emergency and stressful situations,where only instinctive and rapid reactions will be effective.

Protections are intended to:• Provide full authority to the PF to consistently achieve the best possible aircraft performance in

extreme conditions• Reduce the risks of overcontrolling, or overstressing the aircraft• Provide PF with an instinctive and immediate procedure to ensure that the PF achieves the best

possible result.

BANK ANGLE PROTECTION

Bank angle protection prevents that any major upset, or PF mishandling, causes the aircraft tobe in a high-bank situation (wherein aircraft recovery is complex, due to the difficulty to properlyassess such a situation and readily react). Bank angle protection provides the PF with full authorityto efficiently achieve any required roll maneuver.




The maximum achievable bank angle is plus or minus:• 67 °, within the Normal Flight envelope (2.5 g level flight)• 40 °, in high Speed protection (to prevent spiral dive)• 45 °, in high Angle-Of-Attack protection

HIGH SPEED PROTECTION

When flying beyond maximum design speeds VD/MD (which are greater that VMO/MMO), there isan increased potential for aircraft control difficulties and structural concerns, due to high air loads.Therefore, the margin between VMO/MMO and VD/MD must be such that any possible overshoot ofthe normal flight envelope should not cause any major difficulty.High speed protection adds a positive nose-up G demand to a sidestick order, in order to protect theaircraft, in the event of a dive or vertical upset. As a result, this enables a reduction in the marginbetwen VMO/MMO and VD/MD.

Therefore, in a dive situation:• If there is no sidestick input on the sidestick, the aircraft will slightly overshoot VMO/MMO and fly

back towards the envelope.• If the sidestick is maintained full forward, the aircraft will significantly overshoot VMO/MMO

without reaching VD/MD. At approximately VMO +16 / MMO +0.04, the pitch nose-down authoritysmoothly reduces to zero (which does not mean that the aircraft stabilizes at that speed).

airbus HIGH SPEED PROTECTION

The PF, therefore, has full authority to perform a high speed/steep dive escape maneuver, whenrequired, via a reflex action on the sidestick.




Note: 1. An OVERSPEED warning is provided.2. At high altitude, this may result in activation of the angle of attack protection.

Depending on the ELAC standard, the crew may have to push on the stick to get out ofthis protection law.

LOAD FACTOR PROTECTION

On commercial aircraft, high load factors can be encountered during evasive maneuvers due topotential collisions, or CFIT …Pulling "g" is efficient, if the resulting maneuver is really flown with this "g" number. If the aircraft isnot able to fly this trajectory, or to perform this maneuver, pulling "g" will be detrimental.

On commercial aircraft, the maximum load that is structurally allowed is:• 2.5 g in clean configuration,• 2.0 g with the flaps extended.

AIRBUS LOAD FACTOR PROTECTION and safety

On most commercial aircraft, the potential for an efficient 2.5 g maneuver is very remote.Furthermore, as G Load information is not continuously provided in the cockpit, airline pilots are notused to controlling this parameter. This is further evidenced by inflight experience, which revealsthat: In emergency situations, initial PF reaction on a yoke or sidestick is hesitant, then aggressive.With load factor protection, the PF may immediately and instinctively pull the sidestick full aft: Theaircraft will initially fly a 2.5 g maneuver without losing time. Then, if the PF still needs to maintainthe sidestick full aft stick, because the danger still exists, then the high AOA protection will take over.Load factor protection enhances this high AOA protection.Load factor protection enables immediate PF reaction, without any risk of overstressing the aircraft.Flight experience has also revealed that an immediate 2.5 g reaction provides larger obstacleclearance, than a hesitant and delayed high G Load maneuver (two-second delay).

HIGH PITCH ATTITUDE PROTECTION

Excessive pitch attitudes, caused by upsets or inappropriate maneuvers, lead to hazardoussituations:• Too high a nose-up ▸ Very rapid energy loss• Too low a nose-down ▸ Very rapid energy gain

Furthermore, there is no emergency situation that requires flying at excessive attitudes. For thesereasons, pitch attitude protection limits pitch attitude to plus 30 °/minus 15 °.




Pitch attitude protection enhances high speed protection, high load factor protection, and high AOAprotection.

HIGH ANGLE-OF-ATTACK (AOA) PROTECTION

High AOA protection enables the PF to pull the sidestick full aft in dangerous situations, and thusconsistently achieve the best possible aircraft lift. This action on the sidestick is instinctive, and thehigh AOA protection minimizes the risk of stalls or control loss.

High AOA protection is an aerodynamic protection:• The PF will notice if the normal flight envelope is exceeded for any reason, because the autopitch

trim will stop, the aircraft will sink to maintain its current AOA (alpha PROT, strong static stability),and a significant change in aircraft behavior will occur.

• If the PF then pulls the sidestick full aft, a maximum AOA (approximately corresponding to CLMax) is commanded. In addition, the speedbrakes will automatically retract, if extended.

airbus AOA PROTECTION

In addition to this aerodynamic protection, there are three more energy features:• If ATHR is in SPEED mode, the speed cannot drop below VLS, even if the target speed is below

VLS• If the angle-of-attack still increases and reaches ALPHA Floor threshold, the A/THR triggers

TOGA thrust and engages (unless in some cases of one engine-out).

In case of an emergency situation, such as Windshear or CFIT, the PF is assisted in order tooptimize aircraft performance via the:• A/THR: Adds thrust to maintain the speed above VLS• ALPHA FLOOR: Provides TOGA thrust• HIGH AOA protection: Provides maximum aerodynamic lift




• Automatic speedbrake retraction: Minimizes drag.

OPERATIONAL RECOMMENDATIONS:

When flying at alpha max, the PF can make gentle turns, if necessary.The PF must not deliberately fly the aircraft in alpha protection, except for brief periods, whenmaximum maneuvering speed is required.If alpha protection is inadvertently entered, the PF must exit it as quickly as possible, by easingthe sidestick forward to reduce the angle-of-attack, while simultaneously adding power (if alphafloor has not yet been activated, or has been cancelled). If alpha floor has been triggered, it mustbe cancelled with the instinctive disconnect pushbutton (on either thrust lever), as soon as a safespeed is resumed.

In case of GPWS/SHEAR:• Set the thrust levers to TOGA• Pull the sidestick to full aft (For shear, fly the SRS, until full aft sidestick).• Initially maintain the wings level

This immediately provides maximum lift/maximum thrust/minimum drag. Therefore, CFIT escapemaneuvers will be much more efficient.

PROTECTED A/C VERSUS NON PROTECTED A/C GO-AROUND TRAJECTORY

The above-illustrated are typical trajectories flown by all protected or not protected aircraft, whenthe PF applies the escape procedure after an aural “ GPWS PULL UP” alert.The graph demonstrates the efficiency of the protection, to ensure a duck-under that is 50 %lower, a bucket-distance that is 50 % shorter, a safety margin that more than doubles (due to aquicker reaction time), and a significant altitude gain (± 250 ft). These characteristics are commonto all protected aircraft, because the escape procedure is easy to achieve, and enables the PF tofly the aircraft at a constant AOA, close to the max AOA. It is much more difficult to fly the stickshaker AOA on an aircraft that is not protected.




Ident.: OP-020-00005434.0002001 / 27 JUN 08Criteria: 22-1022, 22-1038, 22-1052, P3511, P3686, SA�

2 Applicable to: MSN 0002-0029, 0033, 0035-0039, 0042, 0044, 0052-0055, 0059-0073, 0076-0078, 0081-0088, 0091-0094, 0098-0112,0115-0117, 0119-0120, 0122-0124, 0126-0151, 0154-0159, 0161-0170, 0172-0184, 0186-0190, 0193-0196, 0198-0205, 0207, 0209-0212,0214-0220, 0223-0229, 0231-0233, 0235-0246, 0248-0251, 0253-0258, 0264-0270, 0274, 0277-0280, 0283-0293, 0295, 0299-0300, 0302-0305,0308-0317, 0322-0324, 0326-0328, 0330-0331, 0333-0337, 0341-0344, 0346, 0348-0352, 0354, 0356-0357, 0359, 0362-0366, 0370-0371,0376-0379, 0382-0386, 0389-0394, 0401-0405, 0411-0415, 0420-0422, 0424-0430, 0434-0440, 0442-0450, 0452-0466, 0468, 0470-0477,0479-3996

OBJECTIVES

One of the PF's primary tasks is to maintain the aircraft within the limits of the normal flightenvelope. However, some circumstances, due to extreme situations or aircraft mishandling, mayprovoke the violation of these limits.Despite system protections, the PF must not exceed deliberately the normal flight envelope. Inaddition, these protections are not designed to be structural limit protections (e.g. opposite rudderpedal inputs). Rather, they are designed to assist the PF in emergency and stressful situations,where only instinctive and rapid reactions will be effective.

Protections are intended to:• Provide full authority to the PF to consistently achieve the best possible aircraft performance in

extreme conditions• Reduce the risks of overcontrolling, or overstressing the aircraft• Provide PF with an instinctive and immediate procedure to ensure that the PF achieves the best

possible result.

BANK ANGLE PROTECTION

Bank angle protection prevents that any major upset, or PF mishandling, causes the aircraft tobe in a high-bank situation (wherein aircraft recovery is complex, due to the difficulty to properlyassess such a situation and readily react). Bank angle protection provides the PF with full authorityto efficiently achieve any required roll maneuver.

The maximum achievable bank angle is plus or minus:• 67 °, within the Normal Flight envelope (2.5 g level flight)• 40 °, in high Speed protection (to prevent spiral dive)• 45 °, in high Angle-Of-Attack protection

HIGH SPEED PROTECTION

When flying beyond maximum design speeds VD/MD (which are greater that VMO/MMO), there isan increased potential for aircraft control difficulties and structural concerns, due to high air loads.Therefore, the margin between VMO/MMO and VD/MD must be such that any possible overshoot ofthe normal flight envelope should not cause any major difficulty.




High speed protection adds a positive nose-up G demand to a sidestick order, in order to protect theaircraft, in the event of a dive or vertical upset. As a result, this enables a reduction in the marginbetwen VMO/MMO and VD/MD.

Therefore, in a dive situation:• If there is no sidestick input on the sidestick, the aircraft will slightly overshoot VMO/MMO and fly

back towards the envelope.• If the sidestick is maintained full forward, the aircraft will significantly overshoot VMO/MMO

without reaching VD/MD. At approximately VMO +16 / MMO +0.04, the pitch nose-down authoritysmoothly reduces to zero (which does not mean that the aircraft stabilizes at that speed).

airbus HIGH SPEED PROTECTION

The PF, therefore, has full authority to perform a high speed/steep dive escape maneuver, whenrequired, via a reflex action on the sidestick.

Note: 1. An OVERSPEED warning is provided.2. At high altitude, this may result in activation of the angle of attack protection.

Depending on the ELAC standard, the crew may have to push on the stick to get out ofthis protection law.

LOAD FACTOR PROTECTION

On commercial aircraft, high load factors can be encountered during evasive maneuvers due topotential collisions, or CFIT …Pulling "g" is efficient, if the resulting maneuver is really flown with this "g" number. If the aircraft isnot able to fly this trajectory, or to perform this maneuver, pulling "g" will be detrimental.




On commercial aircraft, the maximum load that is structurally allowed is:• 2.5 g in clean configuration,• 2.0 g with the flaps extended.

AIRBUS LOAD FACTOR PROTECTION and safety

On most commercial aircraft, the potential for an efficient 2.5 g maneuver is very remote.Furthermore, as G Load information is not continuously provided in the cockpit, airline pilots are notused to controlling this parameter. This is further evidenced by inflight experience, which revealsthat: In emergency situations, initial PF reaction on a yoke or sidestick is hesitant, then aggressive.With load factor protection, the PF may immediately and instinctively pull the sidestick full aft: Theaircraft will initially fly a 2.5 g maneuver without losing time. Then, if the PF still needs to maintainthe sidestick full aft stick, because the danger still exists, then the high AOA protection will take over.Load factor protection enhances this high AOA protection.Load factor protection enables immediate PF reaction, without any risk of overstressing the aircraft.Flight experience has also revealed that an immediate 2.5 g reaction provides larger obstacleclearance, than a hesitant and delayed high G Load maneuver (two-second delay).

HIGH PITCH ATTITUDE PROTECTION

Excessive pitch attitudes, caused by upsets or inappropriate maneuvers, lead to hazardoussituations:• Too high a nose-up ▸ Very rapid energy loss• Too low a nose-down ▸ Very rapid energy gain

Furthermore, there is no emergency situation that requires flying at excessive attitudes. For thesereasons, pitch attitude protection limits pitch attitude to plus 30 °/minus 15 °.Pitch attitude protection enhances high speed protection, high load factor protection, and high AOAprotection.

HIGH ANGLE-OF-ATTACK (AOA) PROTECTION

High AOA protection enables the PF to pull the sidestick full aft in dangerous situations, and thusconsistently achieve the best possible aircraft lift. This action on the sidestick is instinctive, and thehigh AOA protection minimizes the risk of stalls or control loss.




High AOA protection is an aerodynamic protection:• The PF will notice if the normal flight envelope is exceeded for any reason, because the autopitch

trim will stop, the aircraft will sink to maintain its current AOA (alpha PROT, strong static stability),and a significant change in aircraft behavior will occur.

• If the PF then pulls the sidestick full aft, a maximum AOA (approximately corresponding to CLMax) is commanded. In addition, the speedbrakes will automatically retract, if extended.

airbus AOA PROTECTION

In addition to this aerodynamic protection, there are three more energy features:• If ATHR is in SPEED mode, the speed cannot drop below VLS, even if the target speed is below

VLS• An aural low-energy "SPEED SPEED SPEED" warning, warms the flight crew that the energy of

the aircraft is below a threshold under which they will have to increase thrust, in order to regaina positive flight path angle through pitch control. It is available in CONF 2, CONF 3, and CONFFULL.

The FAC computes the energy level with the following inputs:‐ Aircraft configuration‐ Horizontal deceleration rate‐ Flight path angle

For example, if the aircraft decelerates at 1 kt/sec, and:‐ The FPA is -3 °, the alert will trigger at approximately VLS -8,‐ The FPA is -4 °, the alert will trigger at approximately VLS -2.This alert draws the PF's attention to the SPEED scale, and indicates the need to adjust thrust.It comes immediately before the ALPHA Floor.




• If the angle-of-attack still increases and reaches ALPHA Floor threshold, the A/THR triggersTOGA thrust and engages (unless in some cases of one engine-out).

In case of an emergency situation, such as Windshear or CFIT, the PF is assisted in order tooptimize aircraft performance via the:• A/THR: Adds thrust to maintain the speed above VLS• Low energy warning "SPEED, SPEED, SPEED": Enhances PF awareness• ALPHA FLOOR: Provides TOGA thrust• HIGH AOA protection: Provides maximum aerodynamic lift• Automatic speedbrake retraction: Minimizes drag.

OPERATIONAL RECOMMENDATIONS:

When flying at alpha max, the PF can make gentle turns, if necessary.The PF must not deliberately fly the aircraft in alpha protection, except for brief periods, whenmaximum maneuvering speed is required.If alpha protection is inadvertently entered, the PF must exit it as quickly as possible, by easingthe sidestick forward to reduce the angle-of-attack, while simultaneously adding power (if alphafloor has not yet been activated, or has been cancelled). If alpha floor has been triggered, it mustbe cancelled with the instinctive disconnect pushbutton (on either thrust lever), as soon as a safespeed is resumed.

In case of GPWS/SHEAR:• Set the thrust levers to TOGA• Pull the sidestick to full aft (For shear, fly the SRS, until full aft sidestick).• Initially maintain the wings level

This immediately provides maximum lift/maximum thrust/minimum drag. Therefore, CFIT escapemaneuvers will be much more efficient.

PROTECTED A/C VERSUS NON PROTECTED A/C GO-AROUND TRAJECTORY

The above-illustrated are typical trajectories flown by all protected or not protected aircraft, whenthe PF applies the escape procedure after an aural " GPWS PULL UP" alert.




The graph demonstrates the efficiency of the protection, to ensure a duck-under that is 50 %lower, a bucket-distance that is 50 % shorter, a safety margin that more than doubles (due to aquicker reaction time), and a significant altitude gain (± 250 ft). These characteristics are commonto all protected aircraft, because the escape procedure is easy to achieve, and enables the PF tofly the aircraft at a constant AOA, close to the max AOA. It is much more difficult to fly the stickshaker AOA on an aircraft that is not protected.

MECHANICAL BACKUPIdent.: OP-020-00005432.0001001 / 29 MAY 08Criteria: SA�Applicable to: ALL

The purpose of the mechanical backup is to achieve all safety objectives in MMEL dispatch condition:To manage a temporary and total electrical loss, the temporary loss of five fly-by-wire computers, theloss of both elevators, or the total loss of ailerons and spoilers.It must be noted that it is very unlikely that the mechanical backup will be used, due to the fly-by-wirearchitecture. For example, in case of electrical emergency configuration, or an all-engine flameout,alternate law remains available.In the unlikely event of such a failure, mechanical backup enables the PF to safely stabilize theaircraft, using the rudder and manual pitch trim, while reconfiguring the systems.In such cases, the objective is not to fly the aircraft accurately, but to maintain the aircraft attitude safeand stabilized, in order to allow the restoration of lost systems.The pitch trim wheel is used to control pitch. Any action on the pitch trim wheel should be appliedsmoothly, because the THS effect is significant due to its large size.The rudder provides lateral control, and induces a significant roll with a slight delay. The PF shouldapply some rudder to turn, and wait for the aircraft reaction. To stabilize and level the wings, anticipateby releasing the rudder pedals.A red “MAN PITCH TRIM ONLY” message appears on the PFD to immediately inform the PF that themechanical backup is being used.

back-up indication on PFD




ABNORMAL ATTITUDESIdent.: OP-020-00005433.0001001 / 29 MAY 08Criteria: SA�Applicable to: ALL

If the aircraft is, for any reason, far outside the normal flight envelope and reaches an abnormalattitude, the normal controls are modified and provide the PF with maximum efficiency in regainingnormal attitudes. (An example of a typical reason for being far outside the normal flight envelope wouldbe the avoidance of a mid-air collision).

The so-called "abnormal attitude" law is :• Pitch alternate with load factor protection (without autotrim)• Lateral direct law with yaw alternate

These laws trigger, when extreme values are reached:• Pitch (50 ° up, 30 ° down)• Bank (125 °)• AOA (30 °, -10 °)• Speed (440 kt, 60 kt)• Mach (0.96, 0.1).

It is very unlikely that the aircraft will reach these attitudes, because fly-by-wire provides protection toensure rapid reaction far in advance. This will minimize the effect and potential for such aerodynamicupsets.The effectiveness of fly-by-wire architecture, and the existence of control laws, eliminate the need forupset recovery maneuvers to be trained on protected Airbus aircraft.

SIDESTICK AND TAKEOVER P/BIdent.: OP-020-00005435.0001001 / 29 MAY 08Criteria: SA�Applicable to: ALL

When the Pilot Flying (PF) makes an input on the sidestick, an order (an electrical signal) is sent to thefly-by-wire computer. If the Pilot Not Flying (PNF) also acts on the stick, then both signals/orders areadded.Therefore, as on any other aircraft type, PF and PNF must not act on their sidesticks at the same time.If the PNF (or Instructor) needs to take over, the PNF must press the sidestick takeover pushbutton,and announce: "I have control".If a flight crewmember falls on a sidestick, or a mechanical failure leads to a jammed stick (there is noassociate ECAM caution), the "failed" sidestick order is added to the "non failed" sidestick order.In this case, the other not affected flight crewmember must press the sidestick takeover pushbutton forat least 40 s, in order to deactivate the "failed" sidestick.




A pilot can at any time reactivate a deactivated stick by momentarily pressing the takeover pushbuttonon either stick.In case of a "SIDE STICK FAULT" ECAM warning, due to an electrical failure, the affected sidestickorder (sent to the computer) is forced to zero. This automatically deactivates the affected sidestick.This explains why there is no procedure associated with this warning.


OPERATIONAL PHILOSOPHYAP / FD / ATHR


AUTOPILOT/FLIGHT DIRECTORIdent.: OP-030-00005439.0001001 / 04 JUN 08Criteria: SA�Applicable to: ALL

OBJECTIVE

The Auto Pilot (AP) and Flight Director (FD) assist the flight crew to fly the aircraft within the normalflight envelope, in order to:• Optimize performance in the takeoff, go-around, climb, or descent phases• Follow ATC clearances (lateral or vertical)• Repeatedly fly and land the aircraft with very high accuracy in CAT II and CAT III conditions.

To achieve these objectives:• The AP takes over routine tasks. This gives the Pilot Flying (PF) the necessary time and

resources to assess the overall operational situation.• The FD provides adequate attitude or flight path orders, and enables the PF to accurately fly the

aircraft manually.

MANAGED AND SELECTED MODES

The choice of mode is a strategic decision that is taken by the PF.

Managed modes require:• Good FMS navigation accuracy (or GPS PRIMARY)• An appropriate ACTIVE F-PLN (i.e. the intended lateral and vertical trajectory is entered, and the

sequencing of the F-PLN is monitored).

MAIN INTERFACES WITH THE AP/FD




*The DIR TO function is an exception to this rule.


With the FMS, anticipate flight plan updates by preparing:• EN ROUTE DIVERSIONS• DIVERSION TO ALTN• CIRCLING• LATE CHANGE OF RWY

in the SEC F-PLN. This enables the MCDU to be used for short-term actions.

TASKSHARING AND COMMUNICATIONS

The FCU and MCDU must be used, in accordance with the rules outlined below, in order to ensure:• Safe operation (correct entries made)• Effective inter-pilot communication (knowing each other's intentions)• Comfortable operations (use "available hands", as appropriate)

AP/FD MONITORING

The FMA indicates the status of the AP, FD, and A/THR, and their corresponding operating modes.The PF must monitor the FMA, and announce any FMA changes. The flight crew uses the FCU orMCDU to give orders to the AP/FD. The aircraft is expected to fly in accordance with these orders.

The main concern for the flight crew should be:WHAT IS THE AIRCRAFT EXPECTED TO FLY NOW ?WHAT IS THE AIRCRAFT EXPECTED TO FLY NEXT ?

If the aircraft does not fly as expected:

‐ Or, disengage the AP, and fly the aircraft manually.




AUTOPILOT (AP) OPERATION

The AP can be engaged within the normal flight envelope, 5 s after liftoff and at least 100 ft. Itautomatically disengages, when the aircraft flies significantly outside the normal flight envelopelimits.The AP cannot be engaged, when the aircraft is outside the flight envelope. Flight control laws aredesigned to assist the flight crew to return within the flight envelope, in accordance with the selectedstrategy.

The AP may be used:• For autoland: Down to the aircraft landing rollout, in accordance with the limitations indicated in

the FCOM• For other approaches, down to:

‐ The MDA for straight in Non Precision Approach‐ MDA - 100 ft for circling approach‐ 160 ft for ILS approach with CAT1 displayed on FMA‐ 500 ft for all others phases.

It may also be used, in case of:• Engine failure: Without any restriction, within the demonstrated limits, including autoland• Abnormal configuration (e.g. slats/flaps failure): Down to 500 ft AGL. Extra vigilance is required

in these configurations. The flight crew must be ready to take over, if the aircraft deviates from itsintended, safe flight path.

The sidestick's instinctive disconnect pushbutton should be used to disengage the AP. Instinctiveoverride action on the sidestick consists of pushing or pulling the sidestick, when the AP is engaged.This action disengages the AP, and should be done as per design, i.e. in case of an instinctivereaction (to an AP hard over for example).

USE OF THE FD WITHOUT THE AP

When manually flying the aircraft with the FDs on, the FD bars or the FPD symbol provide lateraland vertical orders, in accordance with the active modes that the flight crew selects.

Therefore:‐ Fly with a centered FD or FPD‐ If not using FD orders, turn off the FD.

It is strongly recommended to turn off both FDs, to ensure that the A/THR is in SPEED mode, if theA/THR is active.




AUTOTHRUST (A/THR)Ident.: OP-030-00005436.0001001 / 19 DEC 08Criteria: P3379, P3437, SA�Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0112-0114, 0119, 0123-0124,0138-0139, 0148, 0151, 0163-0170, 0178-0182, 0189-0190, 0193-0196, 0198, 0205, 0212, 0219, 0221-0222, 0225, 0230, 0243, 0245, 0247,0249-0251, 0256-0258, 0289, 0293-0295, 0299-0301, 0304, 0308, 0314-0317, 0322, 0326-0328, 0334-0336, 0338, 0343-0344, 0348-0349,0351, 0354, 0357, 0362-0363, 0365-0366, 0370-0371, 0376, 0379, 0383, 0386, 0389-0394, 0396-0398, 0402, 0406, 0411, 0413-0414, 0416,0422-0425, 0429-0432, 0437, 0440-0441, 0443-0444, 0446-0448, 0451, 0453, 0455, 0460-0461, 0469, 0471, 0476, 0478, 0480-0482, 0501,0507, 0511, 0531, 0534, 0549, 0554, 0658, 0669, 0685

OBJECTIVE

The A/THR computer (within the FG) interfaces directly with the engine computer, referred to as theFADEC.

The A/THR sends to the FADEC the thrust targets that are needed to:• Obtain and maintain a target speed, when in SPEED mode• Obtain a specific thrust setting (e.g. CLB, IDLE), when in THRUST mode.

INTERFACE

When the A/THR is active, the thrust lever position determines the maximum thrust that the A/THRcan command in SPEED or THRUST mode. Therefore, with A/THR active, thrust levers act as athrust limiter or a thrust-rating panel.The A/THR computer does not drive back the thrust levers. The PF sets them to a specific detent onthe thrust lever range.

The A/THR system provides cues that indicate the energy of the aircraft:• Speed, acceleration, or deceleration, obtained by the speed trend vector• N1, and N1 command on the N1 gauge.

All these cues are in the flight crew’s direct line of vision.In other words, the Thrust Lever Angle (TLA) should not be used to monitor correct A/THRoperation. Neither should the thrust lever position of a conventional autothrottle, be considered acue because, in many hazardous situations, the thrust lever position can be misleading (e.g. enginefailure, thrust lever jammed).




the TLA determines Max thrust for the A/THR

1 NORMAL OPERATIONS

The A/THR can only be active, when the thrust levers are between IDLE and the CLB detent.When the thrust levers are beyond the CLB detent, thrust is controlled manually to the thrust leverAngle, and the A/THR is armed (A/THR appears in blue on the FMA). This means that the A/THRis ready to be re-activated, when the flight crew sets the thrust levers back to the CLB detent (orbelow).

A/THR operating sectors _ all engines operating

AT TAKEOFF

The thrust levers are set either full forward to TOGA, or to the FLX detent. Thrust is manuallycontrolled to the TLA, and A/THR is armed. The FMA indicates this in blue.

AFTER TAKEOFF

When the aircraft reaches THR RED ALT, the flight crew sets the thrust levers back to the CLBdetent. This activates A/THR. MAX CLB will, therefore, be the maximum normal thrust setting thatwill be commanded by the A/THR in CLB, CRZ, DES, or APPR, as required.

THRUST LEVER(S) BELOW THE CLB DETENT

If one thrust lever is set to below the CLB detent, the FMA triggers a LVR ASYM message,as a reminder to the flight crew (e.g. this configuration might be required due to an engine’s




high vibration level). However, if all thrust levers are set to below the CLB detent, with the A/THR active, then CLB or LVR CLB flashes in the first FMA column. This is because there is nooperational reason to be in such a situation, and to permanently limit A/THR authority on allengines. In this case, all thrust levers should either be brought back to the CLB detent, or the A/THR should be set to OFF.

OPERATIONS WITH ONE ENGINE INOPERATIVE

The above-noted principles also apply to an one-engine inoperative situation, except that A/THR canonly be active, when thrust levers are set between IDLE and MCT.

A/THR operating technique: one engine inoperative

In case of engine failure, the thrust levers will be in MCT detent for remainder of the flight. This isbecause MCT is the maximum thrust that can usually be commanded by the A/THR for climb oracceleration, in all flight phases (e.g. CLB, CRZ, DES or APPR ).

TO SET AUTOTHRUST TO OFF

How to set A/THR off

1) USE OF INSTINCTIVE DISCONNECT (I/D) PUSHBUTTON

If the I/D pushbutton is pressed when the thrust levers are in CLB detent, thrust will increase toMAX CLB. This may cause a not desired thrust change. For example, during approach, A/THR in




SPEED mode, commands approximately N1 55 %. If the PF presses the I/D pushbutton, the A/THR is set to off, and thrust goes to MAX CLB. This will perturbate the approach.

Therefore, the recommended technique for setting A/THR to off is:‐ Return the thrust levers to approximately the current thrust setting, by observing the TLA

symbol on the thrust gauge‐ Press the I/D pushbutton

This technique minimizes thrust discontinuity, when setting A/THR to off.recommended technique to set A/THR to off

2) THRUST LEVERS SET TO IDLE

If thrust levers are set to IDLE, A/THR is set to off. This technique is usually used in descent,when the A/THR is in THR IDLE, or at landing. During flare, with the A/THR active, the thrustlevers are set to the CLB detent. Then, when thrust reduction is required for landing, the thrustlevers should be moved rapidly and set to the IDLE stop. This will retard thrust, and set A/THR tooff. As a reminder, the "RETARD" aural alert will sound. In flare, this aural alert will occur at 20 ft,except in the case of autoland, where it occurs at 10 ft.It should be noted that, when the thrust levers are set back to IDLE and A/THR set to off: The A/THR can be reactivated by pressing the pushbutton on the FCU, and returning the thrust levers tothe applicable detent. The thrust levers should be immediately returned to the applicable detent, inorder to avoid flashing CLB or LVR CLB message on the first FMA column.

3) USE OF THE FCU PUSHBUTTON

Use of the FCU pushbutton is considered to be an involuntary A/THR off command (e.g. in thecase of a failure). When pressed, thrust is frozen and remains locked at the value it had when theflight crew pressed the A/THR pushbutton, as long as the thrust levers remain in the CLB or MCTdetent.If thrust levers are out of detent, thrust is manually controlled and, therefore, unlocked.A THR LK message appears in amber on the FMAIn this case, when the flight crew moves the thrust levers out of detent, full manual control isrecovered, and the THR LK message disappears from the FMA.This feature should not be used, unless the instinctive disconnect pushbuttons are inoperative.




ALPHA FLOOR

When the aircraft's angle-of-attack goes beyond the ALPHA FLOOR threshold, this means that theaircraft has decelerated significantly (below ALPHA PROT speed): A/THR activates automaticallyand orders TOGA thrust, regardless of the thrust lever position.

The example below illustrates that:• The aircraft is in descent with the thrust levers manually set to IDLE.• The aircraft decelerates, during manual flight with the FD off, as indicated on the FMA.

Speed scale and FMA indication in a typical A Floor Case

When the speed decreases, so that the angle-of-attack reaches the ALPHA FLOOR threshold, A/THR activates and orders TOGA thrust, despite the fact that the thrust levers are at IDLE.When the aircraft accelerates again, the angle-of-attack drops below the ALPHA FLOOR threshold.TOGA thrust is maintained or locked. This enables the flight crew to reduce thrust, as necessary.TOGA LK appears on the FMA to indicate that TOGA thrust is locked. The desired thrust can only berecovered by setting A/THR to off, with the instinctive disconnect pushbutton.ALPHA floor is available, when the flight controls are in NORMAL LAW, from liftoff to 100 ft RA atlanding. It is inhibited in some cases of engine failure.

A/THR USE - SUMMARY

Use of A/THR is recommended during the entire flight. It may be used in most failures cases,including:• Engine failure, even during autoland• Abnormal configurations




A/THR use in flight

A/THR should be monitored via the:• FMA – SPEED / SPEED TREND on the PFD• N1/N1 command (EPR) on the ECAM E/WD.

Ident.: OP-030-00005436.0002001 / 19 DEC 08Criteria: 22-1026, P3379, P3476, SA, 318-100�

2 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0111, 0115-0118, 0120-0122,0125-0137, 0140-0147, 0149-0150, 0152-0162, 0171-0177, 0183-0188, 0191-0192, 0197, 0199-0204, 0206-0211, 0213-0218, 0220, 0223-0224,0226-0229, 0231-0242, 0244, 0246, 0248, 0252-0255, 0259-0288, 0290-0292, 0296-0298, 0302-0303, 0305-0307, 0309-0313, 0318-0321,0323-0325, 0329-0333, 0337, 0339-0342, 0345-0347, 0350, 0352-0353, 0355-0356, 0358-0361, 0364, 0367-0369, 0372-0375, 0377-0378,0380-0382, 0384-0385, 0387-0388, 0395, 0399-0401, 0403-0405, 0407-0410, 0412, 0415, 0417-0421, 0426-0428, 0434-0436, 0438-0439,0442, 0445, 0449-0450, 0452, 0454, 0456-0459, 0462-0468, 0470, 0472-0475, 0477, 0479, 0483-0500, 0502-0506, 0508-0510, 0512-0530,0532-0533, 0535-0548, 0550-0553, 0555-0657, 0659-0668, 0670-0684, 0686-3996

OBJECTIVE

The A/THR computer (within the FG) interfaces directly with the engine computer, referred to as theFADEC.

The A/THR sends to the FADEC the thrust targets that are needed to:• Obtain and maintain a target speed, when in SPEED mode• Obtain a specific thrust setting (e.g. CLB, IDLE), when in THRUST mode.

INTERFACE

When the A/THR is active, the thrust lever position determines the maximum thrust that the A/THRcan command in SPEED or THRUST mode. Therefore, with A/THR active, thrust levers act as athrust limiter or a thrust-rating panel.




The A/THR computer does not drive back the thrust levers. The PF sets them to a specific detent onthe thrust lever range.

The A/THR system provides cues that indicate the energy of the aircraft:• Speed, acceleration, or deceleration, obtained by the speed trend vector• N1, and N1 command on the N1 gauge.

All these cues are in the flight crew’s direct line of vision.In other words, the Thrust Lever Angle (TLA) should not be used to monitor correct A/THRoperation. Neither should the thrust lever position of a conventional autothrottle, be considered acue because, in many hazardous situations, the thrust lever position can be misleading (e.g. enginefailure, thrust lever jammed).

The TLP determines MAX Thrust for the A/THR

3 NORMAL OPERATIONS

The A/THR can only be active, when the thrust levers are between IDLE and the CLB detent.When the thrust levers are beyond the CLB detent, thrust is controlled manually to the thrust leverAngle, and the A/THR is armed . This means that the A/THR is ready to be re-activated, when theflight crew sets the thrust levers back to the CLB detent (or below).A/THR appears in blue on theFMA.

A/THR operating sectors _ all engines operating




AT TAKEOFF

The thrust levers are set either full forward to TOGA, or to the FLX detent. Thrust is manuallycontrolled to the TLA, and A/THR is armed. The FMA indicates this in blue.

AFTER TAKEOFF

When the aircraft reaches THR RED ALT, the flight crew sets the thrust levers back to the CLBdetent. This activates A/THR. MAX CLB will, therefore, be the maximum normal thrust setting thatwill be commanded by the A/THR in CLB, CRZ, DES, or APPR, as required.

THRUST LEVER(S) BELOW THE CLB DETENT

If one thrust lever is set to below the CLB detent, the FMA triggers a LVR ASYM message,as a reminder to the flight crew (e.g. this configuration might be required due to an engine’shigh vibration level). However, if all thrust levers are set to below the CLB detent, with the A/THR active, then the ECAM repeatedly triggers the AUTO FLT A/THR LIMITED caution. This isbecause there is no operational reason to be in such a situation, and to permanently limit A/THRauthority on all engines. In this case, all thrust levers should either be brought back to the CLBdetent, or the A/THR should be set to OFF.

OPERATIONS WITH ONE ENGINE INOPERATIVE

The above-noted principles also apply to an one-engine inoperative situation, except that A/THR canonly be active, when thrust levers are set between IDLE and MCT.

A/THR operating sectors - one engine inoperative

In case of engine failure, the thrust levers will be in MCT detent for remainder of the flight. This isbecause MCT is the maximum thrust that can usually be commanded by the A/THR for climb oracceleration, in all flight phases (e.g. CLB, CRZ, DES or APPR ).




TO SET AUTOTHRUST TO OFF

How to set A/THR off

1) USE OF INSTINCTIVE DISCONNECT (I/D) PUSHBUTTON

If the I/D pushbutton is pressed when the thrust levers are in CLB detent, thrust will increase toMAX CLB. This may cause a not desired thrust change. For example, during approach, A/THR inSPEED mode, commands approximately N1 55 %. If the PF presses the I/D pushbutton, the A/THR is set to off, and thrust goes to MAX CLB. This will perturbate the approach.

Therefore, the recommended technique for setting A/THR to off is:‐ Return the thrust levers to approximately the current thrust setting, by observing the TLA

symbol on the thrust gauge‐ Press the I/D pushbutton

This technique minimizes thrust discontinuity, when setting A/THR to off.recommended technique to set A/THR off

2) THRUST LEVERS SET TO IDLE

If thrust levers are set to IDLE, A/THR is set to off. This technique is usually used in descent,when the A/THR is in THR IDLE, or at landing. During flare, with the A/THR active, the thrustlevers are set to the CLB detent. Then, when thrust reduction is required for landing, the thrustlevers should be moved rapidly and set to the IDLE stop. This will retard thrust, and set A/THR to




off. As a reminder, the "RETARD" aural alert will sound. In flare, this aural alert will occur at 20 ft,except in the case of autoland, where it occurs at 10 ft.It should be noted that, when the thrust levers are set back to IDLE and A/THR set to off: The A/THR can be reactivated by pressing the pushbutton on the FCU, and returning the thrust levers tothe applicable detent. The thrust levers should be immediately returned to the applicable detent, inorder to avoid an ECAM "AUTO FLT A/THR LIMITED" message

3) USE OF THE FCU PUSHBUTTON

Use of the FCU pushbutton is considered to be an involuntary A/THR off command (e.g. in thecase of a failure). When pressed, thrust is frozen and remains locked at the value it had when theflight crew pressed the A/THR pushbutton, as long as the thrust levers remain in the CLB or MCTdetent.If thrust levers are out of detent, thrust is manually controlled and, therefore, unlocked.

An ECAM caution and an FMA message trigger during thrust lock:‐ THR LK appears in amber on the FMA‐ The ECAM caution is:

AUTOFLT: A/THR OFFTHRLEVERS

MOVE

ENG: THRUST LOCKEDTHRLEVERS

MOVE

In this case, when the flight crew moves the thrust levers out of detent, full manual control isrecovered, and the THRUST LOCKED message disappears from the FMA.This feature should not be used, unless the instinctive disconnect pushbuttons are inoperative.

ALPHA FLOOR

When the aircraft's angle-of-attack goes beyond the ALPHA FLOOR threshold, this means that theaircraft has decelerated significantly (below ALPHA PROT speed): A/THR activates automaticallyand orders TOGA thrust, regardless of the thrust lever position.

The example below illustrates that:• The aircraft is in descent with the thrust levers manually set to IDLE.• The aircraft decelerates, during manual flight with the FD off, as indicated on the FMA.




Speed scale and FMA indications in a typical A floor case

When the speed decreases, so that the angle-of-attack reaches the ALPHA FLOOR threshold, A/THR activates and orders TOGA thrust, despite the fact that the thrust levers are at IDLE.When the aircraft accelerates again, the angle-of-attack drops below the ALPHA FLOOR threshold.TOGA thrust is maintained or locked. This enables the flight crew to reduce thrust, as necessary.TOGA LK appears on the FMA to indicate that TOGA thrust is locked. The desired thrust can only berecovered by setting A/THR to off, with the instinctive disconnect pushbutton.ALPHA floor is available, when the flight controls are in NORMAL LAW, from liftoff to 100 ft RA atlanding. It is inhibited in some cases of engine failure.

A/THR USE - SUMMARY

Use of A/THR is recommended during the entire flight.

It may be used in most failures cases, including:• Engine failure, even during autoland• Abnormal configurations

A/THR use in flight




A/THR should be monitored via the:• FMA – SPEED / SPEED TREND on the PFD• N1/N1 command (EPR) on the ECAM E/WD.

AP, FD, A/THR MODE CHANGES AND REVERSIONSIdent.: OP-030-00005437.0001001 / 26 MAR 08Criteria: P4320, P5983, SA�

4 Applicable to: MSN 0003, 0016, 0021-0029, 0033, 0035-0039, 0042-0043, 0045-0059, 0064-0068, 0073-0077, 0080-0082, 0084-0085,0087-0091, 0095-0099, 0102-0103, 0109, 0112-0115, 0119-0120, 0122-0124, 0126-0127, 0132, 0134, 0136, 0138-0143, 0146, 0148-0151, 0154,0157-0159, 0163-0164, 0167-0170, 0173-0177, 0179-0183, 0185, 0189-0191, 0193, 0195-0196, 0199, 0203-0205, 0207, 0210-0212, 0215,0219-0225, 0229-0234, 0237, 0240-0257, 0259-0261, 0264-0266, 0274-0277, 0279-0280, 0283-0284, 0288-0296, 0299-0305, 0308-0317,0320-0328, 0330-0336, 0338, 0341-0345, 0347-0350, 0353-0354, 0356-0357, 0359, 0361-0365, 0368-0371, 0373-0376, 0378-0379,0383-0386, 0389-0398, 0402-0407, 0409, 0411, 0413-0416, 0419-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487,0489-0490, 0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0534, 0537-0540,0542-0543, 0546, 0549, 0551-0552, 0554-0555, 0557-0558, 0561, 0565, 0568-0572, 0575, 0579-0582, 0584, 0587, 0589-0592, 0594,0597, 0601, 0604-0607, 0611, 0613-0615, 0617, 0619-0620, 0622, 0624, 0626, 0628, 0630-0634, 0638-0639, 0645, 0648-0650, 0655-0656,0658-0659, 0661-0662, 0666-0667, 0669-0672, 0675, 0677-0678, 0682-0683, 0685, 0688, 0691, 0693, 0695, 0697, 0702, 0711, 0714, 0719,0721, 0726, 0728, 0731-0732, 0736, 0739-0740, 0742-0743, 0746, 0751-0752, 0756-0759, 0762, 0768-0770, 0773, 0775-0776, 0779-0781,0784-0785, 0787, 0791-0792, 0795, 0797, 0800, 0802-0803, 0805, 0808, 0811-0814, 0816-0817, 0820, 0822-0824, 0826, 0829, 0831, 0834,0836, 0839-0840, 0842, 0845, 0851-0852, 0856-0857, 0865-0866, 0869, 0877, 0880, 0888, 0963, 1008, 1042, 1204, 1227

INTRODUCTION

The flight crew manually engages the modes.

However, they may change automatically, depending on the:• AP, FD, and A/THR system integration• Logical sequence of modes• So-called "mode reversions".

AP, FD, ATHR SYSTEM INTEGRATION

There is a direct relationship between aircraft pitch control, and engine thrust control. Thisrelationship is designed to manage the aircraft’s energy.• If the AP/FD pitch mode controls a vertical trajectory (e.g. ALT, V/S, FPA, G/S):

A/THR controls speed• If the AP/FD pitch mode controls a speed (e.g. OP CLB, OP DES):

A/THR controls thrust (THR CLB, THR IDLE)• If no AP/FD pitch mode is engaged (i.e. AP is off and FD is off):

A/THR controls speed

Therefore, any change in the AP/FD pitch mode is associated with a change in the A/THR mode.

Note: For this reason, the FMA displays the A/THR mode and the AP/FD vertical mode columnsnext to each other.




THE LOGICAL SEQUENCE OF MODES

In climb, when the flight crew selects a climb mode, they usually define an altitude target, and expectthe aircraft to capture and track this altitude. Therefore, when the flight crew selects a climb mode,the next logical mode is automatically armed.For example:

AP/FD mode capture and tracking (1)

The flight crew may also manually arm a mode in advance, so that the AP/FD intercepts a definedtrajectory.Typically, the flight crew may arm NAV, LOC-G/S, and APPNAV-FINAL. When the capture ortracking conditions occur, the mode will change sequentially.


These logical mode changes occur, when the modes are armed. They appear in blue on the FMA.

MODE REVERSIONS

GENERAL

Mode reversions are automatic mode changes that unexpectedly occur, but are designed toensure coherent AP, FD, and A/THR operations, in conjunction with flight crew input (or whenentering a F-PLN discontinuity).

For example, a reversion will occur, when the flight crew:• Changes the FCU ALT target in specific conditions• Engages a mode on one axis, that will automatically disengage the associated mode on the

other axis

Due to the unexpected nature of their occurrence, the FMA should be closely-monitored for modereversions.




FLIGHT CREW CHANGE OF FCU ALT TARGET ▸ ACTIVE VERTICAL MODE NOT POSSIBLE

FCU change resulting reversion to VS mode

This reversion to the V/S (FPA) mode on the current V/S target does not modify the pitchbehaviour of the aircraft.It is the flight crew's responsibility to change it as required.

FLIGHT CREW HDG OR TRK MODE ENGAGEMENT ▸ DISENGAGEMENT OF ASSOCIATEDMODE ON THE VERTICAL AXIS

This reversion is due to the integration of the AP, FD, and A/THR with the FMS.

When the flight crew defines a F-PLN, the FMS considers this F-PLN as a whole (lateral +vertical). Therefore, the AP will guide the aircraft along the entire F-PLN:• Along the LAT F-PLN (NAV – APP NAV modes)• Along the VERT F-PLN (CLB – DES – FINAL modes).

Vertical managed modes can only be used, if the lateral managed NAV mode is used. If the flightcrew decides to divert from the lateral F-PLN, the autopilot will no longer guide the aircraft alongthe vertical F-PLN.Therefore, in climb:

Lateral mode change and vertical mode reversion

In descent:Lateral mode change and vertical mode reversion

This reversion to V/S (FPA) mode on the current V/S target does not modify the pitch behavior ofthe aircraft. It is the flight crew’s responsibility to adapt pitch, if necessary.




THE AIRCRAFT ENTERS A F-PLN DISCONTINUITY

NAV mode is lost, when entering a F-PLN discontinuity. On the lateral axis, the aircraft revertsto HDG (or TRK) mode. On the vertical axis, the same reversion (as the one indicated above)occurs.

THE PF MANUALLY FLIES THE AIRCRAFT WITH THE FD ON, AND DOES NOT FOLLOW THEFD PITCH ORDERS

If the flight crew does not follow the FD pitch orders, an A/THR mode reversion occurs. Thisreversion is effective, when the A/THR is in THRUST MODE (THR IDLE, THR CLB), and theaircraft reaches the limits of the speed envelope (VLS, VMAX):

reversion to speed mode




Ident.: OP-030-00005437.0002001 / 26 MAR 08Criteria: 22-1072, P4320, SA�

5 Applicable to: MSN 0002, 0005-0014, 0019-0020, 0031, 0034, 0040-0041, 0044, 0061-0063, 0069-0072, 0078, 0083, 0086, 0093-0094,0100-0101, 0104-0108, 0110-0111, 0116-0118, 0121, 0125, 0128-0131, 0133, 0135, 0137, 0144-0145, 0147, 0152-0153, 0155-0156, 0160-0162,0165-0166, 0171-0172, 0178, 0184, 0186-0188, 0192, 0194, 0197-0198, 0200-0202, 0206, 0208-0209, 0213-0214, 0216-0218, 0226-0228,0235-0236, 0239, 0258, 0262-0263, 0267-0273, 0278, 0281-0282, 0285-0287, 0297-0298, 0306-0307, 0318-0319, 0329, 0337, 0339-0340,0346, 0351-0352, 0355, 0358, 0360, 0366-0367, 0372, 0377, 0380-0382, 0387-0388, 0399-0401, 0408, 0410, 0412, 0417-0418, 0434, 0458,0468, 0473-0474, 0477, 0484, 0488, 0491, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522, 0524, 0526, 0529, 0532-0533, 0535, 0541,0544-0545, 0548, 0550, 0553, 0556, 0559-0560, 0562-0564, 0566-0567, 0573-0574, 0576-0578, 0583, 0585-0586, 0588, 0593, 0595-0596,0598-0600, 0603, 0608-0610, 0612, 0616, 0618, 0621, 0623, 0625, 0627, 0629, 0635-0637, 0640-0644, 0646-0647, 0651-0654, 0657,0660, 0663-0665, 0668, 0673-0674, 0676, 0679-0681, 0684, 0686-0687, 0689-0690, 0692, 0694, 0696, 0698-0701, 0703-0710, 0712-0713,0715-0718, 0720, 0722-0725, 0727, 0729-0730, 0733-0735, 0737-0738, 0741, 0744-0745, 0747-0750, 0754-0755, 0760-0761, 0763-0767,0771-0772, 0774, 0777-0778, 0782-0783, 0786, 0788-0790, 0793-0794, 0796, 0798-0799, 0801, 0804, 0806-0807, 0809-0810, 0815,0818-0819, 0821, 0825, 0827-0828, 0830, 0832-0833, 0835, 0837-0838, 0841, 0843-0844, 0846-0850, 0853-0855, 0858-0864, 0867-0868,0870-0876, 0878-0879, 0881-0887, 0889-0962, 0964-1007, 1009-1041, 1043-1203, 1205-1226, 1228-3996

INTRODUCTION

The flight crew manually engages the modes.

However, they may change automatically, depending on the:• AP, FD, and A/THR system integration• Logical sequence of modes• So-called "mode reversions".

AP, FD, ATHR SYSTEM INTEGRATION

There is a direct relationship between aircraft pitch control, and engine thrust control. Thisrelationship is designed to manage the aircraft’s energy.• If the AP/FD pitch mode controls a vertical trajectory (e.g. ALT, V/S, FPA, G/S):

A/THR controls speed• If the AP/FD pitch mode controls a speed (e.g. OP CLB, OP DES):

A/THR controls thrust (THR CLB, THR IDLE)• If no AP/FD pitch mode is engaged (i.e. AP is off and FD is off):

A/THR controls speed

Therefore, any change in the AP/FD pitch mode is associated with a change in the A/THR mode.

Note: For this reason, the FMA displays the A/THR mode and the AP/FD vertical mode columnsnext to each other.

THE LOGICAL SEQUENCE OF MODES

In climb, when the flight crew selects a climb mode, they usually define an altitude target, and expectthe aircraft to capture and track this altitude. Therefore, when the flight crew selects a climb mode,the next logical mode is automatically armed.For example:





The flight crew may also manually arm a mode in advance, so that the AP/FD intercepts a definedtrajectory.Typically, the flight crew may arm NAV, LOC-G/S, and APPNAV-FINAL. When the capture ortracking conditions occur, the mode will change sequentially.


These logical mode changes occur, when the modes are armed. They appear in blue on the FMA.

MODE REVERSIONS

GENERAL

Mode reversions are automatic mode changes that unexpectedly occur, but are designed toensure coherent AP, FD, and A/THR operations, in conjunction with flight crew input (or whenentering a F-PLN discontinuity).

For example, a reversion will occur, when the flight crew:• Changes the FCU ALT target in specific conditions• Engages a mode on one axis, that will automatically disengage the associated mode on the

other axis• Manually flies the aircraft with the FD on, but does not follow the FD orders, which leads to the

aircraft to the limits of the flight envelope.

Due to the unexpected nature of their occurrence, the FMA should be closely-monitored for modereversions.

FLIGHT CREW CHANGE OF FCU ALT TARGET ▸ ACTIVE VERTICAL MODE NOT POSSIBLE

FCU change resulting reversion to VS mode




This reversion to the V/S (FPA) mode on the current V/S target does not modify the pitchbehaviour of the aircraft.It is the flight crew's responsibility to change it as required.

FLIGHT CREW HDG OR TRK MODE ENGAGEMENT ▸ DISENGAGEMENT OF ASSOCIATEDMODE ON THE VERTICAL AXIS

This reversion is due to the integration of the AP, FD, and A/THR with the FMS.When the flight crew defines a F-PLN, the FMS considers this F-PLN as a whole (lateral +vertical).

Therefore, the AP will guide the aircraft along the entire F-PLN:• Along the LAT F-PLN (NAV – APP NAV modes)• Along the VERT F-PLN (CLB – DES – FINAL modes).

Vertical managed modes can only be used, if the lateral managed NAV mode is used. If the flightcrew decides to divert from the lateral F-PLN, the autopilot will no longer guide the aircraft alongthe vertical F-PLN.Therefore, in climb:

Lateral mode change and vertical mode reversion

In descent:Lateral mode change and vertical mode reversion

This reversion to V/S (FPA) mode on the current V/S target does not modify the pitch behavior ofthe aircraft. It is the flight crew’s responsibility to adapt pitch, if necessary.

THE AIRCRAFT ENTERS A F-PLN DISCONTINUITY

NAV mode is lost, when entering a F-PLN discontinuity. On the lateral axis, the aircraft revertsto HDG (or TRK) mode. On the vertical axis, the same reversion (as the one indicated above)occurs.




THE PF MANUALLY FLIES THE AIRCRAFT WITH THE FD ON, AND DOES NOT FOLLOW THEFD PITCH ORDERS

If the flight crew does not follow the FD pitch orders, an A/THR mode reversion occurs. Thisreversion is effective, when the A/THR is in THRUST MODE (THR IDLE, THR CLB), and theaircraft reaches the limits of the speed envelope (VLS, VMAX):

Reversion to speed mode

A/THR in SPEED mode automatically readjusts thrust to regain the target speed. The FD bars willdisappear, because they are not being followed by the PF.

TRIPLE CLICKIdent.: OP-030-00005438.0001001 / 26 MAR 08Criteria: 22-1123, P7790�

6 Applicable to: MSN 0002-0021, 0033, 0044, 0061-0063, 0100-0102, 0108, 0115, 0128-0131, 0133, 0144-0145, 0155-0156, 0184, 0186-0188,0203, 0214-0215, 0220, 0226-0228, 0235-0239, 0244, 0270, 0278, 0285-0287, 0337, 0352, 0377, 0491, 0498, 0509, 0521, 0529, 0544, 0598,0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0777, 0796, 0938, 0985, 0998, 1000, 1020, 1025, 1036, 1133, 1137, 1150-1151, 1189-1190,1201, 1216, 1267, 1271, 1299, 1344, 1387, 1404, 1415, 1444, 1449, 1458, 1471, 1476, 1478, 1502, 1505, 1524, 1599, 1616, 1622, 1640, 1645,1658, 1660, 1677, 1691, 1699, 1733, 1794, 1859, 1873, 1878-1879, 1885, 1894, 1900, 1924, 1928, 1938-1939, 1949, 1951-1953, 1956, 1967,1977, 1991, 2015, 2017, 2019, 2021, 2023-2026, 2028, 2030, 2032-2033, 2035, 2037, 2039, 2041, 2043, 2045, 2047, 2050-2053, 2055, 2057,2059-2060, 2062, 2064, 2066-2067, 2069, 2071-2072, 2074, 2076-2103, 2105-2136, 2138-2142, 2144-2156, 2158-2224, 2226-2241, 2243-2247,2249-2251, 2253-2310, 2312-2380, 2382-2390, 2392-2471, 2473-2487, 2489-2562, 2564-2598, 2600-3996

The "triple click" is an aural alert. It is an attention-getter, designed to draw the flight crew's attention tothe FMA.The PFD FMA highlights a mode change or reversion with a white box around the new mode, and thepulsing of its associated FD bar.The reversions, described in the previous paragraph, are also emphasized via the triple click auralalert.




Note: The triple click also appears in the following, less usual, cases:• SRS ▸ CLB (OPCLB) reversion: If, the flight crew selects a speed on the FCU• The V/S selection is "refused" during ALT *: The flight crew pulls the V/S knob, while in

ALT*• The V/S target is not followed, because the selected target is too high, and leads to

VMIN/VMAX.


OPERATIONAL PHILOSOPHYECAM


PURPOSE OF THE ECAMIdent.: OP-040-00005443.0001001 / 09 JUN 08Criteria: SA�Applicable to: ALL

The Electronic Centralized Aircraft Monitoring (ECAM) system is a main component of Airbus’ two-crewmember cockpit, which also takes the "dark cockpit" and "forward-facing crew" philosophies intoaccount.

The purpose of the ECAM is to:• Display aircraft system information• Monitor aircraft systems• Indicate required flight crew actions, in most normal, abnormal and emergency situations.

As the ECAM is available in most failure situations, it is a significant step in the direction towards apaperless cockpit and the reduction of memory items.

MAIN PRINCIPLESIdent.: OP-040-00005444.0001001 / 02 JUN 08Criteria: SA�Applicable to: ALL

INFORMATION PROVIDED WHEN NEEDED

One of the main advantages of the ECAM is that it displays applicable information to the flight crew,on an "as needed" basis. The following outlines the ECAM’s operating modes:• Normal Mode:

Automatically displays systems and memos, in accordance with the flight phase.• Failure Mode:

Automatically displays the appropriate emergency/abnormal procedures, in addition to theirassociated system synoptic.

• Advisory Mode:Automatically displays the appropriate system synoptic, associated with a drifting parameter.

• Manual Mode:Enables the flight crew to manually select any system synoptic via the ECAM Control Panel(ECP).

Most warnings and cautions are inhibited during critical phases of flight (T/O INHIBIT – LDGINHIBIT), because most system failures will not affect the aircraft’s ability to continue a takeoff orlanding.




FAILURE LEVELS

The ECAM has three levels of warnings and cautions. Each level is based on the associatedoperational consequence(s) of the failure. Failures will appear in a specific color, according toa defined color-coding system, that advises the flight crew of the urgency of a situation in aninstinctive, unambiguous manner. In addition, Level 2 and 3 failures are accompanied by a specificaural warning: A Continuous Repetitive Chime (CRC) indicates a Level 3 failure, and a Single Chime(SC) indicates a Level 2 failure.

Failure Level Priority Color Coding Aural Warning Recommended Crew ActionLevel 3 Safety Red CRC ImmediateLevel 2 Abnormal Amber SC Awareness, then actionLevel 1 Degradation Amber None Awareness, then Monitoring

When there are several failures, the FWC displays them on the Engine Warning Display (E/WD) inan order of priority, determined by the severity of the operational consequences. This ensures thatthe flight crew sees the most important failures first.

FEEDBACK

The ECAM provides the flight crew with feedback, after action is taken on affected controls:• The System Synoptic:

Displays the status change of affected components.• The Memo:

Displays the status of a number of systems selected by the flight crew (e.g. anti ice).• The Procedures:

When the flight crew performs a required action on the cockpit panel, the ECAM usually clearsthe applicable line of the checklist (except for some systems or actions, for which feedback is notavailable).

The ECAM reacts to both failures and pilot action.

ECAM HANDLINGIdent.: OP-040-00005445.0001001 / 26 JUN 08Criteria: SA�Applicable to: ALL

Task sharing is essential to effective ECAM operation, particularly in the case of abnormal operations.

NORMAL OPERATIONS

On ground, the ECAM MEMO is reviewed for feedback on temporarily-selected items (e.g. SEATBELTS/IGNITION/ENG A/I), and to check whether IRs are aligned. If alignment is not complete, thetime remaining will be displayed. It is, therefore, not necessary to refer to the OVHD panel.




In cruise, the main systems should periodically be reviewed during flight (ENG, BLEED, ELECAC/DC, HYD, FUEL, F/CTL), to ensure that they are operating normally, and to detect any potentialproblem in advance.The ECAM MEMO must be included in the instrument review. In cruise, in most of the cases, itshould be blank. It helps to make the flight crew aware of any system that a flight crewmembertemporarily selected, but forgot to deselect.A STS label, displayed at the bottom of the E/WD, indicates that there is a STATUS to be reviewed.Therefore, when a C/L calls for STATUS review, press STS, only if the label appears.If there is a STS at engine shutdown, it will pulse at the bottom of the E/WD. If this is the case, theSTATUS page should be reviewed for help in completing the technical log.

ADVISORY MODE

The flight crewmember that first notices an advisory announces: "ADVISORY on XYZ system".Then, the PF requests the PNF to review the drifting parameter. If time permits, the PNF may referto the QRH non normal procedures section, containing recommended actions in various advisorysituations.

FAILURE MODE

TASK SHARING RULES

When the ECAM displays a warning or a caution, the first priority is to ensure that a safe flightpath is maintained. The successful outcome of any ECAM procedure depends on: Correctreading and application of the procedure, effective task sharing, and conscious monitoring andcrosschecking.

It is important to remember that, after ECAM ACTIONS announcement by the PF:• The PF’s task is to fly the aircraft, navigate, and communicate.• The PNF’s task is to manage the failure, on PF command.

The PF usually remains the PF for the entire flight, unless the Captain decides to take control.The PF will then control the aircraft’s flight path, speed, configuration, and engines. The PF willalso manage navigation and communication, and initiate the ECAM actions to be performed bythe PNF, and check that the actions are completed correctly.The PNF has a considerable workload: Managing ECAM actions and assisting the PF on request.The PNF reads the ECAM and checklist, performs ECAM actions on PF command, requests PFconfirmation to clear actions, and performs actions required by the PF. The PNF never touchesthe thrust levers, even if requested by the ECAM.Some selectors or pushbuttons (including the ENG MASTER switch, FIRE pushbutton, IR, IDGand, in general, all guarded switches) must be completely crosschecked by both the PF andPNF, before they are moved or selected, to prevent the flight crew from inadvertently performingirreversible actions.




To avoid mistakes in identifying the switches, Airbus’ overhead panels are designed to beuncluttered. When the ECAM requires action on overhead panel pushbuttons or switches,the correct system panel can be identified by referring to the white name of the system on theside of each panel. Before performing any action, the PNF should keep this sequence in mind:"System, then procedure/selector, then action" (e.g. "air, crossbleed, close"). This approach, andannouncing an intended selection before action, enables the PNF to keep the PF aware of theprogress of the procedure.It is important to remember that, if a system fails, the associated FAULT light on the systempushbutton (located on the overhead panel) will come on in amber, and enable correctidentification.When selecting a system switch or pushbutton, the PNF should check the SD to verify that theselected action has occurred (e.g. closing the crossbleed valve should change the indications thatappear on the SD).




Crew Coordination

1. The PNF should review the overhead panel and/or associated SD to analyze and confirm thefailure, prior to taking any action, and should bear in mind that the sensors used for the SD maybe different from the sensors that trigger the failure.

2. In case of a failure during takeoff or go-around, ECAM actions should be delayed untilthe aircraft reaches approximately 400 ft, and is stabilized on a safe trajectory. This is anappropriate compromise between stabilizing the aircraft and delaying action.

3. When the ECAM displays several failures, the sequence (action, then request and confirmation,before clearance) should be repeated for each failure. When all necessary actions arecompleted, amber messages and red titles will no longer appear on the E/WD.

4. When the ECAM displays several system pages, the sequence (request and confirmationbefore clearance) should be repeated for each system page.




5. The PF may call out "STOP ECAM" at any time, if other specific actions must be performed(normal C/L, or performing a computer reset). When the action is completed, the PF must callout: "CONTINUE ECAM".

6. When slats are extended, the SD automatically displays the STATUS, unless if the page isempty. The STS should be carefully reviewed, and the required procedure applied.

7. When ECAM actions have been completed, and the ECAM status has been reviewed, the PNFmay refer to the FCOM procedure for supplementary information, if time permits. However, incritical situations the flight should not be prolonged only to consult the FCOM.

IF THE ECAM WARNING (OR CAUTION) DISAPPEARS WHILE APPLYING THE PROCEDURE

If an ECAM warning disappears, while a procedure is being applied, the warning can beconsidered no longer applicable. Application of the procedure can be stopped.For example, during the application of an engine fire procedure, if the fire is successfullyextinguished with the first fire extinguisher bottle, the ENG FIRE warning disappears, and theprocedure no longer applies. Any remaining ECAM procedures should be performed as usual.

SOME ADDITIONAL REMARKS

• There are very few memory items:‐ Emergency descent initiation‐ Immediate actions, in case of an unreliable speed indication‐ Loss of braking‐ Windshear (reactive and predictive)‐ EGPWS and GPWS‐ TCAS

• LAND ASAP (As Soon As Possible):‐ RED LAND ASAP :

Land as soon as possible at the nearest suitable airport at which a safe approach andlanding can be made.

‐ AMBER LAND ASAP:Advice to the flight crew to consider landing at the nearest suitable airport.

Note: The CLOSEST AIRPORTS MCDU page may help the flight crew to determine thenearest suitable airport: This page displays the four airports that are the nearest tothe aircraft's current position. These airports are found in the navigation database,and are displayed regardless of their suitability. The flight crew should keep in mindthat the four closest airports are sorted according to distance, and should refer to theEstimated Time of Arrival (ETA).

• OEB ReminderSome Operational Engineering Bulletins (OEBs) contain information that may impact flight crewaction, in the event of a system failure. OEBs are filed in the QRH.




If the OEB reminder function is activated for an ECAM warning/caution, the ECAM will displaythe : "Refer to QRH Proc" line, when necessary. This line may appear instead of the procedure,or it may be added to the ECAM STATUS.In such failure cases, the flight crew should refer to the applicable procedure in the QRH.

• Some procedures require reference to the QRH

IN CASE OF AN ECAM SYSTEM FAULT

DISPLAY UNIT FAILURE

If one ECAM screen fails, the remaining one will display the E/WD. However, in such a case, if afailure or advisory occurs, the system or status page are not displayed automatically. The PNFcan display a system synoptic on the remaining display unit, by pressing the assigned systempushbutton on the ECP. The synoptic will appear, as long as the pushbutton is pressed.Therefore, in the case of an advisory and/or failure (indicated by an ADV flag that pulses in whiteon the bottom of the E/WD), the PNF must call up the affected system synoptic, by pressing therelated pushbutton.To review two or three pages of status messages: The PNF should release the STS pushbuttonfor less than two seconds, then press and hold it again.

A double ECAM screen configuration can be recovered using the ECAM/ND switching selector:• If the Captain is the PNF, the switch should be set to "CPT".• If the First Officer is the PNF, the switch should be set to "F/O".

The applicable ND screen will then display the second ECAM image.

DMC FAILURES

In case all of the ECAM DMC channels fail, each flight crewmember may display the enginestandby page on their respective ND (generated by the DMCs’ EFIS channel).

ECP FAILURE

In the case of an ECP failure, the CLR, RCL, STS, ALL and EMER CANCEL keys will continue tooperate, because they are hardwired to the FWC/DMC. Therefore, the "ALL" key can be used toscroll all SD pages and display the desired one (by releasing the key, when the desired SD pageappears).

FLUCTUATING CAUTION

Any fluctuating caution can be deleted with the EMER CANCEL pushbutton. When pressed,the EMER CANCEL pushbutton deletes both the aural alert, and the caution for the remainderof the flight. This is indicated on the STATUS page, by the "CANCELLED CAUTION" title. Anycaution messages that have been inhibited via the EMER CANCEL pushbutton can be recalled bypressing and holding the RCL key for more than three seconds.




The EMER CANCEL pushbutton inhibits any aural warning that is associated with a red warning,but does not affect the warning itself.

USE OF SUMMARIESIdent.: OP-040-00005446.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

GENERAL

Summaries consist of QRH procedures, and are designed to assist the flight crew to manageapplicable actions, in the event of an EMER ELEC CONFIG or a dual hydraulic failure.In any case, ECAM actions should be applied first (actions and STATUS review). The PNF shouldrefer to the applicable QRH summary, only after announcing: "ECAM ACTIONS COMPLETED".When a failure occurs, and after performing the ECAM actions, the PNF should refer to the"CRUISE" section of the summary, to determine the landing distance coefficient. Due to the fact thatnormal landing distances also appear on this page, the PNF can compute the landing distance withthe failure, and decide whether or not to divert.

APPROACH PREPARATION

As usual, approach preparation includes a review of the ECAM STATUS.After reviewing the STATUS, the PNF should refer to the "CRUISE" section of the summary, todetermine the VREF correction, and compute the VAPP.This assumes that the PNF is aware of the computation method, and uses the VREF displayed onthe MCDU (with the updated destination). The summary provides a VREF table, in the event thatfailure results in the loss of the MCDU.The LANDING and GO-AROUND sections of the summary should be used for the approachbriefing.

APPROACH

To perform the APPR PROC, the APPROACH section of the summary should be read (mainlybecause of the flap extension procedure, that does not entirely appear on the ECAM).This assumes that the recommendations, provided in this part of the summary are sufficient forunderstanding, and that it will not be necessary for the flight crew to consult the "LANDING WITHFLAPS (SLATS) JAMMED” paper procedure.The PNF should then review the ECAM STATUS, and check that all the APPR PROC actionshave been completed.




sequence

NORMAL OPERATIONS


NORMAL OPERATIONSPRELIMINARY PAGES

TABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET NO-PLP-TOC. P 1/6FCTM 09 JAN 09

NO-PLP. PRELIMINARY PAGESTABLE OF CONTENTS........................................................................................................................................... 1/6SUMMARY OF HIGHLIGHTS.................................................................................................................................. 1/8

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NO-010. GENERALINTRODUCTION...................................................................................................................................................... 1/4USE OF NORMAL CHECK LIST.............................................................................................................................1/4COMMUNICATION................................................................................................................................................... 2/4

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NO-020. PRE STARTMEL........................................................................................................................................................................ 1/22HANDLING OF MAINTENANCE MESSAGES ON ECAM STATUS PAGE........................................................... 3/22SECURED AND TRANSIT STOP..........................................................................................................................4/22SAFETY EXTERIOR INSPECTION.......................................................................................................................4/22PRELIMINARY COCKPIT PREPARATION............................................................................................................5/22EXTERIOR INSPECTION...................................................................................................................................... 5/22ADIRS INITIALIZATION......................................................................................................................................... 6/22COCKPIT PREPARATION..................................................................................................................................... 9/22MISCELLANEOUS............................................................................................................................................... 21/22

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NO-030. STARTENGINE AUTO START.......................................................................................................................................... 2/12average idle engine parameters.............................................................................................................................6/12AVERAGE IDLE ENGINE PARAMETERS ............................................................................................................7/12AVERAGE IDLE ENGINE PARAMETERS.............................................................................................................9/12ENGINE START MALFUNCTION.......................................................................................................................... 9/12MANUAL ENGINE START....................................................................................................................................10/12TAILPIPE FIRE..................................................................................................................................................... 10/12ENGINES WARM UP PERIOD............................................................................................................................ 11/12After Start Flow Pattern........................................................................................................................................ 11/12

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NO-040. TAXIPOWERPUSH........................................................................................................................................................ 1/20TAXI ROLL AND STEERING.................................................................................................................................2/20FIGURES................................................................................................................................................................5/20figures..................................................................................................................................................................... 8/20



TABLE OF CONTENTS


BRAKE CHECK....................................................................................................................................................10/20CARBON BRAKE WEAR..................................................................................................................................... 10/20TAXI SPEED AND BRAKING...............................................................................................................................11/20BRAKE TEMPERATURE .....................................................................................................................................11/20BRAKING ANOMALIES........................................................................................................................................12/20Brake Fans .................................................................................................................................................... 14/20

FLIGHT CONTROL CHECK.................................................................................................................................15/20Takeoff Briefing Confirmation............................................................................................................................... 15/20TAXI WITH ONE ENGINE SHUTDOWN............................................................................................................. 16/20MISCELLANEOUS............................................................................................................................................... 18/20TAXI FLOW PATTERN......................................................................................................................................... 19/20

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NO-050. TAKEOFFTHRUST SETTING.................................................................................................................................................2/18TAKEOFF ROLL..................................................................................................................................................... 5/18TYPICAL AIRCRAFT ATTITUDE AT TAKEOFF AFTER LIFT-OFF....................................................................... 6/18ROTATION.............................................................................................................................................................. 6/18AIRCRAFT GEOMETRY .......................................................................................................................................7/18AIRCRAFT GEOMETRY........................................................................................................................................ 8/18TAIL STRIKE AVOIDANCE...................................................................................................................................11/18MAXIMUM DEMONSTRATED CROSSWIND FOR TAKE-OFF ..........................................................................13/18AP ENGAGEMENT ............................................................................................................................................. 14/18VERTICAL PROFILE............................................................................................................................................ 14/18LATERAL PROFILE..............................................................................................................................................15/18THRUST REDUCTION ALTITUDE.......................................................................................................................15/18ACCELERATION ALTITUDE................................................................................................................................ 15/18TAKE-OFF AT HEAVY WEIGHT.......................................................................................................................... 16/18IMMEDIATE TURN AFTER TAKE-OFF................................................................................................................16/18LOW ALTITUDE LEVEL-OFF................................................................................................................................17/18NOISE ABATEMENT TAKE-OFF......................................................................................................................... 17/18

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NO-060. CLIMBGENERAL.................................................................................................................................................................1/8AP/FD CLIMB MODES ........................................................................................................................................... 1/8SPEED CONSIDERATIONS.................................................................................................................................... 5/8VERTICAL PERFORMANCE PREDICTIONS......................................................................................................... 6/8LATERAL NAVIGATION........................................................................................................................................... 6/8



TABLE OF CONTENTS


10 000 ft FLOW PATTERN...................................................................................................................................... 7/8�

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NO-070. CRUISEPREFACE............................................................................................................................................................... 1/24FMS USE................................................................................................................................................................2/24FMS USE: MISCELLANEOUS...............................................................................................................................6/24COST INDEX........................................................................................................................................................10/24SPEED CONSIDERATIONS.................................................................................................................................11/24ALTITUDE CONSIDERATIONS............................................................................................................................13/24STEP CLIMB.........................................................................................................................................................14/24EFFECT OF ALTITUDE ON FUEL CONSUMPTION...........................................................................................17/24FIGURES.............................................................................................................................................................. 17/24FUEL MONITORING............................................................................................................................................ 19/24FUEL TEMPERATURE.........................................................................................................................................20/24APPROACH PREPARATION................................................................................................................................20/24APPROACH BRIEFING........................................................................................................................................22/24

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NO-080. DESCENTPREFACE............................................................................................................................................................... 1/10COMPUTATION PRINCIPLES............................................................................................................................... 1/10GUIDANCE AND MONITORING............................................................................................................................2/10MODE REVERSION...............................................................................................................................................5/10DESCENT CONSTRAINTS....................................................................................................................................7/1010 000 ft FLOW PATTERN.................................................................................................................................... 9/10

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NO-090. HOLDINGPREFACE................................................................................................................................................................. 1/2HOLDING SPEED AND CONFIGURATION............................................................................................................ 1/2IN THE HOLDING PATTERN.................................................................................................................................. 1/2

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NO-100. APPROACH GENERALPREFACE............................................................................................................................................................... 1/22INITIAL APPROACH.............................................................................................................................................. 2/22INTERMEDIATE APPROACH................................................................................................................................ 6/22FINAL APPROACH...............................................................................................................................................10/22VAPP.....................................................................................................................................................................12/22



TABLE OF CONTENTS


GROUND SPEED MINI........................................................................................................................................14/22STEEP APPROACH............................................................................................................................................. 18/22

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NO-110. ILS APPROACHPREFACE................................................................................................................................................................. 1/6INITIAL APPROACH................................................................................................................................................ 1/6INTERMEDIATE APPROACH.................................................................................................................................. 4/6FINAL APPROACH.................................................................................................................................................. 4/6ILS RAW DATA.........................................................................................................................................................5/6

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NO-120. NON PRECISION APPROACHPREFACE................................................................................................................................................................1/14APPROACH STRATEGY........................................................................................................................................ 1/14LIMITATIONS.......................................................................................................................................................... 1/14INITIAL APPROACH...............................................................................................................................................2/14INTERMEDIATE APPROACH................................................................................................................................ 5/14FINAL APPROACH.................................................................................................................................................8/14REACHING THE MINIMA.....................................................................................................................................10/14LOC ONLY APPROACH....................................................................................................................................... 11/14LOC BACK COURSE APPROACH...................................................................................................................... 11/14

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NO-130. CIRCLING APPROACHPREFACE................................................................................................................................................................. 1/4APPROACH PREPARATION................................................................................................................................... 1/4FINAL INSTRUMENT APPROACH..........................................................................................................................2/4CIRCLING APPROACH........................................................................................................................................... 2/4

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NO-140. VISUAL APPROACHINITIAL APPROACH................................................................................................................................................ 1/4INTERMEDIATE/FINAL APPROACH....................................................................................................................... 2/4

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NO-150. PRECISION APPROACHGENERAL.................................................................................................................................................................1/8DEFINITION..............................................................................................................................................................1/8FLIGHT PREPARATION...........................................................................................................................................2/8APPROACH PREPARATION................................................................................................................................... 3/8



TABLE OF CONTENTS


APPROACH PROCEDURE......................................................................................................................................4/8FAILURE AND ASSOCIATED ACTIONS.................................................................................................................7/8AUTOLAND IN CAT 1 OR BETTER WEATHER CONDITIONS..............................................................................7/8

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NO-160. LANDINGPREFACE............................................................................................................................................................... 1/18MAIN GEAR CLEARANCE.................................................................................................................................... 1/18FLARE.................................................................................................................................................................... 2/18MAXIMUM DEMONSTRATED CROSSWIND FOR LANDING.............................................................................. 3/18CALL OUT.............................................................................................................................................................. 4/18DEROTATION......................................................................................................................................................... 5/18ROLL OUT..............................................................................................................................................................6/18BRAKING .............................................................................................................................................................. 6/18FACTORS AFFECTING LANDING DISTANCE..................................................................................................... 9/18CLEARANCE AT TOUCH DOWN........................................................................................................................ 11/18TAIL STRIKE AVOIDANCE...................................................................................................................................16/18

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NO-170. GO AROUNDPREFACE................................................................................................................................................................. 1/8CONSIDERATIONS ABOUT GO-AROUND.............................................................................................................1/8AP/FD GO-AROUND PHASE ACTIVATION............................................................................................................ 2/8GO-AROUND PHASE.............................................................................................................................................. 4/8ENGINES ACCELERATION.....................................................................................................................................5/8LEAVING THE GO-AROUND PHASE ....................................................................................................................6/8REJECTED LANDING............................................................................................................................................. 7/8

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NO-180. TAXI INBRAKE FANS .................................................................................................................................................. 1/6

BRAKE TEMPERATURE......................................................................................................................................... 2/6ENGINES COOLING PERIOD.................................................................................................................................4/6TAXI WITH ONE ENGINE SHUTDOWN................................................................................................................. 5/6AFTER LANDING FLOW PATTERN........................................................................................................................5/6

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TABLE OF CONTENTS






ENV A318/A319/A320/A321 FLEET NO-PLP-SOH. P 1/8FCTM 09 JAN 09

LocalizationTitle

Page ID Reason

NO-020HANDLING OF MAINTENANCEMESSAGES ON ECAM STATUSPAGE

3/22 1 Solution actual effectivity changed: 0006,0017 removed

NO-020HANDLING OF MAINTENANCEMESSAGES ON ECAM STATUSPAGE

4/22 2 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,2500 removed

NO-020ADIRS INITIALIZATION

6/22 3 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3743,3748,3754,3756,3759,3763,3765,3768,3774,3775,3776,3777,3778,3780,3782,3783,3786,3787,3788,3789,3790,3793,3794,3795,3796,3797,3799,3802,3803,3805,3808,3809,3810,3812,3813,3814,3815,3817,3821,3823,3824,3825,3826,3830,3831,3832,3833,3835,3838,3840,3843,3844,3845,3846,3848,3849,3851,3852,3854,3855,3856,3857,3858,3859,3862,3863,3864,3865,3868,3871,3873,3875,3879,3881,3884,3885,3887,3888,3889,3891,3893,3894,3896,3897,3898,3899,3904,3905,3906,3909,3911,3912,3913,3916,3917,3921,3922,3923,3924,3925,3926,3928,3930,3931,3932,3933,3935,3936,3937,3943,3944,3945,3946,3948,3949,3953,3954,3956,3960,3962,3964,3965,3966,3971,3977,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

NO-020ADIRS INITIALIZATION

8/22 4 Solution actual effectivity changed:3736,3739,3741,3745,3747,3750,3752,3753,3757,3758,3760,3761,3762,3764,3766,3767,3769,3770,3771,3772,3773,3779,3781,3784,3785,3791,3792,3798,3800,3801,3804,3806,3807,3811,3816,3818,3819,3820,3822,3827,3828,3829,3834,3836,3837,3839,3841,3847,3850,3853,3860,3861,3866,3867,3869,3872,3874,3876,3877,3878,3880,3882,3883,3886,3890,3892,3895,3900,3901,3902,3903,3907,3908,3910,3915,3918,3919,3920,3927,3934,3938,3939,3940,3941,3947,3950,3951,3952,3955,3959,3967,3968,3969,3970,3972,3981,3983added

NO-020COCKPIT PREPARATION

9/22 5 Solution actual effectivity changed: 1753 added,0006,0017,0207,0224,0274,0844,0861,0885,0890,0896,0904,0922,0929,0972,0992,0997,1019,1033,1038,1040,1044,1046,1051,1052,1055,1061,1065,1069,1095,1097,1109,1112,1114,1122,1135,1141,1182,1203,1205,1224,1245,1254,1264,1268,1269,1275,1277,1287,1289,1297,1298,1301,1310,1313,1315,1317,1326,1328,1331,1340,1342,1348,1354,1358,1369,1371,1378,1383,1388,1389,1403,1407,1412,1417,1425,1431,1442,1447,1455,1461,1462,1465,1472,1484,1492,1496,1499,1517,1525,1530,1531,1536,1539,1651,1666,1701,1704removed

NO-020COCKPIT PREPARATION

15/22 6 Solution actual effectivity changed:0005,0207,0224,0274,0844,0861,0885,0890,0896,0904,0922,0929,0972,0992,0997,1019,1033,1038,1040,1044,1046,1051,1052,1055,1061,1065,1069,1095,1097,1109,1112,1114,1122,1135,1141,1182,1203,1205,1224,1245,1254,1264,1268,1269,1275,1277,1287,1289,1297,1298,1301,1310,1313,1315,1317,1326,1328,1331,1340,1342,1348,1354,1358,1369,1371,1378,1383,1388,1389,1403,1407,1412,1417,1425,1431,1442,1447,1455,1461,1462,1465,1472,1484,1492,1496,1499,1517,1525,1530,1531,1536,1539,1651,1666,1701,1704,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,1753,2500 removed

NO-030ENGINE AUTO START

2/12 1 Solution actual effectivity changed:3591,3716,3734,3736,3741,3743,3745,3748,3753,3757,3759,3760,3761,3764,3768,3770,3771,3772,3773,3775,3779,3782,3783,3784,3785,3793,3796,3797,3800,3801,3803,3804,3807,3811,3812,3816,3820,3821,3829,3832,3836,3837,3839,3841,3847,3849,3850,3851,3858,3860,3862,3863,3864,3867,3869,3873,3876,3877,3878,3881,3890,3893,3897,3899,3901,3902,3904,3910,3911,3912,3916,3917,3920,3924,3926,3927,3934,3935,3936,3937,3938,3941,3943,3944,3947,3948,3951,3959,3960,3962,3964,3965,3966,3968,3969,3977,3981,3989,3993,3995,3996added, 1374,2500 removed


2/12 2 Page revised to modify the condition for starting the secondengine. For harmonization purpose with the FCOM, the PFmust wait for engine stabilization instead of the peak EGT.


4/12 3 Solution actual effectivity changed:0005,3698,3723,3739,3747,3750,3752,3754,3756,3758,3762,3763,3765,3766,3767,3769,3774,3776,3777,3778,3780,3781,3786,3787,3788,3789,3790,3791,3792,3794,3795,3798,3799,3802,3805,3806,3808,3809,3810,3813,3814,3815,3817,3818,3819,3822,3823,3824,3825,3826,3827,3828,3830,3831,3833,3834,3835,3838,3840,3843,3844,3845,3846,3848,3852,3853,3854,3855,3856,3857,3859,3861,3865,3866,3868,3871,3872,3874,3875,3879,3880,3882,3883,3884,3885,3886,3887,3888,3889,3891,3892,3894,3895,3896,3898,3900,3903,3905,3906,3907,3908,3909,3913,3915,3918,3919,3921,3922,3923,3925,3928,3930,3931,3932,3933,3939,3940,3945,3946,3949,3950,3952,3953,3954,3955,3956,3967,3970,3971,3972,3983,3984added, 0004,0006,0017,0036 removed


4/12 4 Page revised to modify the condition for starting the secondengine. For harmonization purpose with the FCOM, the PFmust wait for engine stabilization instead of the peak EGT.

NO-030average idle engine parameters


NO-030AVERAGE IDLE ENGINEPARAMETERS


NO-040POWERPUSH

1/20 1 Solution actual effectivity changed: 0005 added,0004,0006,0017,0036,1374 removed

NO-040POWERPUSH

2/20 2 Solution actual effectivity changed:3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 2500 removed





LocalizationTitle

Page ID Reason

NO-040FIGURES

5/20 3 Solution actual effectivity changed: 3886,3932 added

NO-040FIGURES

6/20 4 Solution actual effectivity changed:3754,3757,3759,3763,3768,3770,3772,3774,3779,3788,3790,3794,3799,3801,3803,3808,3810,3818,3822,3824,3826,3828,3832,3834,3836,3838,3839,3841,3844,3845,3849,3851,3853,3854,3856,3860,3865,3872,3874,3876,3888,3890,3892,3895,3897,3901,3903,3905,3911,3918,3950,3962,3970,3983added

NO-040figures

8/20 5 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3753,3756,3758,3760,3762,3765,3767,3769,3771,3773,3775,3776,3777,3778,3780,3781,3782,3783,3785,3786,3787,3789,3791,3793,3795,3797,3798,3800,3802,3804,3805,3807,3809,3811,3812,3813,3815,3817,3819,3821,3823,3825,3827,3829,3831,3833,3835,3837,3840,3843,3846,3848,3850,3852,3855,3857,3859,3861,3863,3866,3868,3871,3873,3875,3877,3880,3882,3883,3885,3887,3889,3891,3894,3896,3898,3900,3902,3904,3906,3907,3908,3909,3910,3912,3913,3915,3917,3919,3921,3922,3923,3925,3927,3931,3933,3935,3937,3939,3941,3943,3945,3946,3947,3949,3952,3953,3954,3956,3959,3965,3967,3968,3971,3972,3984,3995added, 0004,0006,0017,0036,1374,2500 removed

NO-040figures

9/20 6 Solution actual effectivity changed:3752,3761,3764,3766,3784,3792,3796,3806,3814,3816,3820,3830,3847,3858,3862,3864,3867,3869,3878,3879,3881,3884,3893,3899,3916,3920,3924,3926,3928,3930,3934,3936,3938,3940,3944,3948,3951,3955,3960,3964,3966,3969,3977,3981,3989,3993,3996added

NO-040BRAKE CHECK


NO-040BRAKE CHECK


NO-040BRAKE TEMPERATURE

11/20 9 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

NO-040BRAKING ANOMALIES

12/20 10 Solution actual effectivity changed:0159,0164,0414,1034,1302 added,0004,0006,0017,0053,0054,0067,0076,0077,0098,0099,0109,0119,0120,0123,0124,0126,0127,0130,0134,0136,0143,0146,0152,0154,0157,0163,0165,0166,0167,0170,0175,0177,0178,0183,0194,0196,0198,0203,0205,0207,0208,0212,0213,0219,0220,0223,0224,0233,0240,0241,0242,0245,0246,0248,0250,0253,0254,0262,0264,0266,0274,0276,0278,0282,0289,0300,0303,0317,0319,0322,0323,0328,0329,0334,0351,0357,0358,0365,0366,0373,0375,0383,0384,0390,0393,0405,0409,0413,0415,0426,0428,0430,0447,0455,0460,0461,0467,0480,0482,0497,0498,0501,0507,0511,0520,0522,0527,0530,0531,0534,0537,0541,0543,0545,0549,0554,0559,0562,0566,0575,0580,0590,0594,0595,0601,0605,0607,0611,0612,0614,0617,0619,0621,0627,0636,0640,0647,0648,0649,0650,0651,0658,0660,0661,0668,0669,0670,0675,0676,0680,0685,0687,0688,0691,0693,0695,0699,0707,0709,0710,0712,0715,0718,0720,0721,0722,0724,0725,0732,0752,0754,0760,0761,0772,0799,0806,0808,0813,0828,0835,0844,0845,0857,0859,0861,0863,0864,0868,0869,0875,0876,0880,0883,0885,0887,0890,0892,0896,0897,0901,0906,0909,0911,0913,0914,0921,0925,0932,0933,0936,0937,0939,0943,0950,0958,0963,0964,0966,0967,0968,0972,0973,0974,0976,0981,0984,0986,0988,0990,0992,0996,0997,1005,1010,1011,1019,1021,1026,1027,1028,1030,1033,1035,1037,1038,1041,1042,1044,1045,1046,1050,1051,1052,1055,1061,1063,1064,1065,1067,1069,1070,1072,1074,1075,1079,1080,1083,1088,1093,1095,1097,1099,1101,1103,1108,1109,1110,1111,1112,1116,1119,1134,1135,1140,1141,1148,1153,1154,1159,1164,1166,1174,1177,1178,1182,1196,1200,1203,1204,1207,1208,1213,1221,1223,1224,1228,1233,1234,1235,1239,1247,1254,1255,1261,1262,1264,1265,1268,1270,1275,1279,1285,1288,1292,1294,1295,1298,1303,1310,1312,1314,1316,1317,1319,1320,1326,1328,1329,1330,1331,1340,1342,1345,1348,1354,1357,1358,1360,1361,1362,1365,1369,1371,1374,1377,1378,1380,1382,1384,1386,1389,1391,1393removed

NO-040BRAKING ANOMALIES

13/20 11 Solution actual effectivity changed:0005,0053,0054,0067,0076,0077,0098,0099,0109,0119,0120,0123,0124,0126,0127,0130,0134,0136,0143,0146,0152,0154,0157,0163,0165,0166,0167,0170,0175,0177,0178,0183,0194,0196,0198,0203,0205,0207,0208,0212,0213,0219,0220,0223,0224,0233,0240,0241,0242,0245,0246,0248,0250,0253,0254,0262,0264,0266,0274,0276,0278,0282,0289,0300,0303,0317,0319,0322,0323,0328,0329,0334,0351,0357,0358,0365,0366,0373,0375,0383,0384,0390,0393,0405,0409,0413,0415,0426,0428,0430,0447,0455,0460,0461,0467,0480,0482,0497,0498,0501,0507,0511,0520,0522,0527,0530,0531,0534,0537,0541,0543,0545,0549,0554,0559,0562,0566,0575,0580,0590,0594,0595,0601,0605,0607,0611,0612,0614,0617,0619,0621,0627,0636,0640,0647,0648,0649,0650,0651,0658,0660,0661,0668,0669,0670,0675,0676,0680,0685,0687,0688,0691,0693,0695,0699,0707,0709,0710,0712,0715,0718,0720,0721,0722,0724,0725,0732,0752,0754,0760,0761,0772,0799,0806,0808,0813,0828,0835,0844,0845,0857,0859,0861,0863,0864,0868,0869,0875,0876,0880,0883,0885,0887,0890,0892,0896,0897,0901,0906,0909,0911,0913,0914,0921,0925,0932,0933,0936,0937,0939,0943,0950,0958,0963,0964,0966,0967,0968,0972,0973,0974,0976,0981,0984,0986,0988,0990,0992,0996,0997,1005,1010,1011,1019,1021,1026,1027,1028,1030,1033,1035,1037,1038,1041,1042,1044,1045,1046,1050,1051,1052,1055,1061,1063,1064,1065,1067,1069,1070,1072,1074,1075,1079,1080,1083,1088,1093,1095,1097,1099,1101,1103,1108,1109,1110,1111,1112,1116,1119,1134,1135,1140,1141,1148,1153,1154,1159,1164,1166,1174,1177,1178,1182,1196,1200,1203,1204,1207,1208,1213,1221,1223,1224,1228,1233,1234,1235,1239,1247,1254,1255,1261,1262,1264,1265,1268,1270,1275,1279,1285,1288,1292,1294,1295,1298,1303,1310,1312,1314,1316,1317,1319,1320,1326,1328,1329,1330,1331,1340,1342,1345,1348,1354,1357,1358,1360,1361,1362,1365,1369,1371,1377,1378,1380,1382,1384,1386,1389,1391,1393,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0036,0159,0164,0414,1034,1302,2500 removed

NO-040Brake Fans

14/20 12 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3753,3754,3756,3757,3758,3759,3760,3762,3763,3765,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3785,3786,3787,3788,3789,3790,3791,3793,3794,3795,3797,3798,3799,3800,3801,3802,3803,3804,3805,3807,3808,3809,3810,3811,3812,3813,3815,3817,3818,3819,3821,3822,3823,3824,3825,3826,3827,3828,3829,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3859,3860,3861,3863,3865,3866,3868,3871,3872,3873,3874,3875,3876,3877,3880,3882,3883,3885,3886,3887,3888,3889,3890,3891,3892,3894,3895,3896,3897,3898,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3917,3918,3919,3921,3922,3923,3925,3927,3931,3932,3933,3935,3937,3939,3941,3943,3945,3946,3947,3949,3950,3952,3953,3954,3956,3959,3962,3965,3967,3968,3970,3971,3972,3983,3984,3995added, 0004,0006,0017,0036,1374,2500 removed

NO-040Takeoff Briefing Confirmation

15/20 13 This paragraph is revised in order to highlight that theTAKEOFF BRIEFING CONFIRMATION should be limitedto the review of the changes that may have occurred sincethe TAKEOFF BRIEFING done at the gate. It is actually notnecessary to confirm again information that have not changedand have been already checked during the TAKEOFFBRIEFING.

NO-040TAXI WITH ONE ENGINESHUTDOWN


NO-040TAXI WITH ONE ENGINESHUTDOWN






LocalizationTitle

Page ID Reason

NO-050THRUST SETTING


NO-050THRUST SETTING


NO-050AIRCRAFT GEOMETRY








NO-050MAXIMUM DEMONSTRATEDCROSSWIND FOR TAKE-OFF

13/18 7 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

NO-050MAXIMUM DEMONSTRATEDCROSSWIND FOR TAKE-OFF


NO-050VERTICAL PROFILE

14/18 9 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

NO-060AP/FD CLIMB MODES

1/8 1 Solution actual effectivity changed: 0768,0776,0797 added,0006,0017,0550,0573,0674,0684,0763 removed


2/8 2 Solution actual effectivity changed:0550,0573,0674,0684,0763 added,0768,0776,0797,1374,1951,2024 removed


3/8 3 Solution actual effectivity changed:0002,0005,0007,0010,0012,0013,0014,0019,0020,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491,1951,2024,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 2500 removed


4/8 4 Solution actual effectivity changed:0002,0004,0007,0010,0012,0013,0014,0019,0020,0036,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491removed

NO-070PREFACE

1/24 1 Solution actual effectivity changed: 0389 removed

NO-070PREFACE

1/24 2 Solution actual effectivity changed:0005,0389,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed





LocalizationTitle

Page ID Reason

NO-070FMS USE


NO-070FMS USE


NO-070FMS USE: MISCELLANEOUS



7/24 6 Solution actual effectivity changed:0207,0224,0274,0992,1383,1407,1461,1484,1530,3734,3736,3741,3743,3747,3748,3750,3754,3757,3760,3761,3762,3763,3764,3767,3770,3771,3772,3774,3778,3779,3780,3781,3783,3784,3786,3787,3788,3789,3790,3794,3799,3800,3801,3803,3804,3805,3807,3808,3810,3811,3812,3816,3817,3819,3823,3824,3826,3832,3835,3837,3838,3843,3844,3845,3847,3854,3856,3857,3860,3861,3867,3868,3869,3871,3877,3882,3888,3889,3890,3892,3894,3899,3902,3905,3908,3909,3910,3913,3916,3917,3919,3920,3922,3923,3927,3933,3934,3938,3939,3941,3946,3947,3948,3951,3952,3953,3954,3959,3968,3972,3981added, 1080,1161,1214,1260,1273,1337,1374,1753,2500removed


9/24 7 Solution actual effectivity changed:0005,0844,0861,0885,0890,0896,0904,0922,0929,0972,0997,1019,1033,1038,1040,1044,1046,1051,1052,1055,1061,1065,1069,1080,1095,1097,1109,1112,1114,1122,1135,1141,1161,1182,1203,1205,1214,1224,1245,1254,1260,1264,1268,1269,1273,1275,1277,1287,1289,1297,1298,1301,1310,1313,1315,1317,1326,1328,1331,1337,1340,1342,1348,1354,1358,1369,1371,1378,1388,1389,1403,1412,1417,1425,1431,1442,1447,1455,1462,1465,1472,1492,1496,1499,1517,1525,1531,1536,1539,1651,1666,1701,1704,3591,3698,3716,3723,3739,3745,3752,3753,3756,3758,3759,3765,3766,3768,3769,3773,3775,3776,3777,3782,3785,3791,3792,3793,3795,3796,3797,3798,3802,3806,3809,3813,3814,3815,3818,3820,3821,3822,3825,3827,3828,3829,3830,3831,3833,3834,3836,3839,3840,3841,3846,3848,3849,3850,3851,3852,3853,3855,3858,3859,3862,3863,3864,3865,3866,3872,3873,3874,3875,3876,3878,3879,3880,3881,3883,3884,3885,3886,3887,3891,3893,3895,3896,3897,3898,3900,3901,3903,3904,3906,3907,3911,3912,3915,3918,3921,3924,3925,3926,3928,3930,3931,3932,3935,3936,3937,3940,3943,3944,3945,3949,3950,3955,3956,3960,3962,3964,3965,3966,3967,3969,3970,3971,3977,3983,3984,3989,3993,3995,3996added, 0004,0036 removed

NO-070SPEED CONSIDERATIONS

11/24 8 Solution actual effectivity changed:0006,0017,0207,0224,0274,0992,1461,1484,1530 removed

NO-070SPEED CONSIDERATIONS

12/24 9 Solution actual effectivity changed:0005,0207,0224,0274,0992,1461,1484,1530,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,2500 removed

NO-070STEP CLIMB


NO-070STEP CLIMB


NO-070FIGURES

17/24 12 Solution actual effectivity changed:3757,3759,3768,3770,3772,3779,3801,3803,3832,3839,3841,3860,3890,3911added

NO-070FIGURES


NO-070FIGURES

18/24 14 Solution actual effectivity changed:0712,3591,3716,3734,3736,3741,3743,3745,3748,3753,3760,3771,3773,3775,3782,3783,3785,3793,3797,3800,3804,3807,3811,3812,3829,3837,3850,3863,3873,3877,3902,3904,3910,3912,3917,3927,3935,3937,3941,3943,3947,3959,3965,3968,3995added, 2500 removed

NO-070FIGURES

19/24 15 Solution actual effectivity changed:3761,3764,3784,3796,3816,3820,3847,3858,3862,3864,3867,3869,3878,3881,3893,3899,3916,3920,3924,3926,3934,3936,3938,3944,3948,3951,3960,3964,3966,3969,3977,3981,3989,3993,3996added

NO-080PREFACE

1/10 1 This paragraph is introduced to highlight that the TERR ONND sw can be switched ON before the DESCENT if necessary(especially in mountainous areas).

NO-080MODE REVERSION

5/10 2 Solution actual effectivity changed: 0768,0776,0797 added,0006,0017,0550,0573,0674,0684,0763 removed





LocalizationTitle

Page ID Reason


6/10 3 Solution actual effectivity changed:0550,0573,0674,0684,0763 added,0768,0776,0797,1374,1951,2024 removed


6/10 4 Solution actual effectivity changed:0002,0005,0007,0010,0012,0013,0014,0019,0020,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491,1951,2024,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 2500 removed


6/10 5 Solution actual effectivity changed:0002,0004,0007,0010,0012,0013,0014,0019,0020,0036,0044,0061,0062,0063,0100,0101,0108,0128,0129,0130,0131,0133,0144,0145,0155,0156,0184,0186,0187,0188,0214,0226,0227,0228,0235,0236,0239,0270,0278,0285,0286,0287,0337,0352,0377,0491removed

NO-080DESCENT CONSTRAINTS

7/10 6 Solution actual effectivity changed:0006,0017,0207,0224,0274,0844,0861,0885,0890,0896,0904,0922,0929,0972,0992,0997,1019,1033,1038,1040,1044,1046,1051,1052,1055,1061,1065,1069,1095,1097,1109,1112,1114,1122,1135,1141,1182,1203,1205,1224,1245,1254,1264,1268,1269,1275,1277,1287,1289,1297,1298,1301,1310,1313,1315,1317,1326,1328,1331,1340,1342,1348,1354,1358,1369,1371,1378,1383,1388,1389,1403,1407,1412,1417,1425,1431,1442,1447,1455,1461,1462,1465,1472,1484,1492,1496,1499,1517,1525,1530,1531,1536,1539,1651,1666,1701,1704removed

NO-080DESCENT CONSTRAINTS

8/10 7 Solution actual effectivity changed:0005,0207,0224,0274,0844,0861,0885,0890,0896,0904,0922,0929,0972,0992,0997,1019,1033,1038,1040,1044,1046,1051,1052,1055,1061,1065,1069,1095,1097,1109,1112,1114,1122,1135,1141,1182,1203,1205,1224,1245,1254,1264,1268,1269,1275,1277,1287,1289,1297,1298,1301,1310,1313,1315,1317,1326,1328,1331,1340,1342,1348,1354,1358,1369,1371,1378,1383,1388,1389,1403,1407,1412,1417,1425,1431,1442,1447,1455,1461,1462,1465,1472,1484,1492,1496,1499,1517,1525,1530,1531,1536,1539,1651,1666,1701,1704,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,2500 removed

NO-100INITIAL APPROACH




NO-100INTERMEDIATE APPROACH




NO-100VAPP

12/22 5 Solution actual effectivity changed: 0005 added,0004,0006,0017,0036 removed

NO-100VAPP

13/22 6 Solution actual effectivity changed:3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 1374,2500 removed

NO-100GROUND SPEED MINI


NO-100GROUND SPEED MINI


NO-100STEEP APPROACH

18/22 9 Solution actual effectivity changed: 3932 added


1/6 1 Solution actual effectivity changed:0006,0017,0213,0325,0348,0375,0409,0497,0537,0988,1828removed





LocalizationTitle

Page ID Reason


3/6 2 Solution actual effectivity changed:0005,0213,0325,0348,0375,0409,0497,0537,0988,1828,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,2500 removed




2/14 2 The table is revised to clarify that it is possible to perform aSelected NPA when the NAV accuracy is high. The previoustable seemed to state that it was not possible which was nottrue and led to misunderstandings concerning the associatedND settings.


3/14 3 Solution actual effectivity changed:0005,0213,0325,0348,0375,0409,0497,0537,0988,1828,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0036,1374,2500 removed


3/14 4 The table is revised to clarify that it is possible to perform aSelected NPA when the NAV accuracy is high. The previoustable seemed to state that it was not possible which was nottrue and led to misunderstandings concerning the associatedND settings.





NO-120FINAL APPROACH


NO-120FINAL APPROACH


NO-120LOC BACK COURSE APPROACH

11/14 9 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3814,3815,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3831,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3846,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3876,3877,3878,3879,3880,3881,3882,3883,3884,3885,3886,3887,3888,3889,3890,3891,3893,3894,3895,3896,3897,3898,3899,3900,3901,3902,3903,3904,3905,3906,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3921,3922,3923,3924,3925,3926,3927,3928,3930,3931,3932,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3956,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

NO-120LOC BACK COURSE APPROACH

12/14 10 Solution actual effectivity changed:3765,3776,3813,3875,3892 added





NO-160FLARE

2/18 1 Addition of information concerning the retard of the thrustlevers, following the "RETARD" auto call-out.





LocalizationTitle

Page ID Reason

NO-160MAXIMUM DEMONSTRATEDCROSSWIND FOR LANDING


NO-160MAXIMUM DEMONSTRATEDCROSSWIND FOR LANDING


NO-160CALL OUT


NO-160CALL OUT


NO-160CLEARANCE AT TOUCH DOWN








NO-170AP/FD GO-AROUND PHASEACTIVATION


NO-170AP/FD GO-AROUND PHASEACTIVATION


NO-170GO-AROUND PHASE


NO-170GO-AROUND PHASE







4/6 3 Solution actual effectivity changed:0664,1021,1027,1199,1218,1554,1681,1716,2357,2381,2599,3752,3761,3764,3766,3784,3792,3796,3806,3814,3816,3820,3830,3847,3858,3862,3864,3867,3869,3878,3879,3881,3884,3893,3899,3916,3920,3924,3926,3928,3930,3934,3936,3938,3940,3944,3948,3951,3955,3960,3964,3966,3969,3977,3981,3989,3993,3996added


NORMAL OPERATIONSGENERAL

ENV A318/A319/A320/A321 FLEET NO-010. P 1/4FCTM 08 JUL 08

INTRODUCTIONIdent.: NO-010-00005440.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The NORMAL OPERATIONS Chapter outlines the techniques that should be applied for each flightphase, in order to optimize the use of Airbus aircraft. This chapter must be read in parallel with theFCOM, which provides normal procedures, and their associated tasksharing, callouts, and checklists.All of these flying techniques are applicable to normal conditions.Other techniques applicable to adverse weather conditions, Refer to SI-010 GENERAL.There are flow patterns at the end of some flight phases to indicate where the actions are to beperformed. All flight crewmembers must apply the flow patterns, to ensure that the flight crew performsthe actions necessary for a specific flight phase, before completing an applicable checklist.

USE OF NORMAL CHECK LISTIdent.: NO-010-00005441.0001001 / 27 JUN 08Criteria: SA�Applicable to: ALL

Airbus' NORMAL CHECKLIST takes into account ECAM information, and includes only those itemsthat can directly impact flight safety and efficiency, if actions are not correctly performed. Thesechecklists are of a "non-action" type (i.e. all actions should be completed from memory before the flightcrew performs the checklist).The NORMAL CHECKLIST includes 9 flight phases. The BEFORE START, BEFORE TAKEOFF, andAFTER TAKEOFF checklists are divided in two sections: The "Down to the Line" section, and the"Below the Line" section. This format is designed to help flight crews to manage the workload.For example, the "BEFORE START - Down to the Line" checklist may be called out, as soon as theLoad and Trim Sheet is available and takeoff data is set. On the other hand, the "BEFORE START -Below the Line" checklist may be called out after obtaining start-up clearance.The Pilot Flying (PF) requests the NORMAL CHECKLIST, and the Pilot Non Flying (PNF) reads it.The checklist actions are referred to as "challenge/response"-type actions. The PF "responds" to the"challenge" only after checking the current status of the aircraft.If the configuration does not correspond to the checklist response, the PF must take corrective actionbefore "responding" to the "challenge". If corrective action is not possible, then the PF must modifythe response to reflect the real situation (with a specific answer). When necessary, the other flightcrewmember must crosscheck the validity of the response. The challenger (PNF) waits for a responsebefore proceeding with the checklist. For the checklist items that are identified as "AS RQRD", theresponse should correspond to the real condition or configuration of the system.The PNF must announce "LANDING CHECKLIST COMPLETED", after reading and completing thechecklist.




COMMUNICATIONIdent.: NO-010-00005442.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

EMERGENCY CALL

Some abnormal/emergency procedures require flight and cabin crews to use specific phraseologywhen communicating with each other. To ensure effective communication between the flight andcabin crews, the standard phraseology may be recalled at the preflight phase.

FROM TO PHRASEOLOGY REMARKScockpit cabin Passenger Address (PA) System:

"PURSER TO COCKPIT, PLEASE!"The Purser, or any other cabin

crewmember, must go to the cockpitCockpit Cabin Passenger Address (PA) System:

"ATTENTION CREW! AT STATIONS!"An emergency evacuation may soon be required.

cockpit cabin Passenger Address (PA) System:"CABIN CREW and PASSEN-

GERS REMAIN SEATED!"

The captain decides that anevacuation is not required

cockpit cabin Passenger Address (PA) System:"PASSENGERS EVACUATE!"

The captain orders an immediate evacuation

cabin cockpit Interphone:"PRIO CAPT"

Any crew member can make sucha call. The flight crew must reply.

CROSS-COCKPIT COMMUNICATION

The term "cross-cockpit communication" refers to communication between the PF and the PNF.This communication is vital for any flight crew. Each time one flight crewmember adjusts or changesinformation and/or equipment on the flight deck, the other flight crewmember must be notified, andan acknowledgement must be obtained.

Such adjustments and changes include:• FMGS alterations• Changes in speed or Mach• Tuning navigation aids• Flight path modifications• System selections (e.g. anti-ice system).

When using cross-cockpit communication, standard phraseology is essential to ensure effectiveflight crew communication. This phraseology should be concise and exact, and is defined in theFCOM (Refer to FCOM/PRO-NOR-SOP-27 COMMUNICATIONS AND STANDARD TERMS).

The flight crew must use the headset:• From the ENGINE START phase until the TOP OF CLIMB phase• From The TOP OF DESCENT phase until the aircraft is parked.




STERILE COCKPIT RULE

When the aircraft is below 10 000 ft, any conversation that is not essential should be avoided: Thisincludes conversations that take place in the cockpit, or between the flight and cabin crewmembers.It is important to adhere to this policy, in order to facilitate communication between both of theflight crew, and to ensure the effective communication of emergency or safety-related information,between flight and cabin crew members.


NORMAL OPERATIONSPRE START


MELIdent.: NO-020-00005447.0001001 / 11 JUN 08Criteria: SA�Applicable to: ALL

GENERAL

The Master Minimum Equipment List (MMEL) is published by the aircraft manufacturer. It is acertified document that enables an aircraft to be dispatched, with some equipment, or functionsinoperative. Some limitations, operational procedures and/or maintenance procedures may have tobe performed. The Minimum Equipment List (MEL) is published by the operator, and approved bylocal authorities. It must be at least as restrictive as MMEL. The MMEL cannot be used to replacethe MEL.Aircraft can be dispatched with one, or more, secondary airframe part/parts missing. In this case,the flight crew must refer to the Configuration Deviation List (CDL), in the Aircraft Flight Manual.

MMEL PHILOSOPHY

To introduce an item in the MMEL, the manufacturer must demonstrate first that the consequencesof the system failure are no more than minor on the flight. The manufacturer must demonstrate then,that the next critical failure, i.e. the failure that has the most critical effect on aircraft operation whenadded to the initial failure, maintains the level of safety.In some cases, this level of safety is maintained provided (o) or (m) procedures are observed.As an example, the aircraft dispatch with one pack inoperative induces a flight level limitationwhereas a pack failure in flight does not induce a flight level limitation.

ATA 100 FORMAT

All items/equipment listed in the MEL are identified using the Air Transport Association (ATA) format.The ATA is the official reference for the classification of aircraft systems and/or functions. Theaircraft systems/functions are classified with six digits.

For example, 21-52-01 refers to:21: ATA 21: Air conditioning52: Air-cooling system01: Air conditioning pack

MEL DESCRIPTION

The MEL has four parts:• ECAM warnings/ MEL entry• List of items that may be inoperative for dispatch• Associated operational procedures• Associated maintenance procedures




MEL OPERATIONAL USE

The MEL usually applies to revenue flights, and should be consulted before taxi out. If a failureoccurs during taxi out, and before the take off roll starts, the decision to continue the flight is subjectto pilot judgment and good airmanship. The Captain may consult the MEL before deciding tocontinue the flight (particularly if the failure has an effect on the takeoff performance).During preliminary cockpit preparation, the flight crew must press the RCL P/B, for at least 3 s, inorder to recall any previous cautions or warnings that have been cleared or cancelled. The flightcrew should consult the technical logbook to confirm that the indications are compatible with theMEL.A failure may occur if a Circuit Breaker (C/B) disengages. When on ground, do not re-engage anyfuel pump C/Bs. The flight crew may re-engage any other tripped C/Bs, provided that the action iscoordinated with the maintenance team, and the cause of the tripped C/B is identified.The MEL section 0 is called ECAM Warnings/MEL Entry. The purpose of this section is to help theflight crew to determine the MEL entry point, when an ECAM caution/warning message triggers. TheECAM Warnings/MEL Entry section provides the relationship between the ECAM caution/warnings,and MEL items, if applicable.If a failed item does not appear in the MEL, it is not possible to dispatch the aircraft. However, itemsthat do not affect the airworthiness of the aircraft, such as galley equipment, entertainment systems,or passenger convenience items, do not appear in the MEL: The dispatch applicability of these itemsis not relevant to the MEL.

In most cases, if the failed item appears in the MEL, the dispatch of the aircraft is authorized,provided that all dispatch conditions are fulfilled:• Check the rectification time interval has not expired• Consider location and, where repair is possible• (*) Means that an INOP placard is required• (O) Means that a specific operational procedure or limitation is required (all listed in the MEL

OPERATIONAL PROCEDURES Chapter)• (M) Means that a specific maintenance procedure is required.

When the MEL requires both maintenance and operational procedures, the maintenance proceduresmust be performed before applying the operational procedures.




MMEL symbol

If some items are mandatory for ETOPS dispatch, a mention "ER" (Extended Range) is added butmandatory items for CATII, CATIII operations, RNP and RVSM may be not mentioned in the MMEL.However, the MEL should include these requirements.

If it is not the case,• Mandatory items for CATII/III are available in QRH• Mandatory items for RVSM are available in FCOM (Refer to FCOM/PRO-SPO-50 REQUIRED

EQUIPMENT/FUNCTIONS FOR RVSM)• Mandatory items for RNP are available in FCOM (Refer to FCOM/PRO-SPO-51 BRNAV IN

EUROPEAN AIRSPACE)

HANDLING OF MAINTENANCE MESSAGES ON ECAM STATUS PAGEIdent.: NO-020-00005448.0001001 / 26 MAR 08Criteria: SA�

1 Applicable to: MSN 0039, 0042, 0087-0088, 0103, 0109, 0120, 0132, 0163-0164, 0168-0169, 0174-0175, 0179, 0189, 0193, 0210, 0221-0222,0225, 0230-0232, 0247, 0257-0259, 0279-0280, 0283-0284, 0294, 0299, 0301-0302, 0305, 0308-0309, 0313-0314, 0338, 0343-0345, 0347,0349, 0354, 0357, 0373, 0376, 0386, 0391, 0405, 0407, 0411

Dispatch with maintenance message displayed on ECAM STATUS page is allowed without specificconditions except for:• BLUE RSVR: Refer to MEL 29-00-01• AIR BLEED: Refer to MEL 36-00-01.




Ident.: NO-020-00005448.0002001 / 26 MAR 08Criteria: 29-1055, K2113, K2962, K3154, SA�

2 Applicable to: MSN 0002-0038, 0040-0041, 0043-0086, 0089-0102, 0104-0108, 0110-0119, 0121-0131, 0133-0162, 0165-0167, 0170-0173,0176-0178, 0180-0188, 0190-0192, 0194-0209, 0211-0220, 0223-0224, 0226-0229, 0233-0246, 0248-0256, 0260-0278, 0281-0282, 0285-0293,0295-0298, 0300, 0303-0304, 0306-0307, 0310-0312, 0315-0337, 0339-0342, 0346, 0348, 0350-0353, 0355-0356, 0358-0372, 0375,0377-0385, 0387-0390, 0392-0404, 0406, 0408-0410, 0412-3996

Dispatch with maintenance message displayed on ECAM STATUS page is allowed without specificconditions except for:• AIR BLEED: Refer to MEL 36-00-01.

SECURED AND TRANSIT STOPIdent.: NO-020-00005449.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

If the last checklist performed by the flight crew is SECURING THE AIRCRAFT C/L, the aircraft is inSECURED STOP. After a SECURED STOP, the flight crew must perform all items in the StandardOperations Procedure (SOP), for the next flight.If the last checklist performed by the flight crew is PARKING C/L, the aircraft is in TRANSIT STOP.After a TRANSIT STOP, items indicated by (*), are the only steps to be completed for TRANSITPREPARATION. i.e. PRELIMINARY COCKPIT PREPARATION, EXTERIOR INSPECTION, andCOCKPIT PREPARATION.

SAFETY EXTERIOR INSPECTIONIdent.: NO-020-00005450.0001001 / 11 JUN 08Criteria: SA�Applicable to: ALL

Safety exterior inspection is performed to ensure that the aircraft and its surroundings are safe foroperations. Items that should be checked include:• Chocks in place• Doors status• Ground crew present• Aircraft environment




PRELIMINARY COCKPIT PREPARATIONIdent.: NO-020-00005451.0001001 / 25 JUN 08Criteria: SA�Applicable to: ALL

OBJECTIVES

The objectives of the preliminary cockpit preparation are:• To ensure that all safety checks are performed before applying electrical power:

‐ The RCL pb is pressed for at least 3 s to display the cautions and warnings from the previousflight.

‐ The technical logbook and MEL are checked at this stage.• To check the liquid levels i.e. oil, hydraulic and oxygen pressure using

‐ The HYD pb is pressed to check the hydraulic level‐ The ENG pb is pressed to check engine oil level (Refer to FCOM/PRO-NOR-SOP-04-C

BEFORE WALK-AROUND - ECAM)‐ The DOOR pb is pressed, to check the oxygen pressure level

• To check the position of surface control levers e.g. slats/flaps, parking brake.

During the Preliminary Cockpit Preparation, the flight crew must also review all OEBs applicable tothe aircraft. The flight crew must pay a particular attention to the red OEBs, and more particularly tothe red OEBs that must be applied before the ECAM procedure.

OXYGEN

The ECAM S/D DOOR page displays the oxygen pressure. When the oxygen pressure is below adefined threshold, an amber half box highlights the value. This advises the flight crew that the bottleshould be refilled. The flight crew should refer to the minimum flight crew oxygen pressure (Refer toFCOM/LIM-35 COCKPIT FIXED OXYGEN SYSTEM). The prolonged dispatch of the aircraft in suchcondition is not recommended.

EXTERIOR INSPECTIONIdent.: NO-020-00005452.0001001 / 11 JUN 08Criteria: SA�Applicable to: ALL

Standard Operating Procedures (SOP) outline the various elements that the flight crew must review ingreater detail. The objectives of the exterior inspection are:• To obtain a global assessment of the aircraft status. Any missing parts or panels will be checked

against the Configuration Deviation List (CDL) for possible dispatch and any potential operationalconsequences.

• To ensure that main aircraft surfaces are in adequate position relative to surface control levers.• To check that there are no leaks e.g. engine drain mast, hydraulic lines.




• To check the status of the essential visible sensors i.e. AOA, pitot and static probes.• To observe any possible abnormalities on the landing gear status:

‐ Wheels and tires status (cut, wear, cracks)‐ Safety pins are removed‐ Brakes status (Brake wear pin length with parking brake ON)‐ Length of oleo. Any difference between the two main landing gears shall be reported.

• To observe any possible abnormality on the engines:‐ Fan blades, turbine exhaust, engine cowl and pylon status‐ Access door closed

ADIRS INITIALIZATIONIdent.: NO-020-00005453.0001001 / 11 JUN 08Criteria: SA�

3 Applicable to: MSN 0002-0909, 0911-2210, 2212-2215, 2217-2276, 2278-2287, 2289-2295, 2297-2334, 2336-2340, 2342-2361, 2363-2382,2384-2395, 2397-2403, 2405-2409, 2411-2413, 2415-2430, 2432-2451, 2453-2466, 2469-2718, 2720-2735, 2737-2755, 2757, 2759-2775,2777-2788, 2790-2800, 2802-2806, 2808-2812, 2814-2832, 2834-2842, 2844, 2846-2857, 2859-2863, 2865-2869, 2871, 2873-2885, 2888,2890-2891, 2893, 2895-2896, 2898-2906, 2908-2923, 2925-2930, 2932-2954, 2956-2975, 2977-2995, 2998-3000, 3003-3010, 3012-3015,3017-3029, 3034, 3036-3042, 3044-3046, 3048-3053, 3055-3057, 3059, 3061, 3063-3065, 3067-3070, 3073, 3075-3077, 3079-3084,3086-3090, 3092-3093, 3095-3096, 3098-3101, 3103-3105, 3107-3108, 3110, 3112-3118, 3120-3126, 3129, 3131-3137, 3139-3141, 3144,3147-3148, 3152-3155, 3157-3159, 3162-3165, 3167-3168, 3170, 3173, 3175-3176, 3178, 3181-3189, 3191-3192, 3194-3202, 3204-3208,3210, 3213, 3215, 3218-3219, 3221, 3223, 3226-3227, 3230-3235, 3238-3239, 3242-3250, 3253-3254, 3257-3262, 3264-3265, 3267-3270,3272-3277, 3279, 3281-3283, 3285, 3289-3293, 3295-3299, 3301-3304, 3308, 3310-3311, 3314-3316, 3318, 3321-3324, 3327-3328, 3330,3332-3339, 3341-3343, 3345-3347, 3350-3351, 3353, 3355-3357, 3359-3363, 3366, 3368-3370, 3372-3374, 3378-3379, 3383, 3386-3387,3389, 3393-3399, 3401-3402, 3404-3405, 3407, 3410-3415, 3417-3422, 3424-3429, 3431-3432, 3434-3435, 3437, 3440-3442, 3444-3445,3447-3450, 3453-3458, 3460-3461, 3463-3466, 3468, 3470-3471, 3474-3477, 3480-3486, 3489, 3491, 3495-3497, 3499, 3501-3506,3510-3513, 3515-3516, 3519-3522, 3524-3525, 3528-3530, 3532, 3536-3539, 3541-3545, 3547-3550, 3553, 3555, 3558-3559, 3561, 3563,3567-3571, 3574, 3576-3584, 3586, 3590-3593, 3596, 3598-3601, 3603-3604, 3607-3614, 3617-3618, 3621, 3625-3629, 3631-3634, 3636-3641,3643-3644, 3648-3650, 3652, 3654, 3661, 3666, 3668-3669, 3673-3677, 3679-3680, 3682-3686, 3688-3689, 3692, 3694-3706, 3708,3711-3712, 3715-3721, 3723, 3726, 3728-3732, 3734-3735, 3737-3738, 3740, 3742-3743, 3746, 3748-3749, 3751, 3754, 3756, 3759, 3763,3765, 3768, 3774-3778, 3780, 3782-3783, 3786-3790, 3793-3797, 3799, 3802-3803, 3805, 3808-3810, 3812-3815, 3817, 3823-3826, 3835,3838, 3843-3846, 3851-3852, 3854-3859, 3862-3865, 3871, 3875, 3891, 3904-3906, 3943-3946, 3821, 3830-3833, 3840, 3848-3849, 3868,3873, 3879, 3881, 3884-3885, 3887-3889, 3893-3894, 3896-3899, 3909, 3911-3913, 3916-3917, 3921-3926, 3928-3933, 3935-3937, 3948-3949,3953-3954, 3956, 3960-3966, 3971, 3977, 3984-3996

ALIGNMENT

At the beginning of the pre-flight checks, the crew sets the ADIRS selectors to NAV, in order to startalignment.The alignment takes approximately 10 min, and must be completed before pushback (before anyaircraft movement).




IN TRANSIT:

ADIRS re-alignment is only necessary, if one of the ADIRS displays a residual ground speedgreater than 5 kt.In this case, a rapid re-alignment should be performed on all 3 IRSs (by setting all the ADIRSto OFF, then all back to ON within 5 s). The fast alignment takes approximately one minute.It involves setting the ground speed to 0, and updating the IRS position to the position of thecoordinates on the INITA page (usually airport reference coordinates).A complete re-alignment is only recommended for Long-range flights, especially if flown outsideradio NAVAID coverage with Aircraft not equipped with GPS.

INITIALIZATION

The F-PLN origin airport coordinates are extracted from the FMS database. These coordinatesappear on the MCDU INITA page, and are normally used for initialization. They are the airportreference coordinates.If a high navigation performance is desired, (i.e. for long-range flights without GPS and withoutradio navigation updates, or if low RNP operation is expected), the crew should adjust the airportreference coordinates to the gate coordinates, provided that this data is published or available onboard. In this case, the flight crew should use the slew keys successively for Latitude and Longitude,instead of inserting the coordinates on the scratchpad, (in order to avoid errors).When performing the BEFORE START C/L, the flight crew will check that the IRS IN ALIGN ECAMMEMO no longer appears, to indicate that the ADIRS are in NAV mode.The crew will check on the POSITION MONITOR page, that the distance between IRS and FMSposition is lower than 5 nm. This will permit to detect any gross error for IRS initialization, which isnot visible as long as GPS PRIMARY is available.Checking runway and SID display on the ND in comparison with the aircraft symbol representing theaircraft present position, (ARC or NAV mode, range 10 nm) during taxi, is a good way to check theglobal consistency of FMGS entries (Position and flight plan).

"RESET IRS TO NAV" MCDU MESSAGE

When the ADIRS are in NAV mode, and new origin airport coordinates are inserted, the RESET IRSTO NAV message triggers.This occurs in transit, when the flight crew enters a new CO-RTE, or enters a new FROM-TO airportpair on the INIT A page, and does not re-align the ADIRS.

In this case, check the coordinates on the INITA page and compare them with:• The coordinates of the origin airport, that are provided on the Airport chart, in order to detect a

possible error in airport entry• The ADIRS position (IRS monitor page).

In most cases the ADIRS position and the airport position do not differ significantly. Therefore, themessage may be cleared without realigning the IRSs.




Ident.: NO-020-00005453.0002001 / 11 JUN 08Criteria: 34-1346, P8194, SA�

4 Applicable to: MSN 0910, 2211, 2216, 2277, 2288, 2296, 2335, 2341, 2362, 2383, 2396, 2404, 2410, 2414, 2431, 2452, 2467-2468, 2719,2736, 2756, 2758, 2776, 2789, 2807, 2813, 2833, 2843, 2845, 2858, 2864, 2870, 2872, 2886-2887, 2889, 2892, 2894, 2897, 2907, 2924, 2931,2955, 2976, 2996-2997, 3001-3002, 3011, 3016, 3030-3033, 3035, 3043, 3047, 3054, 3058, 3060, 3062, 3066, 3071-3072, 3074, 3078, 3085,3091, 3094, 3097, 3102, 3106, 3109, 3111, 3119, 3127-3128, 3130, 3138, 3142-3143, 3145-3146, 3149-3151, 3156, 3160-3161, 3166, 3169,3171-3172, 3174, 3177, 3179-3180, 3190, 3193, 3203, 3209, 3211-3212, 3214, 3216-3217, 3220, 3222, 3224-3225, 3228-3229, 3236-3237,3240-3241, 3251-3252, 3255-3256, 3263, 3266, 3271, 3278, 3280, 3284, 3286-3288, 3294, 3300, 3305-3307, 3309, 3312-3313, 3317,3319-3320, 3325-3326, 3329, 3331, 3340, 3344, 3348-3349, 3352, 3354, 3358, 3364-3365, 3367, 3371, 3375-3377, 3380-3382, 3384-3385,3388, 3390-3392, 3400, 3403, 3406, 3408-3409, 3416, 3423, 3430, 3433, 3436, 3438-3439, 3443, 3446, 3451-3452, 3459, 3462, 3467,3469, 3472-3473, 3478-3479, 3487-3488, 3490, 3492-3494, 3498, 3500, 3507-3509, 3514, 3517-3518, 3523, 3526-3527, 3531, 3533-3535,3540, 3546, 3551-3552, 3554, 3556-3557, 3560, 3562, 3564-3566, 3572-3573, 3575, 3585, 3587-3589, 3594-3595, 3597, 3602, 3605-3606,3615-3616, 3619-3620, 3622-3624, 3630, 3635, 3642, 3645-3647, 3651, 3653, 3655-3660, 3662-3665, 3667, 3670-3672, 3678, 3681, 3687,3690-3691, 3693, 3707, 3709-3710, 3713-3714, 3722, 3724-3725, 3727, 3733, 3736, 3739, 3741, 3744-3745, 3747, 3750, 3752-3753, 3755,3757-3758, 3760-3762, 3764, 3766-3767, 3769-3773, 3779, 3781, 3784-3785, 3791-3792, 3798, 3800-3801, 3804, 3806-3807, 3811, 3816,3822, 3839, 3841, 3847, 3850, 3860-3861, 3874, 3890, 3892, 2801, 3818-3820, 3827-3829, 3834, 3836-3837, 3853, 3866-3867, 3869, 3872,3876-3878, 3880, 3882-3883, 3886, 3895, 3900-3903, 3907-3908, 3910, 3915, 3918-3920, 3927, 3934, 3938-3941, 3947, 3950-3952, 3955,3959, 3967-3970, 3972, 3981-3983

ALIGNMENT

At the beginning of the pre-flight checks, the crew sets the ADIRS selectors to NAV, in order to startalignment.The alignment takes approximately 10 min, and must be completed before pushback (before anyaircraft movement).

IN TRANSIT:

ADIRS re-alignment is only necessary, if one of the ADIRS displays a residual ground speedgreater than 5 kt.In this case, a rapid re-alignment should be performed on all 3 IRSs (by setting all the ADIRSto OFF, then all back to ON within 5 s). The fast alignment takes approximately one minute.It involves setting the ground speed to 0, and updating the IRS position to the position of thecoordinates on the INITA page (usually airport reference coordinates).

INITIALIZATION

The ADIRS are automatically initialized at the GPS position. These GPS coordinates are displayedon the MCDU INIT A page, in replacement of the airport reference coordinates, after the pilotentered the FROM-TO airport pair.When performing the BEFORE START C/L, the crew will check that the IRS IN ALIGN ECAMMEMO has disappeared, as a confirmation that the ADIRS are in NAV mode.




Checking runway and SID display on the ND in comparison with the aircraft symbol representing theaircraft present position, (ARC or NAV mode, range 10 nm) during taxi, is a good way to check theglobal consistency of FMGS entries (Position and flight plan).

"RESET IRS TO NAV" MCDU MESSAGE

When the ADIRS are in NAV mode, and new origin airport coordinates are inserted, the RESET IRSTO NAV message triggers.This occurs, in transit, when the crew performs a fast alignment, since this fast alignment is usuallycompleted before the crew enters the FROM-TO airport pair.Check the validity of the IRS initialization, before clearing this message.

COCKPIT PREPARATIONIdent.: NO-020-00005454.0001001 / 27 JUN 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�

5 Applicable to: MSN 0029, 0035-0039, 0042-0043, 0045-0051, 0056-0059, 0068-0075, 0078-0080, 0083-0090, 0093-0097, 0103-0104,0109-0111, 0113-0114, 0116-0117, 0120, 0122, 0126-0127, 0132, 0135, 0137-0142, 0147-0151, 0154, 0157, 0159, 0161-0164, 0167-0170, 0172,0174-0175, 0179-0183, 0185, 0189-0191, 0193, 0195, 0200-0202, 0209-0210, 0212, 0216-0218, 0221-0222, 0225, 0229-0234, 0242-0243,0245-0261, 0265-0269, 0275-0277, 0279-0280, 0283-0284, 0288-0296, 0301-0305, 0308-0311, 0313-0316, 0320-0321, 0324-0327, 0330-0336,0338, 0341-0350, 0353-0354, 0356-0357, 0359, 0361-0364, 0368-0369, 0371, 0373-0376, 0378-0379, 0382, 0384-0386, 0389, 0391-0398,0401, 0403-0407, 0409, 0411-0416, 0419-0447, 0449-0454, 0456-0470, 0472-0490, 0492-0497, 0499-0500, 0502-0506, 0508, 0510, 0512-0520,0522-0526, 0528, 0530, 0532-0543, 0545-0583, 0585-0597, 0599, 0601-0607, 0609-0617, 0619-0624, 0626-0636, 0638-0643, 0645-0646,0648-0657, 0659, 0661-0668, 0670-0679, 0681-0684, 0686, 0688-0714, 0716-0724, 0726-0763, 0765, 0767-0776, 0779-0785, 0787-0795,0797-0800, 0803-0806, 0808-0817, 0819-0829, 0831, 0833-0843, 0845, 0847-0860, 0862, 0864-0867, 0870-0879, 0881-0884, 0886-0889,0891-0895, 0897-0902, 0905-0906, 0908-0909, 0912, 0914-0921, 0924-0928, 0930-0937, 0939-0940, 0942-0957, 0959-0960, 0963, 0965-0971,0973-0974, 0977-0980, 0982-0984, 0986-0987, 0989-0991, 0993, 0995, 0999, 1001, 1003-1009, 1012-1018, 1022-1024, 1026, 1028-1032,1034-1035, 1039, 1041, 1043, 1045, 1049-1050, 1054, 1056-1057, 1060, 1063-1064, 1068, 1070, 1072, 1074-1076, 1079, 1081, 1083,1085-1086, 1088, 1093-1094, 1098, 1100, 1104-1106, 1108, 1110-1111, 1116-1117, 1120, 1124, 1127-1128, 1138, 1144-1146, 1153-1154, 1163,1165-1166, 1168, 1171, 1174, 1177-1178, 1180-1181, 1192, 1196, 1199, 1202, 1206-1207, 1209-1211, 1217-1218, 1220, 1223, 1226, 1228, 1231,1234, 1237, 1243, 1247-1248, 1252, 1263, 1266, 1272, 1274, 1281-1282, 1284, 1286, 1290-1291, 1293, 1296, 1307, 1312, 1316, 1321, 1323,1330, 1341, 1343, 1345, 1347, 1350, 1357, 1359, 1361-1363, 1370, 1372-1375, 1379, 1395, 1397, 1399, 1401, 1409, 1418, 1420-1422, 1424,1426-1427, 1432, 1435, 1439, 1448, 1450, 1457, 1459-1460, 1469, 1473-1475, 1477, 1480, 1487, 1489, 1495, 1507-1508, 1514, 1522, 1532-1533,1538, 1542, 1545, 1555, 1559, 1561, 1569, 1573, 1581, 1584-1586, 1600, 1609, 1617, 1620, 1627, 1635, 1639, 1647, 1649, 1653-1655, 1664,1667, 1669, 1671, 1674, 1679-1681, 1688, 1692, 1694, 1697-1698, 1702, 1713, 1716, 1728-1729, 1731-1732, 1736-1737, 1741, 1753, 1755, 1768,1793, 1799, 1809, 1816, 1821, 1834, 1836, 1840, 1842, 1845, 1847, 1865, 1892, 1902, 1987, 2058, 2104, 2115, 2143, 2252

FLOW PATTERN

The scan pattern varies, depending on the pilot status, i.e PF, PNF, CM1, or CM2, and the areas ofresponsibility:1. Overhead panel: Extinguish any white lights2. Center instrument panel3. pedestal4. FMGS preparation, and when both pilots are seated:5. Glareshield6. Lateral consoles and CM1/CM2 panels




Cockpit preparation flow pattern

FMGS PROGRAMMING

FMGS programming involves inserting navigation data, then performance data. It is to be noted that:• Boxed fields must be filled• Blue fields inform the crew that entry is permitted• Green fields are used for FMS generated data, and cannot be changed• Magenta characters identify limits (altitude, speed or time), that FMS will attempt to meet• Yellow characters indicate a temporary flight plan display• Amber characters signify that the item being displayed is important and requires immediate action• Small font signifies that data is FMS computed• Large font signifies manually entered data.




This sequence of entry is the most practical. INIT B should not be filled immediately after INIT A,because the FMGS would begin to compute F-PLN predictions. These computations would slowdown the entry procedure.

To obtain correct predictions, the fields of the various pages must be completed correctly, withavailable planned data for the flight:• DATA

The database validity, NAVAIDs and waypoints (possibly stored in previous flight), and PERFFACTOR must be checked on the STATUS page.

• INIT AThe INIT A page provides access to aircraft present position. The flight crew will check that itcorresponds to the real aircraft position. (Refer to NO-020 ADIRS INITIALIZATION).The history wind is the vertical wind profile that has been encountered during the previousdescent and should be entered at this stage if it is representative of the vertical wind profile for thenext flight.

• F-PLN

The F-PLN A page is to be completed thoroughly including:‐ The take-off runway‐ SID‐ Altitude and speed constraints‐ Correct transition to the cruise waypoint‐ Intended step climb/descents, according to the Computerized Flight Plan (CFP).

If time permits, the wind profile along the flight plan may be inserted using vertical revisionthrough wind prompt.




The flight crew should also check the overall route distance (6th line of the F-PLN page), versusCFP distance.

• SEC F-PLNThe SEC F-PLN should be used to consider an alternate runway for take-off, a return to departureairfield or a routing to a take-off alternate.

• RAD NAVThe RAD NAV page is checked, and any required NAVAID should be manually entered usingident. If a NAVAID is reported on NOTAM as unreliable, it must be deselected on the MCDUDATA/POSITION MONITOR/SEL NAVAID page.

• INIT B

The flight crew:‐ Inserts the expected ZFWCG/ZFW, and block fuel to initialize a F-PLN computation.‐ Checks fuel figures consistent with flight preparation fuel figures.

The flight crew will update weight and CG on receipt of the load sheet.After Engine start, the INIT B page is no longer available. The flight crew should use the FUELPRED page for weight and fuel data insertion, if required.

• PERFThe thrust reduction altitude/acceleration altitude (THR RED /ACC) are set to default at 1 500 ft,or at a value defined by airline policy. The THR RED/ACC may be changed in the PERF TAKE-OFF page, if required. The flight crew should consider the applicable noise abatement procedure.

The one-engine-out acceleration altitude must:‐ Be at least 400 ft above airport altitude‐ Ensure that the net flight path is 35 ft above obstacles‐ Ensure that the maximum time for takeoff thrust is not exceeded.

Therefore, there are generally a minimum and a maximum one engine out acceleration altitudevalues. The minimum value satisfies the first two criteria. The maximum value satisfies the lastone. Any value between those two may be retained.The one engine out acceleration altitude is usually defaulted to 1 500 ft AGL and will be updatedas required.The flight crew uses the PERF CLB page to pre-select a speed. For example, "Green Dot" speedfor a sharp turn after take-off.

The crew may also check on the PROG page the CRZ FL, MAX REC FL and OPT FL.Once the FMGS has been programmed, the PNF should then cross check the information prior tothe take-off briefing.When the predictions are available, the crew may print the PREFLIGHT DATA . This listingprovides all the predictions which may be used during the initial part of the flight.




TAKE-OFF BRIEFING

The PF should perform the takeoff briefing at the gate , when the flight crew workload permits,Cockpit preparation has been completed and, before engine start.The takeoff briefing should be relevant, concise and chronological. When a main parameter isreferred to by the PF, both flight crewmembers must crosscheck that the parameter has been set orprogrammed correctly. The takeoff briefing covers the following:

Take off briefing with associated checks

1- MiscellaneousAircraft type and model (Tail strike awareness)Aircraft technical status (MEL and CDL considerations, relevant OEB)NOTAMSWeatherRWY conditionsUse of ENG/Wing Anti IceENG Start ProcedurePush BackExpected Taxi ClearanceUse of RadarUse of Packs for Takeoff




2- INIT B PageBlock Fuel (1) (FOB on EW/D)Estimated TOWExtra time at destination

3- Takeoff Perf PageTO RWYTO CONFFLEX / TOGA (1) (FLEX TOGA on E/WD)V1, VR, V2 (1) (V1, V2 on PFD)TRANS ALTTHR RED / ACC Altitude

4- Flight PlanMinimum Safe AltitudeFirst assigned FL (1) (altitude target in blue on PFD)Flight Plan description (1) (SID on MCDU FPLN page)RAD NAV (1) (RAD NAV on ND)

5- Abnormal Operations

For any failure before V1:CAPT will call "STOP" or "GO"

In case of failure after V1:continue TO, no actions before 400 ft AGL except gear upreaching 400 ft AGL, ECAM actionsreaching EO ACC altitude, stop ECAM, push for ALT, acceleration and clean upat green dot: OP CLB, MCT, continue ECAM, after TO C/L, statusENG OUT routing: EOSID, SID, radar vector, immediate return ...

(1) Items that must be cross-checked on the associated display.

FMS UPDATING

When the load and trim sheet is available, the crew will:• Updates the ZFWCG/ZFW• Checks TOW consistent with load sheet• Checks updated fuel figures• Modify the FLEX TEMP and the take-off speeds as required• Enter the THS position in PERF TAKE OFF page

When the predictions are available, the crew will print the pre-flight data.




Ident.: NO-020-00005454.0002001 / 27 JUN 08Criteria: 22-1089, 22-1090, 22-1103, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1163, 22-1176, 22-1180, 22-1193, 22-1197,22-1209, 22-1217, 22-1218, 22-1219, 22-1233, 22-1235, 22-1240, P7372, P7373, P7519, P7520, P7666, P7706, P7707, SA�

6 Applicable to: MSN 0002-0021, 0031-0034, 0040-0041, 0044, 0052-0055, 0061-0067, 0076-0077, 0081-0082, 0091, 0098-0102, 0108, 0112,0115, 0118-0119, 0121, 0123-0125, 0128-0131, 0133-0134, 0136, 0143-0146, 0152-0153, 0155-0156, 0158, 0160, 0165-0166, 0171, 0173,0176-0178, 0184, 0186-0188, 0192, 0194, 0196-0199, 0203-0208, 0211, 0213-0215, 0219-0220, 0223-0224, 0226-0228, 0235-0241, 0244,0262-0264, 0270-0274, 0278, 0281-0282, 0285-0287, 0297-0300, 0306-0307, 0312, 0317-0319, 0322-0323, 0328-0329, 0337, 0339-0340,0351-0352, 0355, 0358, 0360, 0365-0367, 0370, 0372, 0377, 0380-0381, 0383, 0387-0388, 0390, 0399-0400, 0402, 0408, 0410, 0417-0418,0448, 0455, 0471, 0491, 0498, 0501, 0507, 0509, 0511, 0521, 0527, 0529, 0531, 0544, 0584, 0598, 0600, 0608, 0618, 0625, 0637, 0644, 0647,0658, 0660, 0669, 0680, 0685, 0687, 0715, 0725, 0764, 0766, 0777-0778, 0786, 0796, 0801-0802, 0807, 0818, 0830, 0832, 0844, 0846, 0861,0863, 0868-0869, 0880, 0885, 0890, 0896, 0903-0904, 0907, 0910-0911, 0913, 0922-0923, 0929, 0938, 0941, 0958, 0961-0962, 0964, 0972,0975-0976, 0981, 0985, 0988, 0992, 0994, 0996-0998, 1000, 1002, 1010-1011, 1019-1021, 1025, 1027, 1033, 1036-1038, 1040, 1042, 1044,1046-1048, 1051-1053, 1055, 1058-1059, 1061-1062, 1065-1067, 1069, 1071, 1073, 1077-1078, 1080, 1082, 1084, 1087, 1089-1092, 1095-1097,1099, 1101-1103, 1107, 1109, 1112-1115, 1118-1119, 1121-1123, 1125-1126, 1129-1137, 1139-1143, 1147-1152, 1155-1162, 1164, 1167, 1169-1170,1172-1173, 1175-1176, 1179, 1182-1191, 1193-1195, 1197-1198, 1200-1201, 1203-1205, 1208, 1212-1216, 1219, 1221-1222, 1224-1225, 1227,1229-1230, 1232-1233, 1235-1236, 1238-1242, 1244-1246, 1249-1251, 1253-1262, 1264-1265, 1267-1271, 1273, 1275-1280, 1283, 1285,1287-1289, 1292, 1294-1295, 1297-1306, 1308-1311, 1313-1315, 1317-1320, 1322, 1324-1329, 1331-1340, 1342, 1344, 1346, 1348-1349,1351-1356, 1358, 1360, 1364-1369, 1371, 1376-1378, 1380-1394, 1396, 1398, 1400, 1402-1408, 1410-1417, 1419, 1423, 1425, 1428-1431,1433-1434, 1436-1438, 1440-1447, 1449, 1451-1456, 1458, 1461-1468, 1470-1472, 1476, 1478-1479, 1481-1486, 1488, 1490-1494, 1496-1506,1509-1513, 1515-1521, 1523-1531, 1534-1537, 1539-1541, 1543-1544, 1546-1554, 1556-1558, 1560, 1562-1568, 1570-1572, 1574-1580,1582-1583, 1587-1599, 1601-1608, 1610-1616, 1618-1619, 1621-1626, 1628-1634, 1636-1638, 1640-1646, 1648, 1650-1652, 1656-1663,1665-1666, 1668, 1670, 1672-1673, 1675-1678, 1682-1687, 1689-1691, 1693, 1695-1696, 1699-1701, 1703-1712, 1714-1715, 1717-1727, 1730,1733-1735, 1738-1740, 1742-1752, 1754, 1756-1767, 1769-1792, 1794-1798, 1800-1808, 1810-1815, 1817-1820, 1823-1833, 1835, 1837-1839,1841, 1843-1844, 1846, 1848-1864, 1866-1891, 1893-1901, 1903-1986, 1988-2057, 2059-2103, 2105-2114, 2116-2142, 2144-2251, 2253-3996

FLOW PATTERN

The scan pattern varies, depending on the pilot status, i.e PF, PNF, CM1, or CM2, and the areas ofresponsibility:1. Overhead panel: Extinguish any white lights2. Center instrument panel3. pedestal4. FMGS preparation, and when both pilots are seated:5. Glareshield6. Lateral consoles and CM1/CM2 panels




Cockpit preparation flow pattern

FMGS PROGRAMMING

FMGS programming involves inserting navigation data, then performance data. It is to be noted that:• Boxed fields must be filled• Blue fields inform the crew that entry is permitted• Green fields are used for FMS generated data, and cannot be changed• Magenta characters identify limits (altitude, speed or time), that FMS will attempt to meet• Yellow characters indicate a temporary flight plan display• Amber characters signify that the item being displayed is important and requires immediate action• Small font signifies that data is FMS computed• Large font signifies manually entered data.




This sequence of entry is the most practical. INIT B should not be filled immediately after INIT A,because the FMGS would begin to compute F-PLN predictions. These computations would slowdown the entry procedure.

To obtain correct predictions, the fields of the various pages must be completed correctly, withavailable planned data for the flight:• DATA

The database validity, NAVAIDs and waypoints (possibly stored in previous flight), and PERFFACTOR must be checked on the STATUS page.

• INIT AThe INIT A page provides access to aircraft present position. The flight crew will check that itcorresponds to the real aircraft position. (Refer to NO-020 ADIRS INITIALIZATION).The history wind is the vertical wind profile, that has been encountered during the previousdescent and should be entered at this stage if it is representative of the vertical wind profile for thenext flight.

• F-PLN

The F-PLN A page is to be completed thoroughly including:‐ The take-off runway‐ SID‐ Altitude and speed constraints‐ Correct transition to the cruise waypoint‐ Intended step climb/descents, according to the Computerized Flight Plan (CFP).

If time permits, the wind profile along the flight plan may be inserted using vertical revisionthrough wind prompt.




The flight crew should also check the overall route distance (6th line of the F-PLN page), versusCFP distance.

• SEC F-PLNThe SEC F-PLN should be used to consider an alternate runway for take-off, a return to departureairfield or a routing to a take-off alternate.

• RAD NAVThe RAD NAV page is checked, and any required NAVAID should be manually entered usingident. If a NAVAID is reported on NOTAM as unreliable, it must be deselected on the MCDUDATA/POSITION MONITOR/SEL NAVAID page.

• INIT B

The flight crew:‐ Inserts the expected ZFWCG/ZFW, and block fuel to initialize a F-PLN computation.‐ Checks fuel figures consistent with flight preparation fuel figures.

The flight crew will update weight and CG on receipt of the load sheet.The FMS uses the trip wind for the entire flight from origin to destination. The trip wind is anaverage wind component that may be extracted from the CFP. The trip wind facility is available ifthe wind profile has not already been entered.After Engine start, the INIT B page is no longer available. The flight crew should use the FUELPRED page for weight and fuel data insertion, if required.The INIT B page should not be completed immediately after INIT A, because the FMGS wouldbegin to compute F-PLN predictions. This would slow down the entry procedure.

• PERFThe thrust reduction altitude/acceleration altitude (THR RED /ACC) are set to default at 1 500 ft,or at a value defined by airline policy. The THR RED/ACC may be changed in the PERF TAKE-OFF page, if required. The flight crew should consider the applicable noise abatement procedure.

The one-engine-out acceleration altitude must:‐ Be at least 400 ft above airport altitude‐ Ensure that the net flight path is 35 ft above obstacles‐ Ensure that the maximum time for takeoff thrust is not exceeded.

Therefore, there are generally a minimum and a maximum one engine out acceleration altitudevalues. The minimum value satisfies the first two criteria. The maximum value satisfies the lastone. Any value between those two may be retained.The one engine out acceleration altitude is usually defaulted to 1 500 ft AGL and will be updatedas required.The flight crew uses the PERF CLB page to pre-select a speed. For example, "Green Dot" speedfor a sharp turn after take-off.

The crew may also check on the PROG page the CRZ FL, MAX REC FL and OPT FL.




Once the FMGS has been programmed, the PNF should then cross check the information prior tothe take-off briefing.When the predictions are available, the crew may print the PREFLIGHT DATA . This listingprovides all the predictions which may be used during the initial part of the flight.

TAKE-OFF BRIEFING

The PF should perform the takeoff briefing at the gate , when the flight crew workload permits,Cockpit preparation has been completed and, before engine start.The takeoff briefing should be relevant, concise and chronological. When a main parameter isreferred to by the PF, both flight crewmembers must crosscheck that the parameter has been set orprogrammed correctly. The takeoff briefing covers the following:

Take off briefing with associated checks

1- MiscellaneousAircraft type and model (Tail strike awareness)Aircraft technical status (MEL and CDL considerations, relevant OEB)NOTAMSWeatherRWY conditionsUse of ENG/Wing Anti Ice

To be continued on next page




Continued from previous page1- Miscellaneous

ENG Start ProcedurePush BackExpected Taxi ClearanceUse of RadarUse of Packs for Takeoff

2- INIT B PageBlock Fuel (1) (FOB on EW/D)Estimated TOWExtra time at destination

3- Takeoff Perf PageTO RWYTO CONFFLEX / TOGA (1) (FLEX TOGA on E/WD)V1, VR, V2 (1) (V1, V2 on PFD)TRANS ALTTHR RED / ACC Altitude

4- Flight PlanMinimum Safe AltitudeFirst assigned FL (1) (altitude target in blue on PFD)Flight Plan description (1) (SID on MCDU FPLN page)RAD NAV (1) (RAD NAV on ND)

5- Abnormal Operations

For any failure before V1:CAPT will call "STOP" or "GO"

In case of failure after V1:continue TO, no actions before 400 ft AGL except gear upreaching 400 ft AGL, ECAM actionsreaching EO ACC altitude, stop ECAM, push for ALT, acceleration and clean upat green dot: OP CLB, MCT, continue ECAM, after TO C/L, statusENG OUT routing: EOSID, SID, radar vector, immediate return ...

(1) Items that must be cross-checked on the associated display.

FMS UPDATING

When the load and trim sheet is available, the flight crew:• Updates the ZFWCG/ZFW• Checks that the TOW is consistent with the load sheet• Checks the updated fuel figures• Changes the FLEX TEMP and the take-off speeds as required• Enters the THS position on the PERF TAKE OFF page

When the predictions are available, the flight crew prints out the pre-flight data.




MISCELLANEOUSIdent.: NO-020-00005455.0001001 / 25 JUN 08Criteria: SA�Applicable to: ALL

SEATING POSITION

To achieve a correct seating position, the aircraft is fitted with an eye-position indicator on the centrewindscreen post. The eye-position indicator has two balls on it. When the balls are superimposed oneach other, they indicate that the pilot's eyes are in the correct position.The flight crew should not sit too low, to avoid increasing the cockpit cut-off angle, therefore reducingthe visual segment. During Low Visibility Procedures (LVP), it is important that the pilot's eyesare positioned correctly, in order to maximize the visual segment, and consequently, increase thepossibility of achieving the appropriate visual reference for landing as early as possible.After adjusting the seat, each pilot should adjust the outboard armrest, so that the forearm restscomfortably on it, when holding the sidestick. There should be no gaps between the pilot's forearmand the armrest. The pilot's wrist should not be bent when holding the sidestick. This ensures thatthe pilot can accomplish flight maneuvers by moving the wrist instead of lifting the forearm from thearmrest.Symptoms of incorrect armrest adjustment include over-controlling, and not being able to makesmall, precise inputs.The rudder pedals must then be adjusted to ensure the pilot can achieve both full rudder pedaldisplacement and full braking simultaneously on the same side.The armrest and the rudder pedals have position indicators. These positions should be noted andset accordingly for each flight.

MCDU USE

When clear for start up and taxi, the PF will preferably display the MCDU PERF TAKE OFF pagewhereas the PNF will display the MCDU F-PLN page.


NORMAL OPERATIONSSTART

ENV A318/A319/A320/A321 FLEET NO-030. P 1/12FCTM 09 JAN 09




ENGINE AUTO STARTIdent.: NO-030-00005456.0001001 / 19 DEC 08Criteria: SA�

1 Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0113-0114, 0163-0166,0168-0169, 0178-0180, 0193-0194, 0198, 0225, 0230, 0243, 0247, 0249-0252, 0256-0257, 0259-0261, 0275-0276, 0280, 0291-0292,0295-0296, 0304, 0308, 0314-0317, 0320-0322, 0326-0327, 0332, 0334-0336, 0338, 0344, 0347, 0351, 0353-0354, 0357, 0361-0364,0366, 0368-0369, 0373, 0376, 0385-0386, 0393-0394, 0396-0398, 0405-0406, 0411-0412, 0414-0416, 0423-0425, 0428-0432, 0435, 0437,0439-0444, 0447-0458, 0460-0465, 0467-0476, 0478-0480, 0483-0487, 0489-0490, 0492-0493, 0496, 0499-0500, 0502-0506, 0508, 0510,0512, 0518, 0523, 0527, 0530, 0538-0540, 0542-0543, 0550-0551, 0555-0558, 0560-0561, 0563-0565, 0567-0568, 0571, 0573, 0575, 0580,0582, 0584, 0587, 0589, 0591-0592, 0595, 0597, 0604, 0606, 0613-0614, 0620, 0631-0633, 0638, 0640, 0652, 0655, 0659, 0661, 0663,0667-0668, 0676, 0678, 0680, 0683, 0686-0687, 0690, 0692, 0696, 0698-0699, 0702, 0704-0705, 0709-0710, 0712, 0715, 0718, 0720,0722, 0725, 0731, 0733, 0739, 0741, 0743, 0746-0748, 0751, 0756, 0758-0760, 0762, 0770-0771, 0780, 0783-0784, 0787-0788, 0791-0792,0798, 0802-0806, 0810-0812, 0816, 0820, 0822, 0824-0826, 0834-0836, 0839, 0842-0843, 0847, 0849-0851, 0855-0859, 0862, 0864-0867,0871-0874, 0877-0878, 0881-0882, 0886-0887, 0889, 0892-0893, 0895, 0898-0902, 0908, 0910, 0912-0913, 0915-0916, 0918-0919, 0924,0927-0928, 0930-0932, 0934, 0943-0944, 0948, 0950, 0952-0955, 0963, 0965-0966, 0968-0969, 0974, 0976-0977, 0980, 0983, 0989-0990,0993, 1001, 1003-1004, 1007-1008, 1010, 1013-1015, 1022, 1024, 1031-1032, 1035, 1039, 1042-1043, 1045, 1049-1050, 1053, 1056-1057,1060, 1064, 1066, 1074-1076, 1079-1080, 1082-1083, 1085, 1088, 1092, 1096, 1098, 1103-1105, 1110-1111, 1113, 1115-1118, 1123, 1128,1139-1140, 1142-1143, 1146, 1153, 1156, 1158-1159, 1161, 1163, 1166, 1173-1174, 1177-1178, 1183, 1188, 1192-1197, 1199, 1202, 1204, 1207,1211-1212, 1214-1215, 1218, 1222-1223, 1225, 1227-1228, 1232, 1234-1236, 1239-1240, 1243, 1246, 1248, 1251, 1253, 1256-1258, 1260-1261,1266, 1270, 1272-1274, 1276, 1279-1282, 1284, 1290-1291, 1293, 1295, 1300, 1302, 1304, 1321, 1323, 1327, 1329, 1332-1335, 1338-1339,1341, 1343, 1349-1351, 1353, 1355-1356, 1359, 1363, 1366, 1368, 1373-1376, 1380, 1383-1384, 1395, 1397-1398, 1400-1401, 1406-1411,1418-1424, 1426-1428, 1432-1433, 1435, 1438, 1440, 1445-1446, 1452, 1459-1460, 1463-1464, 1466, 1468-1469, 1474-1475, 1477, 1482,1486-1487, 1490-1491, 1495, 1497, 1500, 1506-1514, 1518, 1522-1523, 1526-1529, 1533-1534, 1537-1538, 1545-1548, 1552, 1555, 1557-1559,1561, 1563, 1565-1566, 1568-1569, 1573-1576, 1580-1581, 1584-1587, 1589-1591, 1593-1596, 1600, 1604, 1606, 1608-1610, 1613-1614,1617, 1619-1621, 1624, 1626-1628, 1631, 1635-1636, 1642-1644, 1647-1650, 1652-1653, 1656, 1661, 1663-1665, 1669-1672, 1675-1676,1680, 1682, 1687-1690, 1695-1698, 1702-1703, 1705, 1707-1708, 1710-1711, 1715, 1721, 1723, 1727-1732, 1734, 1737, 1739, 1741, 1749,1754-1755, 1758, 1760, 1763-1764, 1768, 1771, 1773, 1776, 1782, 1784-1785, 1788, 1790, 1792, 1794, 1798, 1801-1802, 1804, 1807, 1814,1817-1818, 1821-1823, 1825-1827, 1829-1832, 1834-1835, 1837, 1840, 1842-1845, 1847-1850, 1854-1858, 1861-1862, 1865, 1868-1869, 1871,1877-1878, 1880, 1883, 1888, 1891-1893, 1895-1896, 1898-1899, 1902-1904, 1907, 1909-1910, 1912, 1914-1915, 1917-1918, 1922, 1926-1928,1933-1935, 1941, 1944-1948, 1950, 1952-1953, 1955-1958, 1962, 1967, 1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996, 1998,2000, 2004, 2006-2008, 2014-2016, 2020-2021, 2023, 2027, 2029, 2031-2032, 2038, 2040-2042, 2044-2045, 2055, 2058, 2063, 2067, 2070,2073, 2075, 2077, 2079-2080, 2084-2085, 2088-2090, 2094, 2096-2099, 2102, 2105, 2107-2108, 2110-2112, 2118, 2121, 2125, 2128, 2130,2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157, 2159-2161, 2164, 2167-2169, 2172-2173, 2177, 2185, 2188, 2190, 2192-2195,2197, 2200-2205, 2210-2211, 2215-2216, 2223, 2226, 2229, 2231-2232, 2234, 2238, 2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263,2267-2268, 2273, 2275, 2277, 2280-2282, 2284, 2286, 2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310, 2312-2314,2316, 2320-2324, 2326, 2329, 2331, 2334-2336, 2338-2341, 2343, 2345, 2348, 2351-2352, 2355-2356, 2359, 2362-2363, 2366, 2368,2371-2372, 2375-2376, 2379, 2383-2384, 2386, 2389, 2393, 2395-2397, 2401, 2403-2405, 2408, 2410, 2413-2415, 2417-2418, 2421-2424,2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445, 2447, 2449, 2452-2455, 2457-2459, 2461-2462, 2466-2470, 2473, 2475-2476,2479-2480, 2482, 2485, 2489-2491, 2496, 2501-2502, 2504-2505, 2509-2510, 2513, 2515, 2517, 2520-2522, 2524, 2526, 2530-2531,2533-2537, 2553, 2559-2560, 2564, 2566-2568, 2570-2574, 2576-2577, 2579-2580, 2585, 2587, 2589-2590, 2594-2595, 2597-2598, 2600,2602-2604, 2608-2610, 2613-2615, 2621-2622, 2626, 2630-2631, 2634, 2639-2640, 2642-2643, 2645, 2647-2651, 2653, 2655, 2657,2659-2661, 2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682, 2687-2690, 2692, 2694, 2697-2698, 2701, 2703-2704,2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728, 2730-2732, 2734, 2737-2739, 2741, 2747, 2752-2753, 2755, 2759, 2766-2767,2771-2772, 2775, 2780-2781, 2783-2784, 2787, 2791, 2793, 2797, 2799, 2802, 2804, 2808-2809, 2813-2815, 2817, 2823, 2828, 2832-2833,2838, 2840, 2844-2845, 2848, 2850, 2856, 2858-2859, 2862-2864, 2868, 2871-2872, 2874, 2880, 2883, 2886-2888, 2892-2894, 2896, 2898,2900-2901, 2904, 2906, 2908, 2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934, 2936, 2940-2943, 2945, 2948, 2952-2953, 2958,2963, 2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992, 2997, 2999, 3001, 3004-3005, 3007, 3010-3013, 3015, 3017, 3020, 3022,3026, 3029-3030, 3032-3034, 3039, 3042, 3045, 3049-3050, 3057, 3062, 3066-3067, 3069, 3071-3072, 3074-3075, 3077, 3081, 3086, 3089,3091, 3103-3106, 3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159, 3162, 3165-3167, 3172, 3175, 3177, 3183,3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3214, 3216-3217, 3219, 3222, 3227-3229, 3231, 3235, 3239, 3241, 3244,3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270, 3274-3276, 3279-3280, 3283, 3287, 3290, 3292, 3294, 3296-3297, 3301-3303, 3308,3311, 3314-3317, 3319, 3322, 3330, 3332, 3335, 3339, 3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365, 3369, 3371, 3375,3378-3379, 3381-3382, 3384, 3386-3387, 3390, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424, 3428-3430,3434, 3437-3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468-3469, 3474, 3478-3479, 3481, 3483-3484, 3488, 3491, 3493,3495-3497, 3499-3500, 3507, 3509-3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531, 3534-3535, 3538-3539, 3541, 3543, 3546-3548,3550, 3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572, 3575, 3577-3578, 3580-3581, 3583, 3585, 3587-3588, 3590-3592,3595, 3600, 3602-3603, 3606-3607, 3613-3614, 3618, 3621-3622, 3624-3625, 3635-3638, 3641-3642, 3645, 3649-3650, 3654, 3659, 3663,3668-3669, 3671-3674, 3676-3677, 3680-3681, 3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721,3724, 3726, 3730, 3734, 3736-3738, 3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773, 3779, 3782-3785, 3793,3796-3797, 3800-3801, 3803-3804, 3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839, 3841, 3847, 3849-3851, 3858, 3860, 3862-3864,3867, 3890, 3904, 3920, 3775, 3836-3837, 3869, 3873, 3876-3878, 3881, 3893, 3897, 3899, 3901-3902, 3910-3912, 3916-3917, 3924,3926-3927, 3934-3938, 3941-3944, 3947-3948, 3951, 3959-3966, 3968-3969, 3977-3981, 3989-3996

2




Engines usually start using the Automatic Starting function. The Full Authority Digital Engine Control(FADEC) systems control this engine Automatic Starting function, and takes appropriate action, ifengine parameters are exceeded. This function extends significantly the duration of engine life.The thrust levers must be confirmed at "idle" before engine-start. If the thrust levers are not at "idle",the thrust increases above idle after engine-start, and can result in a hazardous situation.However, an ENG START FAULT ECAM warning triggers, to indicate that the flight crew must set thethrust levers to "idle".The engines are started in sequence, preferably engine 2 first, in order to pressurize yellow hydraulicsystem, which supplies the parking brake accumulator.

When the ENG START selector is set to "START", the FADECs are electrically-supplied. When thereis sufficient BLEED PRESS, the PF begins the start sequence by setting the ENG MASTER switch toON. The flight crew should monitor the start sequence:‐ Start valve opens‐ N2 increases‐ IGN A(B)‐ Fuel flow‐ EGT‐ N1‐ Oil pressure increases‐ IGN indication off (Refer to FCOM/PRO-NOR-SOP-08 AUTOMATIC ENGINE START)‐ Start valve closes

When the engine is at idle, or when AVAIL is displayed, the PF can start engine 1.The flight crew should check the relative engine vibration level.When the ENG START selector is set to NORM, the packs return to the OPEN position. APU Bleedshould immediately be turned off, to avoid engine ingestion of exhaust gas.If the start is not successful, the flight crew must use the ECAM as usually done, and avoid instinctivelyselecting the ENG MASTER switch to OFF. This would interrupt the FADEC protective actions (e. g.cranking after hot start).




Ident.: NO-030-00005456.0002001 / 19 DEC 08Criteria: CFMI, SA�

3 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112, 0115-0162, 0167,0170-0177, 0181-0192, 0195-0197, 0199-0224, 0226-0229, 0231-0242, 0244-0246, 0248, 0253-0255, 0258, 0262-0274, 0277-0279, 0281-0290,0293-0294, 0297-0303, 0305-0307, 0309-0313, 0318-0319, 0323-0325, 0328-0331, 0333, 0337, 0339-0343, 0345-0346, 0348-0350, 0352,0355-0356, 0358-0360, 0365, 0367, 0370-0372, 0375, 0377-0384, 0387-0392, 0395, 0399-0404, 0407-0410, 0413, 0417-0422, 0426-0427,0434, 0436, 0438, 0445-0446, 0459, 0466, 0477, 0482, 0488, 0491, 0494-0495, 0497-0498, 0501, 0507, 0509, 0511, 0513-0517, 0519-0522,0524-0526, 0528-0529, 0531-0537, 0541, 0544-0549, 0552-0554, 0559, 0562, 0566, 0569-0570, 0572, 0574, 0576-0579, 0581, 0583,0585-0586, 0588, 0590, 0593-0594, 0596, 0598-0603, 0605, 0607-0612, 0615-0619, 0621-0630, 0634-0637, 0639, 0641-0651, 0653-0654,0656-0658, 0660, 0662, 0664-0666, 0669-0675, 0677, 0679, 0681-0682, 0684-0685, 0688-0689, 0691, 0693-0695, 0697, 0700-0701, 0703,0706-0707, 0711, 0713-0714, 0716-0717, 0719, 0721, 0723-0724, 0726-0730, 0732, 0734-0738, 0740, 0742, 0744-0745, 0749-0750, 0752-0755,0757, 0761, 0763-0769, 0772-0779, 0781-0782, 0785-0786, 0790, 0793-0797, 0799-0801, 0807-0809, 0813-0815, 0817-0819, 0821, 0823,0827-0833, 0837-0838, 0840-0841, 0844-0846, 0848, 0852-0854, 0860-0861, 0863, 0868-0870, 0875-0876, 0879-0880, 0883-0885, 0888,0890-0891, 0894, 0896-0897, 0903-0907, 0909, 0911, 0914, 0917, 0920-0923, 0925-0926, 0929, 0933, 0935-0942, 0945-0947, 0949, 0951,0956-0962, 0964, 0967, 0970-0973, 0975, 0978-0979, 0981-0982, 0984-0988, 0991-0992, 0994-1000, 1002, 1005-1006, 1009, 1011-1012,1016-1021, 1023, 1025-1030, 1033-1034, 1036-1038, 1040-1041, 1044, 1046-1048, 1051-1052, 1054-1055, 1058-1059, 1061-1063, 1065,1067-1073, 1077-1078, 1081, 1084, 1086-1087, 1089-1091, 1093-1095, 1097, 1099-1102, 1106-1109, 1112, 1114, 1119-1122, 1124-1127,1129-1138, 1141, 1144-1145, 1147-1152, 1154-1155, 1157, 1160, 1162, 1164-1165, 1167-1172, 1175-1176, 1179-1182, 1184-1187, 1189-1191,1198, 1200-1201, 1203, 1205-1206, 1208-1210, 1213, 1216-1217, 1219-1221, 1224, 1226, 1229-1231, 1233, 1237-1238, 1241-1242, 1244-1245,1247, 1249-1250, 1252, 1254-1255, 1259, 1262-1265, 1267-1269, 1271, 1275, 1277, 1283, 1285-1289, 1292, 1294, 1296-1299, 1301, 1303,1305-1320, 1322, 1324-1326, 1328, 1330-1331, 1336-1337, 1340, 1342, 1344-1348, 1352, 1354, 1357-1358, 1360-1362, 1364-1365, 1367,1369-1372, 1377-1379, 1381-1382, 1385-1394, 1396, 1399, 1402-1405, 1412-1417, 1425, 1429-1431, 1434, 1436-1437, 1439, 1441-1444,1447-1451, 1453-1458, 1461-1462, 1465, 1467, 1470-1473, 1476, 1478-1481, 1483-1485, 1488-1489, 1492-1494, 1496, 1498-1499, 1501-1505,1515-1517, 1519-1521, 1524-1525, 1530-1532, 1535-1536, 1539-1544, 1549-1551, 1553-1554, 1556, 1560, 1562, 1564, 1567, 1570-1572,1577-1579, 1582-1583, 1588, 1592, 1597-1599, 1601-1603, 1605, 1607, 1611-1612, 1615-1616, 1618, 1622-1623, 1625, 1629-1630, 1632-1634,1637-1641, 1645-1646, 1651, 1654-1655, 1657-1660, 1662, 1666-1668, 1673-1674, 1677-1679, 1681, 1683-1686, 1691-1694, 1699-1701,1704, 1706, 1709, 1712-1714, 1716-1720, 1722, 1724-1726, 1733, 1735-1736, 1738, 1740, 1742-1748, 1750-1753, 1756-1757, 1759, 1761-1762,1765-1767, 1769-1770, 1772, 1774-1775, 1777-1781, 1783, 1786-1787, 1789, 1791, 1793, 1795-1797, 1799-1800, 1803, 1805-1806, 1808-1812,1815-1816, 1819-1820, 1824, 1828, 1833, 1836, 1838-1839, 1841, 1846, 1851-1853, 1859-1860, 1863-1864, 1866-1867, 1870, 1872-1876, 1879,1881-1882, 1884-1887, 1889-1890, 1894, 1897, 1900-1901, 1905-1906, 1908, 1911, 1913, 1916, 1920-1921, 1923-1925, 1929-1932, 1936-1940,1942-1943, 1949, 1951, 1954, 1959-1961, 1963-1966, 1968, 1972-1973, 1975-1976, 1978, 1980-1983, 1988-1991, 1994, 1997, 1999, 2001-2003,2005, 2009-2013, 2017-2019, 2022, 2024-2026, 2028, 2030, 2033-2037, 2039, 2043, 2046-2054, 2056-2057, 2059-2062, 2064-2066,2068-2069, 2071-2072, 2074, 2076, 2078, 2081-2083, 2086-2087, 2091-2093, 2095, 2100-2101, 2103-2104, 2106, 2109, 2113-2117, 2119-2120,2122-2124, 2126-2127, 2129, 2131, 2133-2134, 2140, 2142-2146, 2151, 2154-2155, 2158, 2162-2163, 2165-2166, 2170-2171, 2174-2176,2178-2184, 2186-2187, 2189, 2191, 2196, 2198-2199, 2206-2209, 2212-2214, 2217-2222, 2224-2225, 2227-2228, 2230, 2233, 2235-2237,2239-2245, 2248-2251, 2253, 2256, 2258, 2260, 2262, 2264-2266, 2269-2272, 2274, 2276, 2278-2279, 2283, 2285, 2287, 2289, 2291,2293-2294, 2298, 2300, 2306, 2309, 2311, 2315, 2317-2319, 2325, 2327-2328, 2330, 2332-2333, 2337, 2342, 2344, 2346-2347, 2349-2350,2353-2354, 2357-2358, 2360-2361, 2364-2365, 2367, 2369-2370, 2373-2374, 2377-2378, 2380-2382, 2385, 2387-2388, 2390-2392, 2394,2398-2400, 2402, 2406-2407, 2409, 2411-2412, 2416, 2419-2420, 2425, 2427, 2432, 2436-2437, 2439-2440, 2442, 2446, 2448, 2450-2451,2456, 2460, 2463-2465, 2471-2472, 2474, 2477-2478, 2481, 2483-2484, 2486-2488, 2492-2495, 2497-2499, 2503, 2506-2508, 2511-2512,2514, 2516, 2518-2519, 2523, 2525, 2527-2529, 2532, 2538-2552, 2554-2558, 2561-2563, 2565, 2569, 2575, 2578, 2581-2584, 2586,2588, 2591-2593, 2596, 2599, 2601, 2605-2607, 2611-2612, 2616-2620, 2623-2625, 2627-2629, 2632-2633, 2635-2638, 2641, 2644, 2646,2652, 2654, 2656, 2658, 2662, 2665, 2668, 2672, 2674-2675, 2677-2678, 2681, 2683-2686, 2691, 2693, 2695-2696, 2699-2700, 2702,2705-2709, 2712, 2715-2716, 2719, 2721, 2726-2727, 2729, 2733, 2735-2736, 2740, 2742-2746, 2748-2751, 2754, 2756-2758, 2760-2765,2768-2770, 2773-2774, 2776-2779, 2782, 2785-2786, 2788-2790, 2792, 2794-2796, 2798, 2800-2801, 2803, 2805-2807, 2810-2812, 2816,2818-2822, 2824-2827, 2829-2831, 2834-2837, 2839, 2841-2843, 2846-2847, 2849, 2851-2855, 2857, 2860-2861, 2865-2867, 2869-2870,2873, 2875-2879, 2881-2882, 2884-2885, 2889-2891, 2895, 2897, 2899, 2902-2903, 2905, 2907, 2909-2910, 2912-2913, 2915, 2918,2920-2921, 2923-2926, 2930-2932, 2935, 2937-2939, 2944, 2946-2947, 2949-2951, 2954-2957, 2959-2962, 2964-2968, 2972-2973, 2975,2980, 2985-2986, 2988-2989, 2991, 2993-2996, 2998, 3000, 3002-3003, 3006, 3008-3009, 3014, 3016, 3018-3019, 3021, 3023-3025,3027-3028, 3031, 3035-3038, 3040-3041, 3043-3044, 3046-3048, 3051-3056, 3058-3061, 3063-3065, 3068, 3070, 3073, 3076, 3078-3080,3082-3085, 3087-3088, 3090, 3092-3102, 3107-3111, 3115, 3117-3118, 3121-3123, 3129-3140, 3145-3149, 3151-3155, 3157, 3160-3161,3163-3164, 3168-3171, 3173-3174, 3176, 3178-3182, 3184, 3186-3189, 3191, 3194, 3197, 3199, 3201-3206, 3209, 3211-3213, 3215, 3218,3220-3221, 3223-3226, 3230, 3232-3234, 3236-3238, 3240, 3242-3243, 3245-3247, 3249-3250, 3255-3256, 3260-3262, 3266-3268, 3271-3273,3277-3278, 3281-3282, 3284-3286, 3288-3289, 3291, 3293, 3295, 3298-3300, 3304-3307, 3309-3310, 3312-3313, 3318, 3320-3321,3323-3329, 3331, 3333-3334, 3336-3338, 3340, 3343-3347, 3349, 3353, 3356, 3359, 3361-3364, 3366-3368, 3370, 3372-3374, 3376-3377,3380, 3383, 3385, 3388-3389, 3391, 3394, 3396, 3398-3401, 3403-3404, 3406-3408, 3410-3413, 3415, 3417, 3419-3420, 3422, 3425-3427,3431-3433, 3435-3436, 3440-3448, 3452, 3455-3456, 3460-3461, 3464-3467, 3470-3473, 3475-3477, 3480, 3482, 3485-3487, 3489-3490,3492, 3494, 3498, 3501-3506, 3508, 3511, 3513-3516, 3518, 3521, 3523, 3528-3530, 3532-3533, 3536-3537, 3540, 3542, 3544-3545, 3549,3551, 3553, 3555, 3557, 3559-3560, 3563-3565, 3568-3569, 3571, 3573-3574, 3576, 3579, 3582, 3584, 3586, 3589, 3593-3594, 3596-3599,3601, 3604-3605, 3608-3612, 3615-3617, 3619-3620, 3623, 3626-3634, 3639-3640, 3643-3644, 3646-3648, 3651-3653, 3655-3658, 3660-3662,3664-3667, 3670, 3675, 3678-3679, 3682-3684, 3686-3687, 3689-3691, 3695-3696, 3704, 3706, 3708, 3711, 3715, 3720, 3722-3723, 3725,3727-3729, 3731-3733, 3735, 3739, 3742, 3744, 3746-3747, 3749-3752, 3754-3756, 3762-3763, 3765-3767, 3769, 3774, 3776-3778, 3780-3781,3786-3792, 3794-3795, 3798-3799, 3802, 3805-3806, 3808-3810, 3813-3815, 3817-3819, 3822-3828, 3838, 3843-3846, 3871-3872, 3874-3875,3891-3892, 3903, 3698-3702, 3758, 3830-3831, 3833-3835, 3840, 3848, 3852-3857, 3859, 3861, 3865-3866, 3868, 3879-3880, 3882-3889,3894-3896, 3898, 3900, 3905-3909, 3913-3915, 3918-3919, 3921-3923, 3925, 3928-3933, 3939-3940, 3945-3946, 3949-3950, 3952-3956,3967, 3970-3972, 3983-3984

4




Engines usually start using the Automatic Starting function. The Full Authority Digital Engine Control(FADEC) systems control this engine Automatic Starting function, and takes appropriate action, ifengine parameters are exceeded. This function extends significantly the duration of engine life.The thrust levers must be confirmed at "idle" before engine-start. If the thrust levers are not at "idle",the thrust increases above idle after engine-start, and can result in a hazardous situation. However, anENG START FAULT ECAM warning triggers, to indicate that the flight crew must set the thrust levers to"idle".The engines are started in sequence, preferably engine 2 first, in order to pressurize yellow hydraulicsystem, which supplies the parking brake accumulator.

When the ENG START selector is set to "START", the FADECs are electrically-supplied. When thereis sufficient BLEED PRESS, the PF begins the start sequence by setting the ENG MASTER switch toON. The flight crew should monitor the start sequence:‐ Start valve opens‐ N2 increases‐ IGN A(B)‐ Fuel flow‐ EGT‐ N1‐ Oil pressure increases‐ Start valve closes‐ IGN indication off (Refer to FCOM/PRO-NOR-SOP-08 AUTOMATIC ENGINE START)

When the engine is at idle, or when AVAIL is displayed, the PF can start engine 1.The flight crew should check the relative engine vibration level.When the ENG START selector is set to NORM, the packs return to the OPEN position. APU Bleedshould immediately be turned off, to avoid engine ingestion of exhaust gas.If the start is not successful, the flight crew must use the ECAM as usually done, and avoid instinctivelyselecting the ENG MASTER switch to OFF. This would interrupt the FADEC protective actions (e. g.cranking after hot start).




AVERAGE IDLE ENGINE PARAMETERSIdent.: NO-030-00005457.0003001 / 26 MAR 08Criteria: CFMI�

5 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112, 0115-0162, 0167,0170-0177, 0181-0192, 0195-0197, 0199-0224, 0226-0229, 0231-0242, 0244-0246, 0248, 0253-0255, 0258, 0262-0274, 0277-0279, 0281-0290,0293-0294, 0297-0303, 0305-0307, 0309-0313, 0318-0319, 0323-0325, 0328-0331, 0333, 0337, 0339-0343, 0345-0346, 0348-0350,0352, 0355-0356, 0358-0360, 0365, 0367, 0370-0372, 0375, 0377-0384, 0387-0392, 0395, 0399-0404, 0407-0410, 0413, 0417-0422,0426-0427, 0434, 0436, 0438, 0445-0446, 0459, 0466, 0477, 0482, 0488, 0491, 0494-0495, 0497-0498, 0501, 0507, 0509, 0511, 0513-0516,0521, 0524-0526, 0528-0529, 0531-0532, 0534, 0537, 0544, 0546, 0549, 0554, 0569, 0572, 0576, 0578-0579, 0583, 0586, 0588, 0590,0593-0594, 0598-0601, 0605, 0607-0612, 0615-0619, 0621-0630, 0634, 0636-0637, 0639, 0641, 0644-0651, 0653-0654, 0656-0658, 0660,0662, 0664-0666, 0669-0675, 0677, 0679, 0682, 0684-0685, 0688-0689, 0691, 0693-0695, 0697, 0700, 0706-0707, 0711, 0713-0714,0716-0717, 0719, 0721, 0723-0724, 0726-0730, 0732, 0734-0738, 0740, 0742, 0744-0745, 0749-0750, 0752-0755, 0757, 0761, 0763-0767,0769, 0772-0775, 0777-0779, 0781, 0785-0786, 0790, 0793-0796, 0799-0801, 0807-0809, 0813-0815, 0817-0819, 0821, 0823, 0828-0833,0837-0838, 0840-0841, 0844-0846, 0848, 0852-0854, 0860-0861, 0863, 0868-0869, 0875-0876, 0879-0880, 0883-0885, 0888, 0890, 0894,0896-0897, 0903-0907, 0909, 0911, 0914, 0917, 0921-0923, 0925-0926, 0929, 0933, 0936-0940, 0945-0946, 0949, 0951, 0956-0960, 0962,0964, 0967, 0971-0973, 0975, 0978-0979, 0981-0982, 0984-0986, 0988, 0991-0992, 0994, 0996-1000, 1002, 1005-1006, 1009, 1011,1016-1021, 1023, 1025, 1027-1030, 1033-1034, 1036-1038, 1040-1041, 1044, 1046-1048, 1051-1052, 1055, 1058-1059, 1061-1063, 1065,1067-1073, 1077-1078, 1084, 1086-1087, 1089-1091, 1093-1095, 1097, 1099-1102, 1106-1109, 1112, 1114, 1119-1122, 1124, 1126-1127,1129-1131, 1133-1136, 1138, 1141, 1145, 1147-1149, 1151-1152, 1154-1155, 1157, 1160, 1164-1165, 1167-1172, 1175-1176, 1180-1182, 1184,1187, 1190-1191, 1198, 1200-1201, 1203, 1205-1206, 1208-1210, 1213, 1216-1217, 1219-1221, 1224, 1226, 1229-1231, 1233, 1237-1238, 1242,1245, 1247, 1249-1250, 1252, 1254-1255, 1262-1265, 1267-1269, 1271, 1275, 1277, 1283, 1285-1289, 1292, 1294, 1296-1299, 1301, 1303,1305-1307, 1309-1320, 1324-1326, 1328, 1330-1331, 1336-1337, 1340, 1342, 1344-1348, 1352, 1354, 1357-1358, 1360-1362, 1364-1365, 1367,1369, 1371-1372, 1377-1379, 1381-1382, 1385-1386, 1388-1394, 1396, 1399, 1402-1404, 1412, 1414-1417, 1425, 1429-1431, 1434, 1436-1437,1441-1444, 1447-1449, 1451, 1453-1457, 1461-1462, 1465, 1467, 1471-1473, 1476, 1479-1481, 1483-1485, 1488-1489, 1492-1494, 1496,1498-1499, 1501-1505, 1515-1517, 1519-1521, 1524-1525, 1530-1532, 1535-1536, 1539-1543, 1549-1551, 1553-1554, 1556, 1560, 1562, 1564,1567, 1570-1572, 1577-1579, 1582-1583, 1592, 1597-1599, 1601-1603, 1605, 1607, 1611-1612, 1615-1616, 1618, 1622-1623, 1625, 1629-1630,1632-1634, 1637-1641, 1645-1646, 1651, 1654-1655, 1657-1660, 1662, 1666-1668, 1673-1674, 1677, 1679, 1681, 1683-1686, 1691-1694,1699-1701, 1704, 1706, 1709, 1713-1714, 1716-1720, 1722, 1724-1726, 1733, 1736, 1738, 1740, 1742-1748, 1750-1753, 1756-1757, 1759,1761-1762, 1765-1767, 1769-1770, 1772, 1774-1775, 1777-1781, 1783, 1786-1787, 1789, 1791, 1793, 1795-1797, 1799-1800, 1803, 1805-1806,1808-1812, 1815-1816, 1819-1820, 1824, 1828, 1833, 1836, 1838-1839, 1841, 1846, 1851-1853, 1859-1860, 1863-1864, 1866-1867, 1870,1872-1876, 1879, 1881-1882, 1884-1887, 1889-1890, 1894, 1897, 1900-1901, 1905-1906, 1908, 1911, 1916, 1920-1921, 1923-1925, 1929-1932,1936-1940, 1942-1943, 1949, 1951, 1954, 1959-1961, 1963-1966, 1968, 1972-1973, 1975-1976, 1980-1983, 1988, 1990-1991, 1994, 1997, 1999,2001-2003, 2005, 2009-2013, 2017-2019, 2022, 2024-2026, 2028, 2030, 2033-2037, 2039, 2043, 2046-2054, 2056-2057, 2059-2062, 2064,2066, 2068-2069, 2071-2072, 2074, 2076, 2078, 2081-2083, 2086-2087, 2091-2093, 2095, 2100-2101, 2103-2104, 2106, 2109, 2113-2117,2119-2120, 2122-2124, 2126-2127, 2129, 2131, 2133-2134, 2140, 2142-2145, 2151, 2155, 2158, 2162-2163, 2165-2166, 2170-2171, 2174-2176,2178-2184, 2186-2187, 2189, 2191, 2196, 2198-2199, 2206-2207, 2209, 2212-2214, 2217-2222, 2224-2225, 2227-2228, 2230, 2233, 2235-2237,2239-2245, 2248-2251, 2253, 2256, 2258, 2260, 2262, 2264-2266, 2269-2272, 2274, 2276, 2278-2279, 2283, 2285, 2287, 2289, 2291,2293-2294, 2298, 2300, 2306, 2309, 2311, 2315, 2317-2319, 2325, 2327-2328, 2330, 2332-2333, 2337, 2342, 2344, 2346-2347, 2349-2350,2353-2354, 2357-2358, 2360-2361, 2364-2365, 2367, 2369-2370, 2373-2374, 2377-2378, 2380-2382, 2385, 2387-2388, 2390-2392, 2394,2398-2400, 2402, 2406-2407, 2409, 2411-2412, 2416, 2419-2420, 2425, 2427, 2432, 2436-2437, 2439-2440, 2442, 2446, 2448, 2450-2451,2456, 2460, 2463-2465, 2471-2472, 2474, 2477-2478, 2481, 2483-2484, 2486-2488, 2492-2495, 2497-2499, 2503, 2506-2508, 2511-2512,2514, 2516, 2518-2519, 2523, 2525, 2527-2529, 2532, 2538-2552, 2554-2558, 2561-2563, 2565, 2569, 2575, 2578, 2581-2584, 2586,2588, 2591-2593, 2596, 2599, 2601, 2605-2607, 2611-2612, 2616-2620, 2623-2625, 2627-2629, 2632-2633, 2635-2638, 2641, 2644, 2646,2652, 2654, 2656, 2658, 2662, 2665, 2668, 2672, 2674-2675, 2677-2678, 2681, 2683-2686, 2691, 2693, 2695-2696, 2699-2700, 2702,2705-2709, 2712, 2715-2716, 2719, 2721, 2726-2727, 2729, 2733, 2735-2736, 2740, 2742-2746, 2748-2751, 2754, 2756-2758, 2760-2765,2768-2770, 2773-2774, 2776-2779, 2782, 2785-2786, 2788-2790, 2792, 2794-2796, 2798, 2800-2801, 2803, 2805-2807, 2810-2812, 2816,2818-2822, 2824-2827, 2829-2831, 2834-2837, 2839, 2841-2843, 2846-2847, 2849, 2851-2855, 2857, 2860-2861, 2865-2867, 2869-2870,2873, 2875-2879, 2881-2882, 2884-2885, 2889-2891, 2895, 2897, 2899, 2902-2903, 2905, 2907, 2909-2910, 2912-2913, 2915, 2918,2920-2921, 2923-2926, 2930-2932, 2935, 2937-2939, 2944, 2946-2947, 2949-2951, 2954-2957, 2959-2962, 2964-2968, 2972-2973, 2975,2980, 2985-2986, 2988-2989, 2991, 2993-2996, 2998, 3000, 3002-3003, 3006, 3008-3009, 3014, 3016, 3018-3019, 3021, 3023-3025,3027-3028, 3031, 3035-3038, 3040-3041, 3043-3044, 3046-3048, 3051-3056, 3058-3061, 3063-3065, 3068, 3070, 3073, 3076, 3078-3080,3082-3085, 3087-3088, 3090, 3092-3102, 3107-3111, 3115, 3117-3118, 3121-3123, 3129-3140, 3145-3149, 3151-3155, 3157, 3160-3161,3163-3164, 3168-3171, 3173-3174, 3176, 3178-3182, 3184, 3186-3189, 3191, 3194, 3197, 3199, 3201-3206, 3209, 3211-3213, 3215, 3218,3220-3221, 3223-3226, 3230, 3232-3234, 3236-3238, 3240, 3242-3243, 3245-3247, 3249-3250, 3255-3256, 3260-3262, 3266-3268, 3271-3273,3277-3278, 3281-3282, 3284-3286, 3288-3289, 3291, 3293, 3295, 3298-3300, 3304-3307, 3309-3310, 3312-3313, 3318, 3320-3321,3323-3329, 3331, 3333-3334, 3336-3338, 3340, 3343-3347, 3349, 3353, 3356, 3359, 3361-3364, 3366-3368, 3370, 3372-3374, 3376-3377,3380, 3383, 3385, 3388-3389, 3391, 3394, 3396, 3398-3401, 3403-3404, 3406-3408, 3410-3413, 3415, 3417, 3419-3420, 3422, 3425-3427,3431-3433, 3435-3436, 3440-3448, 3452, 3455-3456, 3460-3461, 3464-3467, 3470-3473, 3475-3477, 3480, 3482, 3485-3487, 3489-3490,3492, 3494, 3498, 3501-3506, 3508, 3511, 3513-3516, 3518, 3521, 3523, 3528-3530, 3532-3533, 3536-3537, 3540, 3542, 3544-3545, 3549,3551, 3553, 3555, 3557, 3559-3560, 3563-3565, 3568-3569, 3571, 3573-3574, 3576, 3579, 3582, 3584, 3586, 3589, 3593-3594, 3596-3599,3601, 3604-3605, 3608-3612, 3615-3617, 3619-3620, 3623, 3626-3634, 3639-3640, 3643-3644, 3646-3648, 3651-3653, 3655-3658, 3660-3662,3664-3667, 3670, 3675, 3678-3679, 3682-3684, 3686-3687, 3689-3691, 3695-3696, 3704, 3706, 3708, 3711, 3715, 3720, 3722-3723, 3725,3727-3729, 3731-3733, 3735, 3739, 3742, 3744, 3746-3747, 3749-3752, 3754-3756, 3762-3763, 3765-3767, 3769, 3774, 3776-3778, 3780-3781,3786-3792, 3794-3795, 3798-3799, 3802, 3805-3806, 3808-3810, 3813-3815, 3817-3819, 3822-3828, 3838, 3843-3846, 3871-3872, 3874-3875,3891-3892, 3903, 3698-3702, 3758, 3830-3831, 3833-3835, 3840, 3848, 3852-3857, 3859, 3861, 3865-3866, 3868, 3879-3880, 3882-3889,3894-3896, 3898, 3900, 3905-3909, 3913-3915, 3918-3919, 3921-3923, 3925, 3928-3933, 3939-3940, 3945-3946, 3949-3950, 3952-3956,3967, 3970-3972, 3983-3984

As soon as the engine-start is complete, the flight crew should check the stabilized parameters. At ISAsea level:

N1 about 19.5 %




N2 about 58.5 %EGT about 390 °CFF about 275 kg/h- 600 lb/h

AVERAGE IDLE ENGINE PARAMETERSIdent.: NO-030-00005457.0001001 / 26 MAR 08Criteria: IAE�Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0113-0114, 0163-0166,0168-0169, 0178-0180, 0193-0194, 0198, 0225, 0230, 0243, 0247, 0249-0252, 0256-0257, 0259-0261, 0275-0276, 0280, 0291-0292, 0295-0296,0304, 0308, 0314-0317, 0320-0322, 0326-0327, 0332, 0334-0336, 0338, 0344, 0347, 0351, 0353-0354, 0357, 0361-0363, 0366, 0368-0369,0373, 0376, 0386, 0393-0394, 0396-0398, 0405-0406, 0411, 0414-0416, 0423-0424, 0428-0432, 0437, 0440-0441, 0443-0444, 0447, 0449,0451, 0467, 0469, 0476, 0478, 0480, 0486, 0490, 0492, 0499


EPR about 1.01N1 about 23.8 %N2 about 57.7 %EGT about 385 °CFF about 330 kg/h - 730 lb/h




Ident.: NO-030-00005457.0010001 / 26 MAR 08Criteria: IAE, G-V2522-A5, G-V2524-A5, G-V2527-A5, G-V2527E-A5, G-V2527M-A5, G-V2530-A5, G-V2533-A5�

6 Applicable to: MSN 0364, 0385, 0412, 0425, 0435, 0439, 0442, 0448, 0450, 0452-0458, 0460-0465, 0468, 0470-0475, 0479, 0483-0485,0487, 0489, 0493, 0496, 0500, 0502-0506, 0508, 0510, 0512, 0518, 0523, 0527, 0530, 0538-0540, 0542-0543, 0550-0551, 0555-0558,0560-0561, 0563-0565, 0567-0568, 0571, 0573, 0575, 0580, 0582, 0584, 0587, 0589, 0591-0592, 0595, 0597, 0604, 0606, 0613-0614, 0620,0631-0633, 0638, 0640, 0652, 0655, 0659, 0661, 0663, 0667-0668, 0676, 0678, 0680, 0683, 0686-0687, 0690, 0692, 0696, 0698-0699,0702, 0704-0705, 0709-0710, 0712, 0715, 0718, 0720, 0722, 0725, 0731, 0733, 0739, 0741, 0743, 0746-0748, 0751, 0756, 0758-0760,0762, 0770-0771, 0780, 0783-0784, 0787-0788, 0791-0792, 0798, 0802-0806, 0810-0812, 0816, 0820, 0822, 0824-0826, 0834-0836,0839, 0842-0843, 0847, 0849-0851, 0855-0859, 0862, 0864-0867, 0871-0874, 0877-0878, 0881-0882, 0886-0887, 0889, 0892-0893, 0895,0898-0902, 0908, 0910, 0912-0913, 0915-0916, 0918-0919, 0924, 0927-0928, 0930-0932, 0934, 0943-0944, 0948, 0950, 0952-0955,0963, 0965-0966, 0968-0969, 0974, 0976-0977, 0980, 0983, 0989-0990, 0993, 1001, 1003-1004, 1007-1008, 1010, 1013-1015, 1022, 1024,1031-1032, 1035, 1039, 1042-1043, 1045, 1049-1050, 1053, 1056-1057, 1060, 1064, 1066, 1074-1076, 1079-1080, 1082-1083, 1085, 1088,1092, 1096, 1098, 1103-1105, 1110-1111, 1113, 1115-1118, 1123, 1128, 1139-1140, 1142-1143, 1146, 1153, 1156, 1158-1159, 1161, 1163, 1166,1173-1174, 1177-1178, 1183, 1188, 1192-1197, 1199, 1202, 1204, 1207, 1211-1212, 1214-1215, 1218, 1222-1223, 1225, 1227-1228, 1232,1234-1236, 1239-1240, 1243, 1246, 1248, 1251, 1253, 1256-1258, 1260-1261, 1266, 1270, 1272-1274, 1276, 1279-1282, 1284, 1290-1291,1293, 1295, 1300, 1302, 1304, 1321, 1323, 1327, 1329, 1332-1335, 1338-1339, 1341, 1343, 1349-1351, 1353, 1355-1356, 1359, 1363,1366, 1368, 1373-1376, 1380, 1383-1384, 1395, 1397-1398, 1400-1401, 1406-1411, 1418-1424, 1426-1428, 1432-1433, 1435, 1438, 1440,1445-1446, 1452, 1459-1460, 1463-1464, 1466, 1468-1469, 1474-1475, 1477, 1482, 1486-1487, 1490-1491, 1495, 1497, 1500, 1506-1514, 1518,1522-1523, 1526-1529, 1533-1534, 1537-1538, 1545-1548, 1552, 1555, 1557-1559, 1561, 1563, 1565-1566, 1568-1569, 1573-1576, 1580-1581,1584-1587, 1589-1591, 1593-1596, 1600, 1604, 1606, 1608-1610, 1613-1614, 1617, 1619-1621, 1624, 1626-1628, 1631, 1635-1636, 1642-1644,1647-1650, 1652-1653, 1656, 1661, 1663-1665, 1669-1672, 1675-1676, 1680, 1682, 1687-1690, 1695-1698, 1702-1703, 1705, 1707-1708,1710-1711, 1715, 1721, 1723, 1727-1732, 1734, 1737, 1739, 1741, 1749, 1754-1755, 1758, 1760, 1763-1764, 1768, 1771, 1773, 1776, 1782,1784-1785, 1788, 1790, 1792, 1794, 1798, 1801-1802, 1804, 1807, 1814, 1817-1818, 1821-1823, 1825-1827, 1829-1832, 1834-1835, 1837, 1840,1842-1845, 1847-1850, 1854-1858, 1861-1862, 1865, 1868-1869, 1871, 1877-1878, 1880, 1883, 1888, 1891-1893, 1895-1896, 1898-1899,1902-1904, 1907, 1909-1910, 1912, 1914-1915, 1917-1918, 1922, 1926-1928, 1933-1935, 1941, 1944-1948, 1950, 1952-1953, 1955-1958,1962, 1967, 1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996, 1998, 2000, 2004, 2006-2008, 2014-2016, 2020-2021, 2023, 2027,2029, 2031-2032, 2038, 2040-2042, 2044-2045, 2055, 2058, 2063, 2067, 2070, 2073, 2075, 2077, 2079-2080, 2084-2085, 2088-2090, 2094,2096-2099, 2102, 2105, 2107-2108, 2110-2112, 2118, 2121, 2125, 2128, 2130, 2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157,2159-2161, 2164, 2167-2169, 2172-2173, 2177, 2185, 2188, 2190, 2192-2195, 2197, 2200-2205, 2210-2211, 2215-2216, 2223, 2226, 2229,2231-2232, 2234, 2238, 2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263, 2267-2268, 2273, 2275, 2277, 2280-2282, 2284, 2286,2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310, 2312-2314, 2316, 2320-2324, 2326, 2329, 2331, 2334-2336, 2338-2341,2343, 2345, 2348, 2351-2352, 2355-2356, 2359, 2362-2363, 2366, 2368, 2371-2372, 2375-2376, 2379, 2383-2384, 2386, 2389, 2393,2395-2397, 2401, 2403-2405, 2408, 2410, 2413-2415, 2417-2418, 2421-2424, 2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445, 2447, 2449,2452-2455, 2457-2459, 2461-2462, 2466-2470, 2473, 2475-2476, 2479-2480, 2482, 2485, 2489-2491, 2496, 2501-2502, 2504-2505, 2509-2510,2513, 2515, 2517, 2520-2522, 2524, 2526, 2530-2531, 2533-2537, 2553, 2559-2560, 2564, 2566-2568, 2570-2574, 2576-2577, 2579-2580,2585, 2587, 2589-2590, 2594-2595, 2597-2598, 2600, 2602-2604, 2608-2610, 2613-2615, 2621-2622, 2626, 2630-2631, 2634, 2639-2640,2642-2643, 2645, 2647-2651, 2653, 2655, 2657, 2659-2661, 2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682, 2687-2690,2692, 2694, 2697-2698, 2701, 2703-2704, 2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728, 2730-2732, 2734, 2737-2739, 2741,2747, 2752-2753, 2755, 2759, 2766-2767, 2771-2772, 2775, 2780-2781, 2783-2784, 2787, 2791, 2793, 2797, 2799, 2802, 2804, 2808-2809,2813-2815, 2817, 2823, 2828, 2832-2833, 2838, 2840, 2844-2845, 2848, 2850, 2856, 2858-2859, 2862-2864, 2868, 2871-2872, 2874, 2880,2883, 2886-2888, 2892-2894, 2896, 2898, 2900-2901, 2904, 2906, 2908, 2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934, 2936,2940-2943, 2945, 2948, 2952-2953, 2958, 2963, 2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992, 2997, 2999, 3004-3005, 3007,3010-3013, 3015, 3017, 3020, 3022, 3026, 3029, 3032-3034, 3039, 3042, 3045, 3049-3050, 3057, 3066-3067, 3069, 3071-3072, 3074-3075,3077, 3081, 3086, 3089, 3091, 3103-3106, 3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159, 3162, 3165-3167,3172, 3175, 3177, 3183, 3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3217, 3219, 3222, 3227-3229, 3231, 3235, 3239,3241, 3244, 3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270, 3274-3276, 3279-3280, 3283, 3287, 3290, 3292, 3294, 3296-3297,3301-3303, 3308, 3311, 3314-3317, 3319, 3322, 3330, 3332, 3335, 3339, 3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365,3369, 3375, 3378-3379, 3381-3382, 3384, 3386-3387, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424,3428-3430, 3434, 3437, 3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468, 3474, 3478-3479, 3481, 3483-3484, 3488, 3491, 3493,3495-3497, 3499-3500, 3507, 3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531, 3534-3535, 3538-3539, 3541, 3543, 3546-3548, 3550,3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572, 3575, 3577-3578, 3580-3581, 3583, 3587-3588, 3590-3592, 3595, 3600, 3603,3607, 3613-3614, 3618, 3621-3622, 3624-3625, 3636-3638, 3641, 3645, 3649-3650, 3654, 3659, 3663, 3668-3669, 3671-3674, 3676-3677,3680-3681, 3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721, 3724, 3726, 3730, 3734, 3736-3738,3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773, 3779, 3782-3785, 3793, 3796-3797, 3800-3801, 3803-3804,3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839, 3841, 3847, 3849-3851, 3858, 3860, 3862-3864, 3867, 3890, 3904, 3920, 3775,3836-3837, 3869, 3873, 3876-3878, 3881, 3893, 3897, 3899, 3901-3902, 3910-3912, 3916-3917, 3924, 3926-3927, 3934-3938, 3941-3944,3947-3948, 3951, 3959-3966, 3968-3969, 3977-3981, 3989-3996


EPR about 1.01




N1 about 21.4 %N2 about 57.8 %EGT about 414 °CFF about 350 kg/h - 775 lb/h

Ident.: NO-030-00005457.0013001 / 26 MAR 08Criteria: CFMI, P3060, P3605, P5594�Applicable to: MSN 0517, 0519-0520, 0522, 0533, 0535, 0541, 0545, 0548, 0552-0553, 0559, 0562, 0566, 0570, 0574, 0577, 0581, 0585, 0596,0603, 0635, 0642-0643, 0681, 0701, 0703, 0768, 0776, 0782, 0797, 0827, 0870, 0891, 0920, 0935, 0941-0942, 0947, 0961, 0970, 0987, 0995,1012, 1026, 1054, 1081, 1125, 1132, 1137, 1144, 1150, 1162, 1179, 1185, 1189, 1241, 1244, 1259, 1308, 1322, 1370, 1387, 1405, 1413, 1439,1450, 1458, 1470, 1478, 1544, 1588, 1678, 1712, 1735, 1913, 1978, 1989, 2065, 2146, 2154, 2208


N1 about 19.5 %N2 about 58.5 %EGT about 640 °CFF about 345 kg/h - 760 lb/h

AVERAGE IDLE ENGINE PARAMETERSIdent.: NO-030-00005457.0002001 / 26 MAR 08Criteria: P6310�Applicable to: MSN 3001, 3030, 3062, 3214, 3216, 3371, 3390, 3438, 3469, 3509, 3585, 3602, 3606, 3635, 3642


N1 about 23 %N2 about 62 %EGT about 435 °CFF about 329 kg/h - 725 lb/h

ENGINE START MALFUNCTIONIdent.: NO-030-00005458.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Following an aborted engine start, the crew will consider an engine dry cranking prior resuming anew engine start attempt. Starter limitations in FCOM, Refer to FCOM/LIM-70 STARTER, must beobserved.




MANUAL ENGINE STARTIdent.: NO-030-00005459.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The flight crew should only perform a manual start if:• The EGT margins are low• The residual EGT is high• A dry crank is performed.

It may be appropriate to perform a manual start in high altitude operations, or after an aborted enginestart.The MANUAL ENGINE START procedure is a "read and do" procedure. Refer to FCOM/99 Duref ciblebefore starting a manual engine start.The FADEC has limited control over the manual start process. It ensures that the engine start valvecloses at 50 % N2. It monitors engine parameters, and generates an associated warning whennecessary.It is recommended that the flight crew use the stopwatch to ensure that the starter engagement timeremains within the limits.

TAILPIPE FIREIdent.: NO-030-00005460.0001001 / 28 MAY 08Criteria: SA�Applicable to: ALL

An engine tailpipe fire may occur at engine-start, and may be the result of either excess fuel in thecombustion chamber, or an oil leak in the low-pressure turbine. A tailpipe fire is an internal fire withinthe engine. No critical areas are affected.

If the ground crew reports a tailpipe fire, the flight crew must perform the following actions:• Shut down the engine (MASTER switch set to OFF)• Do NOT press the ENG FIRE pushbutton• Crank the engine, by using either the bleed of the opposite the engine, the APU bleed, or external

pneumatic power (Set ENG START selector to CRANK, then set the MAN START switch to ON).

Do NOT use the ENG FIRE pushbutton, this would stop power to the FADECs, and would stop themotoring sequence. The fire extinguisher must not be used, as it will not extinguish an internal enginefire. As a first priority, the engine must be ventilated.If the ground crew reports a tailpipe fire, and bleed air is not readily available, a ground fire-extinguisher should be used as last resort: Chemical or dry chemical powder causes serious corrosivedamage to the engine.




ENGINES WARM UP PERIODIdent.: NO-030-00005461.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

After engine-start, and in order to avoid thermal shock of the engine, the engine should be operatedat idle or near idle (Refer to FCOM/PRO-NOR-SOP-09-A AFTER START - ENG MODE SELECTOR)before setting the thrust lever to high power. The warm-up can include any taxi time at idle.

AFTER START FLOW PATTERNIdent.: NO-030-00005462.0001001 / 26 JUN 08Criteria: SA�Applicable to: ALL

When the engines have started, the PF sets the ENG MODE selector to NORM to permit normal packoperation. At this time, the After Start Flow Pattern begins.


NORMAL OPERATIONSTAXI


POWERPUSHIdent.: NO-040-00005463.0001001 / 26 MAR 08Criteria: SA�

1 Applicable to: MSN 0002-0044, 0052-0055, 0059-0073, 0076-0078, 0081-0088, 0091-0094, 0098-0162, 0165-0167, 0170-0178, 0180-0192,0194-0395, 0399-0415, 0417-0422, 0424-0430, 0434-0450, 0452-0468, 0470-0485, 0487-0489, 0491, 0493-0498, 0500-1598, 1600-1659,1661-1938, 1940-1990, 1993-2016, 2018-2034, 2036, 2038-2042, 2044-2049, 2052, 2054-2058, 2060-2061, 2063-2070, 2072-2080, 2082-2099,2101-2108, 2110-2118, 2121-2128, 2130-2169, 2171-2175, 2177-2180, 2182-2183, 2185, 2187-2188, 2190-2195, 2197-2212, 2215-2217,2219-2223, 2225-2227, 2229, 2231-2244, 2246-2248, 2250, 2252-2256, 2258-2264, 2266-2267, 2269-2270, 2272-2275, 2278, 2280, 2282,2284-2288, 2290, 2293-2295, 2298, 2301-2305, 2307, 2309-2316, 2318, 2320-2321, 2323-2325, 2327, 2330-2331, 2334, 2336-2337,2339-2343, 2345, 2347-2349, 2351-2352, 2356-2357, 2359, 2363-2365, 2368-2369, 2371-2374, 2381, 2384, 2386, 2388-2391, 2393, 2397,2399, 2405, 2407-2411, 2415-2416, 2421-2422, 2425-2426, 2428-2430, 2432, 2435, 2437, 2447, 2449, 2451, 2454, 2458-2459, 2461-2462,2464, 2466, 2472, 2474, 2478-2480, 2482, 2486, 2488-2489, 2491, 2493-2494, 2498-2499, 2504-2505, 2507-2510, 2517, 2520-2521, 2525,2530, 2532, 2534-2536, 2542-2543, 2545, 2547, 2549, 2551, 2559, 2562-2563, 2568, 2570, 2574, 2577, 2579-2580, 2583, 2589, 2591, 2595,2597, 2599, 2606, 2613-2615, 2618, 2627, 2630, 2635, 2639-2641, 2643, 2647, 2652, 2667, 2669, 2671, 2682, 2690, 2710, 2725, 2755, 2775,2781, 2802, 2805, 2814-2815, 2819, 2832, 2839, 2847-2848, 2871, 2880, 2890, 2900-2901, 2940, 2945, 2948, 2969-2970, 2977, 2992, 3020,3029, 3039, 3072, 3091, 3104, 3106, 3119, 3144, 3150, 3190, 3195, 3200, 3226, 3228, 3250, 3258, 3263, 3269, 3287, 3311, 3342, 3348

If a Power Push Unit (PPU) is to be used for pushback, the PPU will be placed on the left main landinggear and engine 2 will be started at the gate. This will pressurize the yellow hydraulic circuit for parkingbrake. The nose wheel steering, on green hydraulic circuit, is ensured via the PTU. Prior push back,check that there is no NWS DISC memo on the EWD.The flight crew is in charge of the steering according to ground indications through the interphone.Due to a face-to-face situation between ground personnel and flight crew, a clear understanding ofdirectional phraseology is essential. The engine 1 will be started when the power push is completedand PPU removed.During power push, the crew will not use the brakes, unless required due to an emergency and will notmove flight controls or flap lever.In case of emergency, the PPU should be immediately removed out of the evacuation area.Nevertheless, cabin evacuation is possible with the PPU in place.




Ident.: NO-040-00005463.0003001 / 26 MAR 08Criteria: P4576, SA�

2 Applicable to: MSN 1599, 1660, 1939, 1991, 2017, 2035, 2037, 2043, 2050-2051, 2053, 2059, 2062, 2071, 2081, 2100, 2109, 2119-2120,2129, 2170, 2176, 2181, 2184, 2186, 2189, 2196, 2213-2214, 2218, 2224, 2228, 2230, 2245, 2249, 2251, 2257, 2265, 2268, 2271, 2276-2277,2279, 2281, 2283, 2289, 2291-2292, 2296-2297, 2299-2300, 2306, 2308, 2317, 2319, 2322, 2326, 2328-2329, 2332-2333, 2335, 2338, 2344,2346, 2350, 2353-2355, 2358, 2360-2362, 2366-2367, 2370, 2375-2380, 2382-2383, 2385, 2387, 2392, 2394-2396, 2398, 2400-2404, 2406,2412-2414, 2417-2420, 2423-2424, 2427, 2431, 2433-2434, 2436, 2438-2446, 2448, 2450, 2452-2453, 2455-2457, 2460, 2463, 2465, 2467-2471,2473, 2475-2477, 2481, 2483-2485, 2487, 2490, 2492, 2495-2497, 2501-2503, 2506, 2511-2516, 2518-2519, 2522-2524, 2526-2529, 2531, 2533,2537-2541, 2544, 2546, 2548, 2550, 2552-2558, 2560-2561, 2564-2567, 2569, 2571-2573, 2575-2576, 2578, 2581-2582, 2584-2588, 2590,2592-2594, 2596, 2598, 2600-2605, 2607-2612, 2616-2617, 2619-2626, 2628-2629, 2631-2634, 2636-2638, 2642, 2644-2646, 2648-2651,2653-2666, 2668, 2670, 2672-2681, 2683-2689, 2691-2709, 2711-2724, 2726-2754, 2756-2774, 2776-2780, 2782-2801, 2803-2804, 2806-2813,2816-2818, 2820-2831, 2833-2838, 2840-2846, 2849-2870, 2872-2879, 2881-2889, 2891-2899, 2902-2939, 2941-2944, 2946-2947, 2949-2968,2971-2976, 2978-2991, 2993-3019, 3021-3028, 3030-3038, 3040-3071, 3073-3090, 3092-3103, 3105, 3107-3118, 3120-3143, 3145-3149,3151-3189, 3191-3194, 3196-3199, 3201-3225, 3227, 3229-3249, 3251-3257, 3259-3262, 3264-3268, 3270-3286, 3288-3310, 3312-3341,3343-3347, 3349-3996

If a Power Push Unit (PPU) is to be used for pushback, the PPU will be placed on the left main landinggear and engine 2 will be started at the gate. This will pressurize the yellow hydraulic circuit for parkingbrake and NWS. Prior push back, check that there is no NWS DISC memo on the EWD.The flight crew is in charge the steering according to ground indications through the interphone. Due toa face-to-face situation between ground personnel and flight crew, a clear understanding of directionalphraseology is essential.The engine 1 will be started when the power push is completed and PPU removed.During power push, the crew will not use the brakes, unless required due to an emergency and will notmove flight controls or flap lever.In case of emergency, the PPU should be immediately removed out of the evacuation area.Nevertheless, cabin evacuation is possible with the PPU in place.

TAXI ROLL AND STEERINGIdent.: NO-040-00005464.0001001 / 30 MAY 08Criteria: SA�Applicable to: ALL

Before taxi, check that the amber "NWS DISC" ECAM message is off, to ensure that steering is fullyavailable.

THRUST USE

Only a little power is needed above thrust idle, in order to get the aircraft moving (N1 40 %).Excessive thrust application can result in exhaust-blast damage or Foreign Object Damage (FOD).Thrust should normally be used symmetrically.

TILLER AND RUDDER PEDALS USE

Pedals control nosewheel steering at low speed (± 6 ° with full pedal deflection). Therefore, onstraight taxiways and on shallow turns, the pilot can use the pedals to steer the aircraft, keeping ahand on the tiller. In sharper turns, the pilot must use the tiller.




STEERING TECHNIQUE

The Nosewheel steering is "by-wire" with no mechanical connection between the tiller and thenosewheel. The relationship between tiller deflection and nosewheel angle is not linear and the tillerforces are light.

Therefore, the PF should move the tiller smoothly and maintain the tiller's position. Any correctionshould be small and smooth, and maintained for enough time to enable the pilot to assess theoutcome. Being over-active on the tiller will cause uncomfortable oscillations.On straight taxiways, the aircraft is correctly aligned on the centerline, when the centerline is lined-up between the PFD and ND.

Proper centerline following

If both pilots act on the tiller or pedals, their inputs are added until the maximum value of thesteering angle (programmed within the BSCU) is reached.




When the seating position is correct, the cut-off angle is 20 °, and the visual ground geometryprovides an obscured segment of 42 ft (12.5 m). During taxi, a turn must be initiated before anobstacle approaches the obscured segment. This provides both wing and tail clearance, withsymmetric thrust and no differential braking.Asymmetric thrust can be used to initiate a tight turn and to keep the aircraft moving during the turn.If nosewheel lateral skidding occurs while turning, reduce taxi speed or increase turn radius. Avoidstopping the aircraft in a turn, because excessive thrust will be required to start the aircraft movingagain.The flight crew should be aware that the main gear on the inside of a turn will always cut thecorner and track inside of the nosewheel track. For this reason, the oversteering technique may beconsidered especially for A321 where main gear is 20 m behind the pilot.

Oversteering technique

When exiting a tight turn, the pilot should anticipate the steer out. Additionally, the pilot should allowthe aircraft to roll forward for a short distance to minimize the stress on the main gears.In the event that one or more tires is/are deflated on the main landing gear, the maximum permittedsteering angle will be limited by the aircraft speed. Therefore, with one tire deflated, the aircraftspeed is limited to 7 kt and nosewheel steering can be used. With two tires deflated, the aircraftspeed is limited to 3 ktand nosewheel steering angle should be limited to 30 °.For turns of 90 ° or more, the aircraft speed should be less than 10 kt.

180 ° TURN

For turn of 180°, the following procedure is recommended for making a turn in the most efficient way.

For the CM1• Taxi on the right hand side of the runway and turn left to establish a 25 ° divergence from the

runway axis (using the ND or PFD) with a ground speed between 5 kt and 8 kt• When CM1 assesses to be physically over the runway edge, smoothly initiate a full deflection turn

to the right




• Asymmetric thrust will be used during the turn. Anticipation is required to ensure that asymmetricthrust is established before the turn is commenced, between 30 % and 35 % (or 1.02 and 1.03EPR), to maintain a continuous speed of approximately 5 to 8 kt throughout the manoeuvre

• It is essential to keep minimum ground speed during the turn in order not to need to increase thethrust too significantly so as not to get stuck. It is a good practice that the CM2 calls the GS fromND while in turn

• Differential braking is allowed, but a braked pivot turn is not recommended as a general rule (i.e.braking to fully stop the wheels on one main gear), to avoid stress on the landing gear assembly

• On wet or contaminated runway, more specifically when turning on the runway white oryellow painted marking, tight turn lead to jerky rides of the nose wheel which are noisy anduncomfortable.

For the CM2, the procedure is symmetrical (taxi on the left hand side of the runway).Aircraft dimensions

FIGURESIdent.: NO-040-00005465.0001001 / 26 MAR 08Criteria: 318-100�

3 Applicable to: MSN 1599, 1660, 1939, 1991, 2017, 2035, 2051, 2059, 2071, 2081, 2100, 2109, 2218, 2276, 2317, 2328, 2333, 2344, 2350,2358, 2367, 2377, 2394, 2523, 2544, 2552, 2575, 2582, 2601, 2686, 2750, 2910, 2918, 2931, 2951, 2955, 2967, 2972, 3001, 3009, 3030, 3038,3062, 3092, 3100, 3110, 3163, 3214, 3216, 3220, 3225, 3238, 3333, 3363, 3371, 3390, 3438, 3469, 3509, 3530, 3585, 3602, 3606, 3617, 3635,3642, 3751, 3886, 3932

Y R3 R4 R5 R6 NWS Lim-it Angle

Minimum Run-way Width with

Asymmetric Thrust10 ft 17 in

3.10 m36 ft 42 in

11.10 m67 ft 59 in20.60 m

51 ft 18 in15.60 m

58 ft 73 in17.90 m

75 ° 30 m99 ft




Ident.: NO-040-00005465.0002001 / 26 MAR 08Criteria: 319-100�

4 Applicable to: MSN 0546, 0572, 0578, 0588, 0598, 0600, 0608-0610, 0612, 0616, 0618, 0621, 0623, 0625, 0627, 0629, 0634, 0636-0637,0639, 0641, 0644, 0646-0647, 0649, 0651, 0654, 0656, 0660, 0670, 0672, 0679, 0682, 0686, 0688-0691, 0693-0695, 0697, 0700, 0711, 0713,0717, 0719, 0721, 0723, 0727-0729, 0732, 0734, 0736, 0738, 0740, 0742, 0744, 0748, 0750, 0752, 0755, 0757, 0759, 0763, 0767, 0769, 0773,0779, 0783, 0785, 0788-0790, 0794, 0798, 0800, 0804, 0813, 0817, 0821, 0825, 0829, 0831, 0833, 0837, 0840, 0843, 0845, 0847, 0850, 0853,0858, 0860, 0862, 0867, 0869, 0871, 0873, 0875, 0880, 0882, 0885, 0889-0890, 0893, 0896, 0898, 0904, 0906, 0910, 0913, 0917, 0922,0924, 0929, 0931, 0933, 0938, 0944, 0946, 0948-0949, 0952, 0965, 0972, 0976, 0979-0980, 0985, 0989, 0997-0998, 1000, 1002, 1010, 1016,1018-1020, 1022, 1025, 1029, 1031, 1033-1034, 1036, 1038, 1040, 1043, 1046, 1048-1049, 1051, 1053, 1055-1056, 1058, 1062, 1064, 1066,1068-1069, 1071, 1073-1074, 1077-1078, 1082, 1084, 1086, 1088-1092, 1095-1098, 1100, 1102-1103, 1106-1107, 1109, 1111, 1113, 1115-1116,1118, 1120, 1122, 1124, 1126-1127, 1129, 1131, 1135-1136, 1139-1140, 1142, 1145, 1147, 1149, 1151, 1154-1155, 1157, 1159-1160, 1164-1165,1167, 1169-1170, 1172, 1176, 1178, 1180, 1182, 1184, 1190-1191, 1193, 1197, 1201, 1203, 1205, 1209, 1211-1212, 1216, 1222-1223, 1225, 1228,1230, 1232, 1236, 1239, 1243, 1245, 1247, 1249, 1252, 1254, 1256, 1258, 1261, 1263, 1265, 1267, 1269, 1271, 1275, 1277-1279, 1281, 1283,1285, 1287, 1289, 1291, 1295, 1297, 1301, 1303, 1305, 1309, 1311, 1313, 1315, 1317, 1319, 1321, 1323-1326, 1328-1329, 1331, 1335-1336,1338, 1340, 1342, 1344, 1346, 1348, 1350, 1352, 1354, 1358, 1360, 1362, 1364, 1369, 1371, 1373-1375, 1377-1378, 1380, 1382, 1384, 1386,1388-1389, 1391-1393, 1395, 1397, 1401, 1404, 1406, 1410, 1414-1415, 1420, 1423, 1426, 1429, 1434, 1440, 1444-1445, 1449, 1453, 1456,1460, 1463, 1466, 1468, 1471, 1474, 1477, 1479, 1483, 1485, 1488, 1490, 1494, 1498, 1501, 1505, 1507, 1510, 1513, 1515, 1520, 1522, 1524,1527, 1529, 1534, 1537, 1541, 1543, 1545, 1547, 1549, 1551-1552, 1556, 1558, 1560, 1562-1563, 1565, 1567, 1569-1570, 1573-1577, 1579,1581-1583, 1585, 1589-1590, 1592, 1594, 1598, 1600-1601, 1603-1604, 1606, 1608, 1612, 1616, 1618, 1622, 1625, 1627, 1630, 1634, 1640,1643, 1645, 1647, 1649, 1653-1654, 1656, 1659, 1662, 1664, 1668, 1671, 1673, 1677, 1679, 1683-1685, 1688, 1693, 1698-1699, 1703, 1706,1709, 1714, 1718, 1722, 1727, 1729, 1731, 1733, 1737-1738, 1740, 1742-1743, 1745-1746, 1750, 1752-1753, 1756, 1758-1759, 1761, 1765-1766,1768, 1770, 1774, 1778-1779, 1781, 1786, 1790-1791, 1795-1796, 1800-1801, 1803, 1805, 1808, 1810, 1815, 1819-1820, 1824, 1826, 1828,1831, 1833, 1837, 1839, 1841, 1844, 1846, 1851, 1853, 1855, 1863, 1866, 1870, 1872, 1875-1876, 1880, 1882, 1884, 1886, 1890, 1893,1897, 1901, 1908, 1912, 1916, 1923, 1925, 1934, 1936, 1938, 1943, 1947, 1952, 1955, 1959, 1962-1963, 1971, 1976, 1980, 1982, 1986, 1990,1997, 1999-2000, 2002, 2004, 2007-2008, 2010, 2012-2013, 2015, 2019, 2023, 2026, 2028, 2030, 2032-2033, 2037, 2039, 2043, 2047, 2050,2052-2053, 2057, 2062, 2066, 2069, 2072, 2074, 2078, 2083, 2086-2087, 2089, 2091, 2093, 2095-2096, 2098, 2101, 2103, 2113, 2119-2120,2122, 2124, 2126-2127, 2129, 2131, 2170, 2172, 2174, 2176, 2179, 2181, 2184, 2186, 2188, 2192, 2194, 2196, 2198, 2200, 2202-2203, 2205,2209, 2213-2214, 2222, 2224, 2228, 2230, 2232, 2236-2237, 2240-2241, 2243, 2245, 2249, 2251, 2253, 2258, 2260, 2262-2266, 2268-2269,2271, 2273, 2277, 2279, 2281, 2283, 2285, 2287, 2289, 2293, 2295-2296, 2298, 2300, 2302, 2304, 2306, 2308, 2311, 2313, 2318-2319, 2321,2326, 2332, 2335, 2339, 2341, 2346, 2348, 2353, 2355, 2360, 2362, 2365, 2369-2371, 2373, 2375, 2378-2380, 2382-2383, 2385, 2387,2389, 2392, 2396, 2398, 2400, 2402, 2404, 2406, 2408, 2412, 2414, 2416, 2418, 2420-2421, 2424, 2426-2427, 2429, 2431, 2433, 2435-2436,2438, 2440, 2442, 2444, 2446, 2448, 2450, 2452, 2454, 2456, 2458, 2460, 2463-2471, 2473-2474, 2477, 2481, 2483, 2485, 2487, 2490,2492, 2494-2495, 2497, 2499-2501, 2503, 2505, 2507-2508, 2510, 2512, 2514, 2516, 2518-2519, 2525, 2527-2528, 2532, 2534, 2538, 2541,2545-2548, 2550-2551, 2554-2561, 2565, 2567-2568, 2570, 2572, 2574, 2578-2579, 2581, 2585-2586, 2588, 2592-2593, 2595, 2597, 2603,2605, 2607, 2611, 2614-2615, 2617-2618, 2621-2622, 2624-2625, 2628-2629, 2631-2632, 2634, 2636, 2638-2639, 2641, 2643-2644, 2646,2648, 2650, 2652, 2655, 2657, 2659-2660, 2662, 2664, 2666-2667, 2669, 2672-2673, 2675, 2677, 2679, 2681, 2684, 2690-2691, 2693-2694,2697-2698, 2700, 2702, 2704, 2709, 2711, 2715-2716, 2718, 2720, 2723, 2727, 2729, 2733, 2735, 2738-2739, 2742, 2744, 2746, 2748, 2751,2754, 2757, 2762-2763, 2765, 2769, 2771, 2773-2774, 2777, 2779-2780, 2782, 2784, 2786, 2788, 2790, 2795, 2797, 2803, 2805-2806,2811-2813, 2815, 2818-2819, 2821, 2825, 2827, 2829, 2831, 2833, 2836-2837, 2839, 2841, 2843, 2845, 2847, 2849-2850, 2852, 2854,2857-2858, 2860, 2864, 2866, 2870, 2872-2873, 2876, 2878-2879, 2884, 2886-2894, 2897-2898, 2901, 2905, 2907, 2913, 2921, 2923, 2925,2929, 2935, 2938, 2940, 2942, 2946, 2948-2949, 2954, 2959, 2961, 2963, 2969, 2976, 2978-2979, 2981, 2983, 2985, 2997, 3003, 3007, 3011,3017, 3019-3020, 3024, 3026, 3028, 3032, 3036, 3041, 3043, 3045-3046, 3049, 3053-3054, 3057, 3059, 3061, 3065, 3069, 3073, 3077-3078,3082, 3084-3085, 3088, 3090, 3094, 3096, 3102, 3104, 3108, 3114, 3116, 3118, 3122, 3124, 3128, 3133-3134, 3137, 3139, 3142, 3144, 3165,3168-3169, 3171-3172, 3175-3176, 3179, 3181, 3184, 3186, 3188, 3193, 3195, 3200, 3202, 3204, 3209, 3226, 3231, 3243, 3245, 3248, 3250,3252-3253, 3255, 3258, 3260, 3269, 3271, 3276, 3279, 3281, 3285, 3288, 3292, 3298, 3300, 3305, 3309, 3311, 3317, 3320, 3324, 3331, 3336,3342, 3344, 3346-3347, 3352, 3356, 3358, 3364, 3375, 3377, 3380, 3385, 3388, 3393, 3395, 3403, 3406-3407, 3411, 3413, 3415, 3417, 3421,3424, 3426, 3428, 3432, 3436, 3442-3443, 3445, 3447, 3450, 3452, 3454, 3463, 3466-3467, 3491, 3500, 3513, 3518, 3520, 3533-3534, 3537,3542, 3544, 3548, 3551, 3555, 3560-3561, 3564, 3569, 3571, 3578, 3580, 3586, 3588-3590, 3595, 3604, 3608, 3614-3615, 3620, 3632, 3634,3647, 3651, 3657, 3660-3661, 3663, 3671, 3675, 3680, 3683-3687, 3689, 3691, 3694, 3700, 3702, 3704-3705, 3710, 3720, 3727-3728, 3733,3735, 3742, 3744, 3746, 3754, 3757, 3759, 3763, 3768, 3770, 3772, 3774, 3779, 3788, 3790, 3794, 3799, 3801, 3803, 3808, 3810, 3822,3824, 3828, 3832, 3838-3839, 3841, 3844-3845, 3849, 3851, 3860, 3874, 3888, 3890, 3892, 3903, 2706, 2801, 3638, 3818, 3826, 3834, 3836,3853-3854, 3856, 3865, 3872, 3876, 3895, 3897, 3901, 3905, 3911, 3918, 3950, 3962, 3970, 3983

Y R3 R4 R5 R6 NWS Lim-it Angle

Minimum Runway Widthwith Asymmetric Thrust





Continued from previous page13 ft 2 in4.01 m

39 ft 9 in12.11 m

70 ft 10 in21.58 m

54 ft 6 in16.6 m

64 ft 1 in19.77 m

75 ° 30 m99 ft




FIGURESIdent.: NO-040-00005465.0003001 / 26 MAR 08Criteria: 320-100, 320-200�

5 Applicable to: MSN 0002-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487,0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534, 0537, 0539-0540,0542-0543, 0545, 0548-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569, 0571, 0573-0575, 0577, 0579-0580,0582, 0584-0585, 0587, 0589-0590, 0592, 0594, 0596, 0601-0603, 0605, 0607, 0611, 0613, 0615, 0617, 0619, 0622, 0624, 0626, 0628, 0630,0635, 0638, 0640, 0643, 0645, 0648, 0650, 0653, 0655, 0657-0659, 0661-0662, 0665, 0667, 0669, 0671, 0673, 0676, 0678, 0681, 0683, 0685,0696, 0698, 0701-0710, 0712, 0714, 0716, 0718, 0720, 0722, 0724, 0726, 0730, 0733, 0735, 0737, 0739, 0741, 0743, 0745, 0747, 0749, 0751,0754, 0756, 0758, 0760, 0762, 0764, 0766, 0768, 0770, 0772, 0774, 0776, 0778, 0780, 0782, 0784, 0786, 0791, 0793, 0795, 0797, 0799,0801, 0803, 0805, 0807, 0809, 0812, 0814, 0816, 0818, 0820, 0822, 0824, 0826, 0828, 0830, 0832, 0834, 0836, 0838-0839, 0842, 0844,0846, 0849, 0851, 0854, 0856-0857, 0859, 0861, 0863, 0865-0866, 0868, 0870, 0872, 0874, 0876-0877, 0879, 0881, 0883-0884, 0886, 0888,0892, 0894-0895, 0897, 0899-0900, 0902-0903, 0905, 0907, 0909, 0911-0912, 0914, 0916, 0918-0919, 0921, 0923, 0925, 0927-0928, 0930,0932, 0934, 0936-0937, 0939, 0942-0943, 0945, 0947, 0950-0951, 0953, 0955, 0957-0958, 0960, 0962, 0964, 0966-0967, 0969, 0971, 0973,0975, 0977-0978, 0981-0982, 0984, 0986, 0988, 0990, 0992, 0994, 0996, 0999, 1001, 1003, 1005, 1007, 1009, 1011, 1013-1014, 1026, 1028,1030, 1032, 1035, 1037, 1039, 1041, 1044, 1047, 1050, 1052, 1054, 1057, 1059, 1061, 1063, 1065, 1067, 1070, 1072, 1075-1076, 1079, 1081,1083, 1085, 1087, 1093, 1099, 1101, 1104-1105, 1108, 1110, 1112, 1114, 1117, 1119, 1121, 1123, 1125, 1128, 1130, 1132, 1134, 1137-1138, 1141,1143, 1146, 1148, 1150, 1152, 1156, 1158, 1162-1163, 1166, 1168, 1171, 1173, 1175, 1177, 1179, 1181, 1183, 1187, 1189, 1192, 1194, 1196,1198, 1200, 1206, 1208, 1210, 1213, 1215, 1217, 1221, 1224, 1226, 1229, 1231, 1234-1235, 1237, 1240, 1242, 1244, 1246, 1248, 1251, 1253,1255, 1257, 1259, 1262, 1264, 1266, 1268, 1270, 1272, 1274, 1280, 1282, 1284, 1286, 1288, 1290, 1292, 1294, 1296, 1298, 1300, 1302, 1304,1306, 1308, 1310, 1312, 1314, 1316, 1318, 1320, 1322, 1327, 1330, 1332, 1334, 1337, 1339, 1341, 1343, 1345, 1347, 1349, 1351, 1353, 1355,1357, 1359, 1361, 1363, 1365, 1367-1368, 1370, 1372, 1376, 1379, 1381, 1383, 1385, 1387, 1390, 1394, 1396, 1398, 1400, 1402, 1405, 1407,1409, 1411, 1413, 1416, 1418-1419, 1422, 1424, 1427, 1430, 1432, 1435, 1437, 1439, 1441, 1443, 1446, 1448, 1450, 1452, 1454, 1457, 1459,1461, 1464, 1467, 1469-1470, 1473, 1475, 1478, 1480, 1482, 1484, 1486, 1489, 1491, 1493, 1495, 1497, 1500, 1502, 1504, 1506, 1508-1509,1512, 1514, 1516, 1518, 1523, 1526, 1528, 1530, 1532-1533, 1535, 1538, 1540, 1542, 1544, 1546, 1548, 1550, 1553, 1555, 1557, 1559, 1561,1564, 1566, 1568, 1571, 1578, 1580, 1584, 1586, 1588, 1591, 1593, 1595, 1597, 1605, 1609-1610, 1613, 1615, 1617, 1620-1621, 1624, 1626,1628, 1631, 1633, 1635, 1637, 1639, 1641, 1644, 1646, 1648, 1650, 1652, 1655, 1657, 1661, 1663, 1665, 1667, 1669, 1672, 1674, 1676, 1678,1680, 1682, 1686-1687, 1689, 1692, 1694, 1696-1697, 1700, 1702, 1705, 1708, 1710, 1712, 1715, 1717, 1719, 1721, 1723, 1725, 1728, 1730,1732, 1735-1736, 1739, 1741, 1744, 1747, 1749, 1751, 1754-1755, 1757, 1760, 1762, 1764, 1767, 1769, 1771, 1773, 1775, 1777, 1780, 1782,1784-1785, 1787, 1789, 1792-1793, 1797, 1799, 1802, 1804, 1806, 1809, 1812-1814, 1816, 1818, 1821-1823, 1825, 1827, 1829, 1832, 1834-1835,1838, 1840, 1842, 1845, 1847, 1849, 1852, 1854, 1856-1858, 1860-1862, 1864-1865, 1867-1868, 1871, 1873-1874, 1877, 1879, 1883, 1885,1888-1889, 1891-1892, 1894-1896, 1898-1900, 1902-1904, 1906-1907, 1909-1911, 1913-1915, 1917-1920, 1922, 1924, 1927, 1929-1931, 1933,1935, 1937, 1940, 1942, 1944-1945, 1948-1949, 1951, 1954, 1957-1958, 1961, 1964-1965, 1968-1969, 1973, 1975, 1979, 1981, 1983, 1987,1989, 1993, 1996, 1998, 2001, 2003, 2006, 2009, 2011, 2014, 2016, 2018, 2020, 2022, 2024, 2027, 2029, 2031, 2034, 2036, 2038, 2040, 2042,2044, 2046, 2048-2049, 2054, 2056, 2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2077, 2079, 2082, 2084-2085, 2088, 2090, 2092,2094, 2097, 2099, 2102, 2104, 2106, 2108, 2112, 2114, 2116, 2118, 2121, 2123, 2125, 2128, 2130, 2132-2169, 2171, 2173, 2175, 2177-2178,2180, 2182-2183, 2185, 2187, 2189, 2191, 2193, 2195, 2197, 2199, 2201, 2204, 2206-2207, 2210, 2212, 2215, 2217, 2219, 2221, 2223, 2225,2227, 2229, 2231, 2233, 2235, 2238-2239, 2242, 2244, 2246, 2248, 2250, 2252, 2254, 2256-2257, 2259, 2272, 2274-2275, 2278, 2280, 2282,2284, 2286, 2288, 2291-2292, 2294, 2297, 2299, 2301, 2307, 2310, 2312, 2314, 2316, 2322, 2325, 2327, 2329, 2331, 2334, 2336, 2338, 2340,2343, 2345, 2347, 2349, 2352, 2354, 2356, 2359, 2361, 2364, 2366, 2368, 2372, 2374, 2376, 2384, 2386, 2388, 2390-2391, 2393, 2395,2397, 2399, 2401, 2403, 2405, 2407, 2409, 2411, 2413, 2415, 2417, 2419, 2422-2423, 2425, 2428, 2430, 2432, 2434, 2437, 2439, 2441, 2443,2445, 2447, 2449, 2451, 2453, 2455, 2457, 2459, 2461, 2475, 2478-2479, 2482, 2484, 2486, 2489, 2491, 2493, 2496, 2498, 2502, 2504, 2506,2509, 2511, 2513, 2515, 2517, 2520, 2522, 2524, 2526, 2529, 2531, 2533, 2535, 2537, 2539-2540, 2542, 2562, 2564, 2566, 2569, 2571, 2573,2576-2577, 2580, 2583-2584, 2587, 2589, 2591, 2594, 2596, 2598, 2600, 2602, 2604, 2606, 2608-2609, 2612-2613, 2616, 2619-2620, 2623,2626-2627, 2630, 2633, 2635, 2637, 2640, 2642, 2645, 2647, 2649, 2651, 2654, 2656, 2658, 2661, 2663, 2665, 2668, 2670-2671, 2674, 2676,2678, 2680, 2683, 2685, 2688-2689, 2692, 2695-2696, 2699, 2701, 2703, 2705, 2708, 2710, 2712, 2714, 2717, 2719, 2721, 2724-2725, 2728,2731-2732, 2734, 2737, 2740, 2743, 2745, 2747, 2749, 2752-2753, 2755, 2758, 2760-2761, 2764, 2766, 2768, 2770, 2772, 2775-2776, 2778,2781, 2783, 2785, 2787, 2789, 2791-2792, 2794, 2796, 2798, 2800, 2802, 2804, 2807-2808, 2810, 2814, 2816-2817, 2820, 2822, 2824, 2826,2828, 2830, 2832, 2834-2835, 2838, 2840, 2842, 2844, 2846, 2848, 2851, 2853, 2855-2856, 2859, 2861, 2863, 2865, 2867, 2869, 2871,2874-2875, 2877, 2880-2881, 2883, 2885, 2896, 2899-2900, 2902, 2904, 2906, 2908-2909, 2911, 2914-2915, 2917, 2920, 2922, 2924, 2926,2928, 2930, 2932, 2934, 2937, 2939, 2941, 2943-2945, 2947, 2950, 2952-2953, 2956, 2958, 2960, 2962, 2964, 2966, 2968, 2970, 2973,2975, 2977, 2980, 2982, 2984, 2986-2995, 2998, 3000, 3002, 3004, 3006, 3008, 3010, 3012, 3014, 3016, 3018, 3021, 3023, 3025, 3027,3029, 3031, 3033, 3035, 3037, 3039-3040, 3042, 3044, 3047-3048, 3050, 3052, 3055-3056, 3058, 3060, 3063-3064, 3066, 3068, 3071-3072,3074, 3076, 3079-3080, 3083, 3086-3087, 3089, 3091, 3093, 3095, 3097, 3099, 3101, 3103, 3105, 3107, 3109, 3111, 3113, 3115, 3117, 3119,3121, 3123, 3125, 3127, 3129, 3131-3132, 3135-3136, 3138, 3140-3141, 3143, 3145, 3147-3162, 3164, 3166-3167, 3170, 3173-3174, 3177-3178,3180, 3182-3183, 3185, 3187, 3189-3190, 3192, 3194, 3196-3197, 3199, 3201, 3203, 3205-3206, 3208, 3210-3211, 3213, 3215, 3218-3219,3221, 3223-3224, 3227-3228, 3230, 3232, 3234, 3236-3237, 3239-3240, 3242, 3244, 3246, 3256-3257, 3259, 3261, 3263-3264, 3266, 3268,3270, 3272-3273, 3275, 3277-3278, 3280, 3282, 3284, 3286-3287, 3289, 3291, 3293, 3295-3296, 3299, 3301, 3303-3304, 3306, 3308, 3310,3312-3314, 3316, 3318-3319, 3321, 3323, 3325, 3327-3328, 3330, 3332, 3335, 3337-3338, 3341, 3343, 3345, 3348-3349, 3351, 3353-3354,3357, 3359, 3361-3362, 3365-3366, 3368, 3370, 3373-3374, 3376, 3378-3379, 3381, 3383-3384, 3386, 3389, 3391-3392, 3394, 3396, 3398,3400, 3402, 3404, 3408-3410, 3412, 3414, 3416, 3418, 3420, 3422-3423, 3425, 3427, 3430-3431, 3433, 3435, 3437, 3439-3440, 3444,3446, 3448-3449, 3451, 3453, 3455-3457, 3460-3461, 3464-3465, 3468, 3470, 3472-3490, 3492, 3494-3497, 3499, 3501-3503, 3505-3506,3508, 3510-3511, 3514-3517, 3519, 3521, 3524, 3526, 3528-3529, 3531-3532, 3535-3536, 3538, 3540-3541, 3543, 3545, 3547, 3549-3550,3553-3554, 3556, 3558-3559, 3562-3563, 3565, 3567-3568, 3570, 3572, 3574, 3576-3577, 3579, 3581-3582, 3594, 3596-3599, 3601, 3603,3605, 3607, 3609-3611, 3613, 3616, 3618, 3621-3622, 3624, 3626-3628, 3630-3631, 3640-3641, 3643-3644, 3646, 3648-3650, 3652, 3654,3656, 3658-3659, 3662, 3664, 3666-3668, 3670, 3672, 3674, 3676-3677, 3679, 3690, 3692-3693, 3695-3699, 3701, 3703, 3706-3707,3709, 3711, 3713-3716, 3718-3719, 3721, 3723-3724, 3726, 3729, 3731-3732, 3734, 3736, 3739, 3741, 3743, 3745, 3747-3748, 3750, 3753,3755-3756, 3760, 3762, 3765, 3767, 3769, 3771, 3773, 3780-3783, 3785-3787, 3789, 3791, 3793, 3795, 3800, 3802, 3804-3805, 3807, 3809,3811-3813, 3815, 3817, 3823, 3829, 3835, 3843, 3850, 3863, 3871, 3875, 3891, 3904, 3937, 3591, 3758, 3775-3778, 3797-3798, 3819, 3821,3825, 3827, 3831, 3833, 3837, 3840, 3846, 3848, 3852, 3855, 3857, 3859, 3861, 3866, 3868, 3873, 3877, 3880, 3882-3883, 3885, 3887, 3889,3894, 3896, 3898, 3900, 3902, 3906-3910, 3912-3915, 3917, 3919, 3921-3923, 3925, 3927, 3931, 3933, 3935, 3939, 3941-3943, 3945-3947,3949, 3952-3954, 3956-3959, 3965, 3967-3968, 3971-3972, 3984, 3995

Y R3 R4 R5 R6 NWS Limit Angle Minimum Runway Widthwith Asymmetric Thrust





Continued from previous page15 ft 1 in4.61 m

45 ft 5 in13.84 m

72 ft 2 in21.99 m

60 ft18.3 m

71 ft 1 in21.91 m

75 ° 30 m99 ft

Ident.: NO-040-00005465.0005001 / 26 MAR 08Criteria: 321-100, 321-200�

6 Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522,0524, 0526, 0529, 0532, 0535, 0538, 0541, 0544, 0550, 0552, 0555, 0557, 0560, 0563-0564, 0567, 0570, 0576, 0581, 0583, 0586, 0591, 0593,0595, 0597, 0599, 0604, 0606, 0614, 0620, 0631-0633, 0642, 0652, 0663-0664, 0666, 0668, 0674-0675, 0677, 0680, 0684, 0687, 0692, 0699,0715, 0725, 0731, 0746, 0761, 0765, 0771, 0775, 0777, 0781, 0787, 0792, 0796, 0802, 0806, 0808, 0810-0811, 0815, 0819, 0823, 0827, 0835,0841, 0848, 0852, 0855, 0864, 0878, 0887, 0891, 0901, 0908, 0915, 0920, 0926, 0935, 0940-0941, 0954, 0956, 0959, 0961, 0963, 0968, 0970,0974, 0983, 0987, 0991, 0993, 0995, 1004, 1006, 1008, 1012, 1015, 1017, 1021, 1023-1024, 1027, 1042, 1045, 1060, 1080, 1094, 1133, 1144,1153, 1161, 1174, 1185, 1188, 1195, 1199, 1202, 1204, 1207, 1214, 1218-1220, 1227, 1233, 1238, 1241, 1250, 1260, 1273, 1276, 1293, 1299,1307, 1333, 1356, 1366, 1399, 1403, 1408, 1412, 1417, 1421, 1425, 1428, 1431, 1433, 1436, 1438, 1442, 1447, 1451, 1455, 1458, 1462, 1465,1472, 1476, 1481, 1487, 1492, 1496, 1499, 1503, 1511, 1517, 1519, 1521, 1525, 1531, 1536, 1539, 1554, 1572, 1587, 1596, 1602, 1607, 1611,1614, 1619, 1623, 1629, 1632, 1636, 1638, 1642, 1651, 1658, 1666, 1670, 1675, 1681, 1690-1691, 1695, 1701, 1704, 1707, 1711, 1713, 1716,1720, 1724, 1726, 1734, 1748, 1763, 1772, 1776, 1783, 1788, 1794, 1798, 1807, 1811, 1817, 1836, 1843, 1848, 1850, 1859, 1869, 1878, 1881,1887, 1905, 1921, 1926, 1928, 1932, 1941, 1946, 1950, 1953, 1956, 1960, 1966-1967, 1970, 1972, 1974, 1977-1978, 1984, 1988, 1994-1995,2005, 2021, 2041, 2045, 2055, 2060, 2064, 2067, 2076, 2080, 2105, 2107, 2110, 2115, 2117, 2190, 2208, 2211, 2216, 2220, 2226, 2234, 2247,2255, 2261, 2267, 2270, 2290, 2303, 2305, 2309, 2315, 2320, 2323-2324, 2330, 2337, 2342, 2351, 2357, 2363, 2381, 2410, 2462, 2472, 2476,2480, 2488, 2521, 2530, 2536, 2543, 2549, 2553, 2563, 2590, 2599, 2610, 2653, 2682, 2687, 2707, 2713, 2726, 2730, 2736, 2741, 2756,2759, 2767, 2793, 2799, 2809, 2823, 2862, 2868, 2882, 2895, 2903, 2912, 2916, 2919, 2927, 2933, 2936, 2957, 2965, 2971, 2974, 2996, 2999,3005, 3013, 3015, 3022, 3034, 3051, 3067, 3070, 3075, 3081, 3098, 3106, 3112, 3120, 3126, 3130, 3146, 3191, 3198, 3207, 3212, 3217, 3222,3229, 3233, 3235, 3241, 3247, 3249, 3251, 3254, 3262, 3265, 3267, 3274, 3283, 3290, 3294, 3297, 3302, 3307, 3315, 3322, 3326, 3329, 3334,3339-3340, 3350, 3355, 3360, 3367, 3369, 3372, 3382, 3387, 3397, 3399, 3401, 3405, 3419, 3429, 3434, 3441, 3458-3459, 3462, 3471, 3493,3498, 3504, 3507, 3512, 3522-3523, 3525, 3527, 3539, 3546, 3552, 3557, 3566, 3573, 3575, 3583-3584, 3587, 3592-3593, 3600, 3612, 3619,3623, 3625, 3629, 3633, 3636-3637, 3639, 3645, 3653, 3655, 3665, 3669, 3673, 3678, 3681-3682, 3688, 3708, 3712, 3717, 3722, 3725, 3730,3737-3738, 3740, 3749, 3752, 3761, 3764, 3766, 3784, 3792, 3796, 3806, 3814, 3816, 3820, 3847, 3858, 3862, 3867, 3878-3879, 3920, 3830,3864, 3869, 3881, 3884, 3893, 3899, 3916, 3924, 3926, 3928-3930, 3934, 3936, 3938, 3940, 3944, 3948, 3951, 3955, 3960, 3964, 3966, 3969,3977-3981, 3989-3993, 3996

Y R3 R4 R5 R6 NWS Limit Angle Minimum Runway Widthwith Asymmetric Thrust

16 ft 9 in5.1 m

59 ft 1 in18 m

74 ft 6 in22.7 m

74 ft 2 in22.6 m

80 ft 5 in24.5 m

75 ° 32 m105 ft

It must be noted that since R6 > R4, wing obstacle clearance does not imply tail obstacle clearance




BRAKE CHECKIdent.: NO-040-00005466.0001001 / 26 MAR 08Criteria: SA�

7 Applicable to: MSN 0002-1598, 1600-1659, 1661-1938, 1940-1990, 1993-2016, 2018-2034, 2036, 2038-2042, 2044-2049, 2052, 2054-2058,2060-2061, 2063-2070, 2072-2080, 2082-2099, 2101-2108, 2110-2118, 2121-2128, 2130-2169, 2171-2175, 2177-2180, 2182-2183, 2185,2187-2188, 2190-2195, 2197-2212, 2215-2217, 2219-2223, 2225-2227, 2229, 2231-2244, 2246-2248, 2250, 2252-2256, 2258-2264, 2266-2267,2269-2270, 2272-2275, 2278, 2280, 2282, 2284-2288, 2290, 2293-2295, 2298, 2301-2305, 2307, 2309-2316, 2318, 2320-2321, 2323-2325,2327, 2330-2331, 2334, 2336-2337, 2339-2343, 2345, 2347-2349, 2351-2352, 2356-2357, 2359, 2363-2365, 2368-2369, 2371-2374, 2381,2384, 2386, 2388-2391, 2393, 2397, 2399, 2405, 2407-2411, 2415-2416, 2421-2422, 2425-2426, 2428-2430, 2432, 2435, 2437, 2447, 2449,2451, 2454, 2458-2459, 2461-2462, 2464, 2466, 2472, 2474, 2478-2480, 2482, 2486, 2488-2489, 2491, 2493-2494, 2498-2499, 2504-2505,2507-2510, 2517, 2520-2521, 2525, 2530, 2532, 2534-2536, 2542-2543, 2545, 2547, 2549, 2551, 2559, 2562-2563, 2568, 2570, 2574, 2577,2579-2580, 2583, 2589, 2591, 2595, 2597, 2599, 2606, 2613-2615, 2618, 2627, 2630, 2635, 2639-2641, 2643, 2647, 2652, 2667, 2669, 2671,2682, 2690, 2710, 2725, 2755, 2775, 2781, 2802, 2805, 2814-2815, 2819, 2832, 2839, 2847-2848, 2871, 2880, 2890, 2900-2901, 2940, 2945,2948, 2969-2970, 2977, 2992, 3020, 3029, 3039, 3072, 3091, 3104, 3106, 3119, 3144, 3150, 3190, 3195, 3200, 3226, 3228, 3250, 3258, 3263,3269, 3287, 3311, 3342, 3348

When cleared to taxi, the PF should set the Parking Brake to "OFF". When the aircraft starts to move,the PF should check the efficiency of the normal braking system by gently pressing the brake pedals,to ensure that the aircraft slows down. The PNF should also check the triple brake indicator to ensurethat brake pressure drops to zero. This indicates a successful changeover to the normal brakingsystem.



When cleared to taxi, the PF should set the Parking Brake to "OFF". When the aircraft starts to move,the PF should check the efficiency of the normal braking system by gently pressing the brake pedals.

CARBON BRAKE WEARIdent.: NO-040-00005467.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Carbon brake wear depends on the number of brake applications and on brake temperature. Itdoes not depend on the applied pressure, or the duration of the braking. The temperature at which




maximum brake wear occurs depends on the brake manufacturer. Therefore, the only way the pilot canminimize brake wear is to reduce the number of brake applications.

TAXI SPEED AND BRAKINGIdent.: NO-040-00005468.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

On long, straight taxiways, and with no ATC or other ground traffic constraints, the PF should allowthe aircraft to accelerate to 30 kt, and should then use one smooth brake application to decelerate to10 kt. The PF should not "ride" the brakes. The GS indication on the ND should be used to assess taxispeed.

BRAKE TEMPERATUREIdent.: NO-040-00005469.0001001 / 28 MAY 08Criteria: SA�

9 Applicable to: MSN 0002-0042, 0044-0112, 0115-0564, 0566-0574, 0576-0579, 0581-0658, 0660, 0662-0666, 0668-0933, 0935-0950,0952-0989, 0991-0998, 1000-1013, 1015-1137, 1139-1167, 1169-1176, 1178-1182, 1184-1216, 1218-1225, 1227-1382, 1384-1406, 1408-1417,1419-1423, 1425-1458, 1460-1696, 1698-1731, 1733-1986, 1988-3996

The FCOM limits brake temperature to 300 °C before takeoff is started.This limit ensures that, in the case of hydraulic fluid leakage, any hydraulic fluid, that may come intocontact with the brake units, will not be ignited in the wheelwell.This limit does not ensure that, in the case of a high energy rejected takeoff, the maximum brakeenergy limitation will be respected.Thermal oxidation increases at high temperatures. Therefore, if the brakes absorb too much heat,carbon oxidation will increase. This is the reason why the brakes should not be used repeatedly attemperatures above 500 °C during normal operation. In addition, after heavy braking, the use ofbrake fans can increase oxidation of the brake surface hot spots, if the brakes are not thermallyequalized.

Ident.: NO-040-00005469.0002001 / 28 MAY 08Criteria: 32-1174, P4507, SA�Applicable to: MSN 0043, 0113-0114, 0565, 0575, 0580, 0659, 0661, 0667, 0934, 0951, 0990, 0999, 1014, 1138, 1168, 1177, 1183, 1217, 1226,1383, 1407, 1418, 1424, 1459, 1697, 1732, 1987

The FCOM limits brake temperature to 260 °C before take-off is started.This limit ensures that, in the case of hydraulic fluid leakage, any hydraulic fluid, that may come intocontact with the brake units, will not be ignited in the wheelwell.This limit does not ensure that, in the case of a high energy rejected takeoff, the maximum brakeenergy limitation will be respected.Thermal oxidation increases at high temperatures. Therefore, if the brakes absorb too much heat,carbon oxidation will increase. This is the reason why the brakes should not be used repeatedly at




temperatures above 500 °C during normal operation. In addition, after heavy braking, the use ofbrake fans can increase oxidation of the brake surface hot spots, if the brakes are not thermallyequalized.

BRAKING ANOMALIESIdent.: NO-040-00005470.0001001 / 26 MAR 08Criteria: SA�

10 Applicable to: MSN 0020-0034, 0040-0042, 0052, 0055, 0059, 0064-0065, 0081-0082, 0103, 0141, 0149-0150, 0158-0160, 0164, 0171, 0176,0189-0190, 0193, 0204, 0210, 0231-0232, 0244, 0249, 0255, 0259-0260, 0263, 0272-0273, 0277, 0281, 0283-0284, 0288, 0290, 0297-0298,0302, 0304-0307, 0309-0313, 0318, 0324, 0330, 0333, 0339-0343, 0345, 0350, 0355-0356, 0359-0360, 0363-0364, 0367-0368, 0370-0372,0378, 0380-0381, 0387-0388, 0391, 0394, 0399, 0402, 0404, 0408, 0410, 0414, 0417-0421, 0424, 0429, 0436, 0441, 0443, 0448-0449, 0471,0521, 0524, 0542, 0546, 0553, 0558, 0561, 0572, 0574, 0586, 0588, 0622, 0629, 0634-0635, 0639, 0643, 0653, 0656-0657, 0662-0665,0672-0673, 0677, 0682, 0696-0697, 0719, 0726, 0728, 0736, 0742, 0749, 0755, 0757, 0762, 0766, 0769-0770, 0773-0774, 0778-0779,0785-0786, 0790, 0793, 0798, 0800-0801, 0803, 0807, 0809-0810, 0817-0818, 0823, 0829-0832, 0838, 0843, 0846, 0850, 0854, 0873, 0882,0884, 0894, 0903-0905, 0907, 0916, 0922-0924, 0929, 0931, 0934, 0938, 0946, 0948-0949, 0953, 0956-0957, 0962, 0971, 0975, 0977-0979,1002-1003, 1006, 1022, 1034, 1040, 1043, 1047, 1049, 1054, 1056, 1058-1059, 1062, 1086-1087, 1092, 1096, 1114, 1122, 1124, 1139, 1144,1149, 1151, 1157, 1167, 1171, 1180, 1183, 1187, 1191, 1195, 1202, 1205, 1210-1211, 1219, 1226, 1229-1230, 1238, 1240, 1243, 1245-1246,1248-1251, 1257, 1263, 1269, 1272, 1274, 1276, 1281, 1284, 1287, 1289, 1297, 1301-1302, 1304, 1311, 1313, 1315, 1323, 1327, 1332-1333,1337-1339, 1349, 1351, 1353, 1355, 1366

If the ACCU PRESS drops below 1 500 PSI, the flight crew should be aware that the Parking Brakecan, quite suddenly, become less efficient. This explains the amber range on the hydraulic pressuregauge of the ACCU PRESS.If the flight crew encounters any braking problems during taxi, they should set the A/SKID & N/WSTRG Sw to OFF. They should not apply pressure to the pedals while setting the A/SKID & N/WSTRG Sw to OFF. Then, the PF should refer to the triple brake indicator and modulate the pressure asnecessary.When parking brake is ON, pressing the pedals has no effect on braking. Consequently, if for anyreason the aircraft moves forward while the park brake is ON, the parking brake must be released inorder to get braking efficiency from the pedals.




Ident.: NO-040-00005470.0002001 / 26 MAR 08Criteria: 32-1201, P4576, P6375, SA�

11 Applicable to: MSN 0002-0019, 0035-0039, 0043-0051, 0053-0054, 0056-0058, 0061-0063, 0066-0080, 0083-0102, 0104-0140, 0142-0148,0151-0157, 0161-0163, 0165-0170, 0172-0175, 0177-0188, 0191-0192, 0194-0203, 0205-0209, 0211-0230, 0233-0243, 0245-0248, 0250-0254,0256-0258, 0261-0262, 0264-0270, 0274-0276, 0278-0280, 0282, 0285-0287, 0289, 0291-0296, 0299-0301, 0303, 0308, 0314-0317, 0319-0323,0325-0329, 0331-0332, 0334-0338, 0344, 0346-0349, 0351-0354, 0357-0358, 0361-0362, 0365-0366, 0369, 0373-0377, 0379, 0382-0386,0389-0390, 0392-0393, 0395-0398, 0400-0401, 0403, 0405-0407, 0409, 0411-0413, 0415-0416, 0422-0423, 0425-0428, 0430-0435, 0437-0440,0442, 0444-0447, 0450-0470, 0472-0520, 0522-0523, 0525-0541, 0543-0545, 0548-0552, 0554-0557, 0559-0560, 0562-0571, 0573,0575-0585, 0587, 0589-0621, 0623-0628, 0630-0633, 0636-0638, 0640-0642, 0644-0652, 0654-0655, 0658-0661, 0666-0671, 0674-0676,0678-0681, 0683-0695, 0698-0718, 0720-0725, 0727, 0729-0735, 0737-0741, 0743-0748, 0750-0754, 0756, 0758-0761, 0763-0765, 0767-0768,0771-0772, 0775-0777, 0780-0784, 0787-0788, 0791-0792, 0794-0797, 0799, 0802, 0804-0806, 0808, 0811-0816, 0819-0822, 0824-0828,0833-0837, 0839-0842, 0844-0845, 0847-0849, 0851-0853, 0855-0872, 0874-0881, 0883, 0885-0893, 0895-0902, 0906, 0908-0915, 0917-0921,0925-0928, 0930, 0932-0933, 0935-0937, 0939-0945, 0947, 0950-0952, 0954-0955, 0958-0961, 0963-0970, 0972-0974, 0976, 0980-1001,1004-1005, 1007-1021, 1023-1033, 1035-1039, 1041-1042, 1044-1046, 1048, 1050-1053, 1055, 1057, 1060-1061, 1063-1085, 1088-1091,1093-1095, 1097-1113, 1115-1121, 1123, 1125-1138, 1140-1143, 1145-1148, 1150, 1152-1156, 1158-1166, 1168-1170, 1172-1179, 1181-1182,1184-1185, 1188-1190, 1192-1194, 1196-1201, 1203-1204, 1206-1209, 1212-1218, 1220-1225, 1227-1228, 1231-1237, 1239, 1241-1242, 1244,1247, 1252-1256, 1258-1262, 1264-1268, 1270-1271, 1273, 1275, 1277-1280, 1282-1283, 1285-1286, 1288, 1290-1296, 1298-1300, 1303,1305-1310, 1312, 1314, 1316-1322, 1324-1326, 1328-1331, 1334-1336, 1340-1348, 1350, 1352, 1354, 1356-1365, 1367-3996

If the ACCU PRESS drops below 1 500 PSI, the flight crew should be aware that the Parking Brakecan, quite suddenly, become less efficient. This explains the amber range on the hydraulic pressuregauge of the ACCU PRESS.If the flight crew encounters any braking problems during taxi, they should set the A/SKID & N/WSTRG Sw to OFF. They should not apply pressure to the pedals while setting the A/SKID & N/WSTRG Sw to OFF. Then, the PF should refer to the triple brake indicator and modulate the pressure asnecessary.




BRAKE FANS Ident.: NO-040-00005471.0001001 / 28 MAY 08Criteria: SA�

12 Applicable to: MSN 0002-0042, 0044-0112, 0115-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476,0478-0483, 0485-0487, 0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534,0537, 0539-0540, 0542-0543, 0545-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0566, 0568-0569, 0571-0574, 0577-0579, 0582,0584-0585, 0587-0590, 0592, 0594, 0596, 0598, 0600-0603, 0605, 0607-0613, 0615-0619, 0621-0630, 0634-0641, 0643-0651, 0653-0658,0660, 0662, 0665, 0669-0673, 0676, 0678-0679, 0681-0683, 0685-0686, 0688-0691, 0693-0698, 0700-0714, 0716-0724, 0726-0730,0732-0745, 0747-0760, 0762-0764, 0766-0770, 0772-0774, 0776, 0778-0780, 0782-0786, 0788-0791, 0793-0795, 0797-0801, 0803-0805,0807, 0809, 0812-0814, 0816-0818, 0820-0822, 0824-0826, 0828-0834, 0836-0840, 0842-0847, 0849-0851, 0853-0854, 0856-0863, 0865-0877,0879-0886, 0888-0890, 0892-0900, 0902-0907, 0909-0914, 0916-0919, 0921-0925, 0927-0933, 0936-0939, 0942-0950, 0952-0953, 0955,0957-0958, 0960, 0962, 0964-0967, 0969, 0971-0973, 0975-0982, 0984-0986, 0988-0989, 0992, 0994, 0996-0998, 1000-1003, 1005, 1007,1009-1011, 1013, 1016, 1018-1020, 1022, 1025-1026, 1028-1041, 1043-1044, 1046-1059, 1061-1079, 1081-1093, 1095-1132, 1134-1137,1139-1143, 1145-1152, 1154-1160, 1162-1167, 1169-1173, 1175-1176, 1178-1182, 1184, 1187, 1189-1194, 1196-1198, 1200-1201, 1203,1205-1206, 1208-1213, 1215-1216, 1221-1225, 1228-1232, 1234-1237, 1239-1240, 1242-1249, 1251-1259, 1261-1272, 1274-1275, 1277-1292,1294-1298, 1300-1306, 1308-1332, 1334-1355, 1357-1365, 1367-1382, 1384-1398, 1400-1402, 1404-1406, 1409-1411, 1413-1416, 1419-1420,1422-1423, 1426-1427, 1429-1430, 1432, 1434-1435, 1437, 1439-1441, 1443-1446, 1448-1450, 1452-1454, 1456-1457, 1460-1461, 1463-1464,1466-1471, 1473-1475, 1477-1480, 1482-1486, 1488-1491, 1493-1495, 1497-1498, 1500-1502, 1504-1510, 1512-1516, 1518, 1520, 1522-1524,1526-1530, 1532-1535, 1537-1538, 1540-1553, 1555-1571, 1573-1586, 1588-1595, 1597-1601, 1603-1606, 1608-1610, 1612-1613, 1615-1618,1620-1622, 1624-1628, 1630-1631, 1633-1635, 1637, 1639-1641, 1643-1650, 1652-1657, 1659-1665, 1667-1669, 1671-1674, 1676-1680,1682-1689, 1692-1694, 1696, 1698-1700, 1702-1703, 1705-1706, 1708-1710, 1712, 1714-1715, 1717-1719, 1721-1723, 1725, 1727-1731,1733, 1735-1747, 1749-1762, 1764-1771, 1773-1775, 1777-1782, 1784-1787, 1789-1793, 1795-1797, 1799-1806, 1808-1810, 1812-1816,1818-1835, 1837-1842, 1844-1847, 1849, 1851-1858, 1860-1868, 1870-1877, 1879-1880, 1882-1886, 1888-1904, 1906-1920, 1922-1925, 1927,1929-1931, 1933-1940, 1942-1945, 1947-1949, 1951-1952, 1954-1955, 1957-1959, 1961-1965, 1968-1969, 1971, 1973, 1975-1976, 1979-1983,1986, 1989-1993, 1996-2004, 2006-2020, 2022-2040, 2042-2044, 2046-2054, 2056-2059, 2061-2063, 2065-2066, 2068-2075, 2077-2079,2081-2104, 2106, 2108-2109, 2112-2114, 2116, 2118-2189, 2191-2207, 2209-2210, 2212-2215, 2217-2219, 2221-2225, 2227-2233, 2235-2246,2248-2254, 2256-2260, 2262-2266, 2268-2269, 2271-2289, 2291-2302, 2304, 2306-2308, 2310-2314, 2316-2319, 2321-2322, 2325-2329,2331-2336, 2338-2341, 2343-2350, 2352-2356, 2358-2362, 2364-2380, 2382-2409, 2411-2461, 2463-2471, 2473-2475, 2477-2479, 2481-2487,2489-2520, 2522-2529, 2531-2535, 2537-2542, 2544-2548, 2550-2552, 2554-2562, 2564-2589, 2591-2598, 2600-2609, 2611-2652, 2654-2681,2683-2686, 2688-2706, 2708-2712, 2714-2725, 2727-2729, 2731-2735, 2737-2740, 2742-2755, 2757-2758, 2760-2766, 2768-2792, 2794-2798,2800-2808, 2810-2822, 2824-2861, 2863-2867, 2869-2881, 2883-2894, 2896-2902, 2904-2911, 2913-2915, 2917-2918, 2920-2926, 2928-2932,2934-2935, 2937-2956, 2958-2964, 2966-2970, 2972-2973, 2975-2995, 2997-2998, 3000-3004, 3006-3012, 3014, 3016-3021, 3023-3033,3035-3050, 3052-3066, 3068-3069, 3071-3074, 3076-3080, 3082-3097, 3099-3105, 3107-3111, 3113-3119, 3121-3125, 3127-3129, 3131-3145,3147-3190, 3192-3197, 3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228, 3230-3232, 3234, 3236-3240, 3242-3246, 3248, 3250,3252-3253, 3255-3261, 3263-3264, 3266, 3268-3273, 3275-3282, 3284-3289, 3291-3293, 3295-3296, 3298-3301, 3303-3306, 3308-3314,3316-3321, 3323-3325, 3327-3328, 3330-3333, 3335-3338, 3341-3349, 3351-3354, 3356-3359, 3361-3366, 3368, 3370-3371, 3373-3381,3383-3386, 3388-3396, 3398, 3400, 3402-3404, 3406-3418, 3420-3428, 3430-3433, 3435-3440, 3442-3457, 3460-3461, 3463-3470,3472-3492, 3494-3497, 3499-3503, 3505-3506, 3508-3511, 3513-3521, 3524, 3526, 3528-3538, 3540-3545, 3547-3551, 3553-3556, 3558-3565,3567-3572, 3574, 3576-3582, 3585-3586, 3588-3591, 3594-3599, 3601-3611, 3613-3618, 3620-3622, 3624, 3626-3628, 3630-3632, 3634-3635,3640-3644, 3646-3652, 3654, 3656-3664, 3666-3668, 3670-3672, 3674-3677, 3679-3680, 3683-3687, 3689-3707, 3709-3711, 3713-3716,3718-3721, 3723-3724, 3726-3729, 3731-3736, 3739, 3741-3748, 3750-3751, 3753-3760, 3762-3763, 3765, 3767-3783, 3785-3791, 3793-3795,3807-3813, 3815, 3817-3819, 3863, 3871-3877, 3937, 3638, 3797-3805, 3821-3829, 3831-3846, 3848-3857, 3859-3861, 3865-3866, 3868,3880, 3882-3883, 3885-3892, 3894-3898, 3900-3915, 3917-3919, 3921-3923, 3925, 3927, 3931-3933, 3935, 3939, 3941-3943, 3945-3947,3949-3950, 3952-3954, 3956-3959, 3962, 3965, 3967-3968, 3970-3972, 3983-3984, 3995

Brake fans cool the brakes, and the brake temperature sensor. Therefore, when the brake fansare running, the indicated brake temperature will be significantly lower than the indicated braketemperature when the brake fans are off.Therefore, as soon as the brake fans are switched on, the indicated brake temperature decreasesalmost instantaneously. On the other hand, when the brake fans are switched off, it will take severalminutes for the indicated brake temperature to increase and match the real brake temperature.




When the fans are running, the difference between the indicated and the actual brake temperaturecan range from 50 °C (when the actual brake temperature is 100 °C) to 150 °C (when the actual braketemperature is 300 °C). Therefore, before takeoff, if the fans are running, the flight crew should refer tothe indicated brake temperature. When the indicated brake temperature is above 150 °C, takeoff mustbe delayed.Brake fans should not be used during takeoff, in order to avoid Foreign Object Damage to fans andbrakes.

FLIGHT CONTROL CHECKIdent.: NO-040-00005472.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

At a convenient stage, before or during taxi, and before arming the autobrake, the PF silently appliesfull longitudinal and lateral sidestick deflection. On the F/CTL page, the PNF checks and calls out fulltravel of elevators and ailerons, and correct deflection and retraction of spoilers. As each full travel/neutral position is reached, the PNF calls out:• "Full up, full down, neutral"• "Full left, full right, neutral"

The PF silently checks that the PNF calls are in accordance with the sidestick order. The PF thenpresses the PEDAL DISC pb on the nose wheel tiller and silently applies full left and full right rudderand then returns the rudder to neutral. The PNF follows on the rudder pedals and, when each fulltravel/neutral position is reached, calls out:• "Full left, full right, neutral"

Full control input must be held for sufficient time for full travel to be reached and indicated on F/CTLpage.The PNF then applies full longitudinal and lateral sidestick deflection, and on the F/CTL page, silentlychecks full travel and correct sense of all elevators and ailerons, and correct deflection and retractionof all spoilers.If this check is carried out during taxiing, it is essential that the PF remains head-up throughout theprocedure.

TAKEOFF BRIEFING CONFIRMATIONIdent.: NO-040-00005473.0001001 / 28 NOV 08Criteria: SA�Applicable to: ALL

13 The TAKEOFF BRIEFING CONFIRMATION should only review any changes that may have occurredsince the full TAKEOFF BRIEFING done at the parking bay (e.g. change of SID, change in runwayconditions, etc.).




If ATC clears the aircraft to maintain a specific heading after takeoff, turn the FCU HDG selector todisarm the NAV. The current aircraft heading will be displayed on the FCU and the ND, and the flightcrew can then set the cleared heading. Once airborne, and above 30 ft, RA, RWY TRK engages. Toapply the clearance, the FCU HDG knob should be pulled. Once cleared to resume the SID, a HDGadjustment may be necessary to intercept the desired track for NAV capture.

TAXI WITH ONE ENGINE SHUTDOWNIdent.: NO-040-00005474.0001001 / 26 MAR 08Criteria: SA�


Brake life and fuel savings may govern company policy on permitting aircraft to taxi with one engineshut down. However, if taxiing out with one engine shutdown, the crew should be aware of thefollowing:• It is recommended to retain the use of engine 1 during taxi to maintain the green hydraulic system

for normal braking and NWS.• Before releasing the parking brake, the yellow electrical pump will be set ON to pressurize the yellow

hydraulic system (ALT/PARK BRK) and avoid PTU operation. The crew will check the hydraulicyellow accumulator pressure.

• Slow or tight turns in the direction of the operating engine may not be possible at high gross weights.• It is not possible for ground personnel to protect the engine against fire, when the aircraft moves

away from the ramp.• The remaining engines should be started with sufficient time for engine warm-up before takeoff.• Any faults encountered during or after starting the remaining engine may require a return to the gate

for maintenance and thus generate a further departure delay.• Taxi with one engine shut down may require higher thrust than usual. Caution must, therefore, be

exercised to avoid excessive jet-blast and the risk of Foreign Object Damage (FOD).• The use of APU is recommended but the APU bleed should be switched off to avoid ingestion of

exhaust gases by the air conditioning system.• Before ENG2 start,

‐ The yellow pump is set off to check correct operation of the PTU‐ APU BLEED is set back to ON for ENG2 bleed start.






Brake life and fuel savings may govern company policy on permitting aircraft to taxi with one engineshut down. However, if taxiing out with one engine shutdown, the crew should be aware of thefollowing:• It is recommended to retain the use of engine 1 during taxi to maintain the green hydraulic system

for normal braking.• Before releasing the parking brake, the yellow electrical pump will be set ON to pressurize the yellow

hydraulic circuit (ALT/PARK BRK and NWS) and avoid PTU operation. The crew will check thehydraulic yellow accumulator pressure.

• Slow or tight turns in the direction of the operating engine may not be possible at high gross weights.• It is not possible for ground personnel to protect the engine against fire, when the aircraft moves

away from the ramp.• The remaining engines should be started with sufficient time for engine warm-up before takeoff.• Any faults encountered during or after starting the remaining engine may require a return to the gate

for maintenance and thus generate a further departure delay.• Taxi with one engine shut down may require higher thrust than usual. Caution must, therefore, be

exercised to avoid excessive jet-blast and the risk of Foreign Object Damage (FOD).• The use of APU is recommended but the APU bleed should be switched off to avoid ingestion of

exhaust gases by the air conditioning system.• Before ENG2 start,

‐ The yellow is set off to check correct operation of the PTU‐ APU BLEED is set back to ON for ENG2 bleed start.




MISCELLANEOUSIdent.: NO-040-00005475.0001001 / 28 MAY 08Criteria: SA�Applicable to: ALL

STROBE LIGHT When the STROBE lights are set to AUTO, they come on automatically when the aircraft is airborne.The ON position can be used to turn on the lights on ground for crossing, backtracking or entering arunway.

PACKS

If the takeoff has to be achieved without air bleed fed from the engines for performance reasons,but air conditioning desired, the APU bleed may be used with packs ON, thus maintaining engineperformance level and passenger comfort. In case of APU auto shut down during takeoff, the enginethrust is frozen till the thrust is manually reduced. The packs revert to engine bleed which causes anincrease of EGT to keep N1/EPR.If the takeoff is performed with one pack unserviceable, the procedure states to set the failed packto OFF. The takeoff may be performed with the other pack ON (if performances permit) with TOGAor FLEX thrust, the pack being supplied by the onside bleed. In this asymmetric bleed configuration,the N1 takeoff value is limited to the value corresponding to the bleed ON configuration and takeoffperformance must be computed accordingly.




TAXI FLOW PATTERNIdent.: NO-040-00005476.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

TAXI FLOW PATTERN


NORMAL OPERATIONSTAKEOFF





THRUST SETTINGIdent.: NO-050-00005477.0001001 / 26 MAR 08Criteria: SA�

1 Applicable to: MSN 0002-0042, 0044-0090, 0093-0112, 0115-0164, 0167-0177, 0179-0193, 0195-0197, 0199-0224, 0226-0242, 0244-0248,0253-0258, 0262-0274, 0277-0279, 0281-0290, 0293-0295, 0297-0319, 0323-0325, 0327-0331, 0333, 0336-0337, 0339-0343, 0345-0346,0348-0350, 0352, 0354-0356, 0358-0360, 0362-0363, 0365, 0367, 0370-0372, 0375, 0377-0384, 0387-0392, 0394-0404, 0407-0411,0413-0414, 0416-0424, 0426-0427, 0431-0434, 0436, 0438, 0443-0446, 0449, 0451, 0459, 0466, 0469, 0476-0477, 0482, 0486, 0488,0490-0492, 0494-0495, 0497-0499, 0501, 0507, 0509, 0511, 0513-0517, 0519-0522, 0524-0526, 0528-0529, 0531-0537, 0541, 0544-0549,0552-0554, 0559, 0562, 0566, 0569-0570, 0572, 0574, 0576-0579, 0581, 0583, 0585-0586, 0588, 0590, 0593-0594, 0596, 0598-0603,0605, 0607-0612, 0615-0619, 0621-0630, 0634-0637, 0639, 0641-0651, 0653-0654, 0656-0658, 0660, 0662, 0664-0666, 0669-0675, 0677,0679, 0681-0682, 0684-0685, 0688-0689, 0691, 0693-0695, 0697, 0700-0701, 0703, 0706-0707, 0711, 0713-0714, 0716-0717, 0719, 0721,0723-0724, 0726-0730, 0732, 0734-0738, 0740, 0742, 0744-0745, 0749-0750, 0752-0755, 0757, 0761, 0763-0769, 0772-0779, 0781-0782,0785-0786, 0790, 0793-0797, 0799-0801, 0807-0809, 0813-0815, 0817-0819, 0821, 0823, 0827-0833, 0837-0838, 0840-0841, 0844-0846, 0848,0852-0854, 0860-0861, 0863, 0868-0870, 0875-0876, 0879-0880, 0883-0885, 0888, 0890-0891, 0894, 0896-0897, 0903-0907, 0909, 0911,0914, 0917, 0920-0923, 0925-0926, 0929, 0933, 0935-0942, 0945-0947, 0949, 0951, 0956-0962, 0964, 0967, 0970-0973, 0975, 0978-0979,0981-0982, 0984-0988, 0991-0992, 0994-1000, 1002, 1005-1006, 1009, 1011-1012, 1016-1021, 1023, 1025-1030, 1033-1034, 1036-1038,1040-1041, 1044, 1046-1048, 1051-1052, 1054-1055, 1058-1059, 1061-1063, 1065, 1067-1073, 1077-1078, 1081, 1084, 1086-1087, 1089-1091,1093-1095, 1097, 1099-1102, 1106-1109, 1112, 1114, 1119-1122, 1124-1127, 1129-1138, 1141, 1144-1145, 1147-1152, 1154-1155, 1157, 1160,1162, 1164-1165, 1167-1172, 1175-1176, 1179-1182, 1184-1187, 1189-1191, 1198, 1200-1201, 1203, 1205-1206, 1208-1210, 1213, 1216-1217,1219-1221, 1224, 1226, 1229-1231, 1233, 1237-1238, 1241-1242, 1244-1245, 1247, 1249-1250, 1252, 1254-1255, 1259, 1262-1265, 1267-1269,1271, 1275, 1277, 1283, 1285-1289, 1292, 1294, 1296-1299, 1301, 1303, 1305-1320, 1322, 1324-1326, 1328, 1330-1331, 1336-1337, 1340,1342, 1344-1348, 1352, 1354, 1357-1358, 1360-1362, 1364-1365, 1367, 1369-1372, 1377-1379, 1381-1382, 1385-1394, 1396, 1399, 1402-1405,1412-1417, 1425, 1429-1431, 1434, 1436-1437, 1439, 1441-1444, 1447-1451, 1453-1458, 1461-1462, 1465, 1467, 1470-1473, 1476, 1478-1481,1483-1485, 1488-1489, 1492-1494, 1496, 1498-1499, 1501-1505, 1515-1517, 1519-1521, 1524-1525, 1530-1532, 1535-1536, 1539-1544,1549-1551, 1553-1554, 1556, 1560, 1562, 1564, 1567, 1570-1572, 1577-1579, 1582-1583, 1588, 1592, 1597-1599, 1601-1603, 1605, 1607,1611-1612, 1615-1616, 1618, 1622-1623, 1625, 1629-1630, 1632-1634, 1637-1641, 1645-1646, 1651, 1654-1655, 1657-1660, 1662, 1666-1668,1673-1674, 1677-1679, 1681, 1683-1686, 1691-1694, 1699-1701, 1704, 1706, 1709, 1712-1714, 1716-1720, 1722, 1724-1726, 1733, 1735-1736,1738, 1740, 1742-1748, 1750-1753, 1756-1757, 1759, 1761-1762, 1765-1767, 1769-1770, 1772, 1774-1775, 1777-1781, 1783, 1786-1787,1789, 1791, 1793, 1795-1797, 1799-1800, 1803, 1805-1806, 1808-1812, 1815-1816, 1819-1820, 1824, 1828, 1833, 1836, 1838-1839, 1841,1846, 1851-1853, 1859-1860, 1863-1864, 1866-1867, 1870, 1872-1876, 1879, 1881-1882, 1884-1887, 1889-1890, 1894, 1897, 1900-1901,1905-1906, 1908, 1911, 1913, 1916, 1920-1921, 1923-1925, 1929-1932, 1936-1940, 1942-1943, 1949, 1951, 1954, 1959-1961, 1963-1966,1968, 1972-1973, 1975-1976, 1978, 1980-1983, 1988-1991, 1994, 1997, 1999, 2001-2003, 2005, 2009-2013, 2017-2019, 2022, 2024-2026,2028, 2030, 2033-2037, 2039, 2043, 2046-2054, 2056-2057, 2059-2062, 2064-2066, 2068-2069, 2071-2072, 2074, 2076, 2078, 2081-2083,2086-2087, 2091-2093, 2095, 2100-2101, 2103-2104, 2106, 2109, 2113-2117, 2119-2120, 2122-2124, 2126-2127, 2129, 2131, 2133-2134,2140, 2142-2146, 2151, 2154-2155, 2158, 2162-2163, 2165-2166, 2170-2171, 2174-2176, 2178-2184, 2186-2187, 2189, 2191, 2196, 2198-2199,2206-2209, 2212-2214, 2217-2222, 2224-2225, 2227-2228, 2230, 2233, 2235-2237, 2239-2245, 2248-2251, 2253, 2256, 2258, 2260, 2262,2264-2266, 2269-2272, 2274, 2276, 2278-2279, 2283, 2285, 2287, 2289, 2291, 2293-2294, 2298, 2300, 2306, 2309, 2311, 2315, 2317-2319,2325, 2327-2328, 2330, 2332-2333, 2337, 2342, 2344, 2346-2347, 2349-2350, 2353-2354, 2357-2358, 2360-2361, 2364-2365, 2367,2369-2370, 2373-2374, 2377-2378, 2380-2382, 2385, 2387-2388, 2390-2392, 2394, 2398-2400, 2402, 2406-2407, 2409, 2411-2412, 2416,2419-2420, 2425, 2427, 2432, 2436-2437, 2439-2440, 2442, 2446, 2448, 2450-2451, 2456, 2460, 2463-2465, 2471-2472, 2474, 2477-2478,2481, 2483-2484, 2486-2488, 2492-2495, 2497-2499, 2503, 2506-2508, 2511-2512, 2514, 2516, 2518-2519, 2523, 2525, 2527-2529, 2532,2538-2552, 2554-2558, 2561-2563, 2565, 2569, 2575, 2578, 2581-2584, 2586, 2588, 2591-2593, 2596, 2599, 2601, 2605-2607, 2611-2612,2616-2620, 2623-2625, 2627-2629, 2632-2633, 2635-2638, 2641, 2644, 2646, 2652, 2654, 2656, 2658, 2662, 2665, 2668, 2672, 2674-2675,2677-2678, 2681, 2683-2686, 2691, 2693, 2695-2696, 2699-2700, 2702, 2705-2709, 2712, 2715-2716, 2719, 2721, 2726-2727, 2729, 2733,2735-2736, 2740, 2742-2746, 2748-2751, 2754, 2756-2758, 2760-2765, 2768-2770, 2773-2774, 2776-2779, 2782, 2785-2786, 2788-2790,2792, 2794-2796, 2798, 2800-2801, 2803, 2805-2807, 2810-2812, 2816, 2818-2822, 2824-2827, 2829-2831, 2834-2837, 2839, 2841-2843,2846-2847, 2849, 2851-2855, 2857, 2860-2861, 2865-2867, 2869-2870, 2873, 2875-2879, 2881-2882, 2884-2885, 2889-2891, 2895, 2897,2899, 2902-2903, 2905, 2907, 2909-2910, 2912-2913, 2915, 2918, 2920-2921, 2923-2926, 2930-2932, 2935, 2937-2939, 2944, 2946-2947,2949-2951, 2954-2957, 2959-2962, 2964-2968, 2972-2973, 2975, 2980, 2985-2986, 2988-2989, 2991, 2993-2996, 2998, 3000-3003, 3006,3008-3009, 3014, 3016, 3018-3019, 3021, 3023-3025, 3027-3028, 3030-3031, 3035-3038, 3040-3041, 3043-3044, 3046-3048, 3051-3056,3058-3065, 3068, 3070, 3073, 3076, 3078-3080, 3082-3085, 3087-3088, 3090, 3092-3102, 3107-3111, 3115, 3117-3118, 3121-3123, 3129-3140,3145-3149, 3151-3155, 3157, 3160-3161, 3163-3164, 3168-3171, 3173-3174, 3176, 3178-3182, 3184, 3186-3189, 3191, 3194, 3197, 3199,3201-3206, 3209, 3211-3216, 3218, 3220-3221, 3223-3226, 3230, 3232-3234, 3236-3238, 3240, 3242-3243, 3245-3247, 3249-3250,3255-3256, 3260-3262, 3266-3268, 3271-3273, 3277-3278, 3281-3282, 3284-3286, 3288-3289, 3291, 3293, 3295, 3298-3300, 3304-3307,3309-3310, 3312-3313, 3318, 3320-3321, 3323-3329, 3331, 3333-3334, 3336-3338, 3340, 3343-3347, 3349, 3353, 3356, 3359, 3361-3364,3366-3368, 3370-3374, 3376-3377, 3380, 3383, 3385, 3388-3391, 3394, 3396, 3398-3401, 3403-3404, 3406-3408, 3410-3413, 3415, 3417,3419-3420, 3422, 3425-3427, 3431-3433, 3435-3436, 3438, 3440-3448, 3452, 3455-3456, 3460-3461, 3464-3467, 3469-3473, 3475-3477,3480, 3482, 3485-3487, 3489-3490, 3492, 3494, 3498, 3501-3506, 3508-3509, 3511, 3513-3516, 3518, 3521, 3523, 3528-3530, 3532-3533,3536-3537, 3540, 3542, 3544-3545, 3549, 3551, 3553, 3555, 3557, 3559-3560, 3563-3565, 3568-3569, 3571, 3573-3574, 3576, 3579, 3582,3584-3586, 3589, 3593-3594, 3596-3599, 3601-3602, 3604-3606, 3608-3612, 3615-3617, 3619-3620, 3623, 3626-3635, 3639-3640, 3642-3644,3646-3648, 3651-3653, 3655-3658, 3660-3662, 3664-3667, 3670, 3675, 3678-3679, 3682-3684, 3686-3687, 3689-3691, 3695-3696, 3704,3706, 3708, 3711, 3715, 3720, 3722-3723, 3725, 3727-3729, 3731-3733, 3735, 3739, 3742, 3744, 3746-3747, 3749-3752, 3754-3756,3762-3763, 3765-3767, 3769, 3774, 3776-3778, 3780-3781, 3786-3792, 3794-3795, 3798-3799, 3802, 3805-3806, 3808-3810, 3813-3815,3817-3819, 3822-3828, 3838, 3843-3846, 3871-3872, 3874-3875, 3891-3892, 3903, 3698-3702, 3758, 3830-3831, 3833-3835, 3840, 3848,3852-3857, 3859, 3861, 3865-3866, 3868, 3879-3880, 3882-3889, 3894-3896, 3898, 3900, 3905-3909, 3913-3915, 3918-3919, 3921-3923,3925, 3928-3933, 3939-3940, 3945-3946, 3949-3950, 3952-3956, 3967, 3970-3972, 3983-3984

The PF should announce "Take-off". The PF then applies power in as follows:




If cross wind is at or below 20 kt and there is no tail wind• From idle to 1.05 EPR / 50 % N1 by reference to the TLA indicator on the EPR / N1 gauge.• When the engine parameters have stabilized, to the FLX/MCT or TOGA detent as appropriate.

In case of tailwind or if cross wind is greater than 20 kt:• From idle to 1.05 EPR / 50 % N1 by reference to the TLA indicator on the EPR / N1 gauge.• Once stabilized, from 1.05 EPR / 50 % N1 to 1.15 EPR / 70 % N1 by reference to the TLA indicator

on the EPR / N1 gauge.• Then, to FLX / TOGA, as required to reach take-off thrust by 40 kt groundspeed.

This procedure ensures that all engines will accelerate similarly. If not properly applied, this may leadto asymmetrical thrust increase, and, consequently, to severe directional control problem.If the thrust levers are not set to the proper take-off detent, e.g. FLX instead of TOGA, a messagecomes up on the ECAM.




Ident.: NO-050-00005477.0002001 / 26 MAR 08Criteria: 73-1065, 73-1075, P7876, SA�

2 Applicable to: MSN 0043, 0091, 0113-0114, 0165-0166, 0178, 0194, 0198, 0225, 0243, 0249-0252, 0259-0261, 0275-0276, 0280, 0291-0292,0296, 0320-0322, 0326, 0332, 0334-0335, 0338, 0344, 0347, 0351, 0353, 0357, 0361, 0364, 0366, 0368-0369, 0373, 0376, 0385-0386,0393, 0405-0406, 0412, 0415, 0425, 0428-0430, 0435, 0437, 0439-0442, 0447-0448, 0450, 0452-0458, 0460-0465, 0467-0468, 0470-0475,0478-0480, 0483-0485, 0487, 0489, 0493, 0496, 0500, 0502-0506, 0508, 0510, 0512, 0518, 0523, 0527, 0530, 0538-0540, 0542-0543,0550-0551, 0555-0558, 0560-0561, 0563-0565, 0567-0568, 0571, 0573, 0575, 0580, 0582, 0584, 0587, 0589, 0591-0592, 0595, 0597, 0604,0606, 0613-0614, 0620, 0631-0633, 0638, 0640, 0652, 0655, 0659, 0661, 0663, 0667-0668, 0676, 0678, 0680, 0683, 0686-0687, 0690,0692, 0696, 0698-0699, 0702, 0704-0705, 0709-0710, 0712, 0715, 0718, 0720, 0722, 0725, 0731, 0733, 0739, 0741, 0743, 0746-0748, 0751,0756, 0758-0760, 0762, 0770-0771, 0780, 0783-0784, 0787-0788, 0791-0792, 0798, 0802-0806, 0810-0812, 0816, 0820, 0822, 0824-0826,0834-0836, 0839, 0842-0843, 0847, 0849-0851, 0855-0859, 0862, 0864-0867, 0871-0874, 0877-0878, 0881-0882, 0886-0887, 0889,0892-0893, 0895, 0898-0902, 0908, 0910, 0912-0913, 0915-0916, 0918-0919, 0924, 0927-0928, 0930-0932, 0934, 0943-0944, 0948, 0950,0952-0955, 0963, 0965-0966, 0968-0969, 0974, 0976-0977, 0980, 0983, 0989-0990, 0993, 1001, 1003-1004, 1007-1008, 1010, 1013-1015,1022, 1024, 1031-1032, 1035, 1039, 1042-1043, 1045, 1049-1050, 1053, 1056-1057, 1060, 1064, 1066, 1074-1076, 1079-1080, 1082-1083,1085, 1088, 1092, 1096, 1098, 1103-1105, 1110-1111, 1113, 1115-1118, 1123, 1128, 1139-1140, 1142-1143, 1146, 1153, 1156, 1158-1159,1161, 1163, 1166, 1173-1174, 1177-1178, 1183, 1188, 1192-1197, 1199, 1202, 1204, 1207, 1211-1212, 1214-1215, 1218, 1222-1223, 1225,1227-1228, 1232, 1234-1236, 1239-1240, 1243, 1246, 1248, 1251, 1253, 1256-1258, 1260-1261, 1266, 1270, 1272-1274, 1276, 1279-1282,1284, 1290-1291, 1293, 1295, 1300, 1302, 1304, 1321, 1323, 1327, 1329, 1332-1335, 1338-1339, 1341, 1343, 1349-1351, 1353, 1355-1356,1359, 1363, 1366, 1368, 1373-1376, 1380, 1383-1384, 1395, 1397-1398, 1400-1401, 1406-1411, 1418-1424, 1426-1428, 1432-1433, 1435, 1438,1440, 1445-1446, 1452, 1459-1460, 1463-1464, 1466, 1468-1469, 1474-1475, 1477, 1482, 1486-1487, 1490-1491, 1495, 1497, 1500, 1506-1514,1518, 1522-1523, 1526-1529, 1533-1534, 1537-1538, 1545-1548, 1552, 1555, 1557-1559, 1561, 1563, 1565-1566, 1568-1569, 1573-1576,1580-1581, 1584-1587, 1589-1591, 1593-1596, 1600, 1604, 1606, 1608-1610, 1613-1614, 1617, 1619-1621, 1624, 1626-1628, 1631, 1635-1636,1642-1644, 1647-1650, 1652-1653, 1656, 1661, 1663-1665, 1669-1672, 1675-1676, 1680, 1682, 1687-1690, 1695-1698, 1702-1703, 1705,1707-1708, 1710-1711, 1715, 1721, 1723, 1727-1732, 1734, 1737, 1739, 1741, 1749, 1754-1755, 1758, 1760, 1763-1764, 1768, 1771, 1773, 1776,1782, 1784-1785, 1788, 1790, 1792, 1794, 1798, 1801-1802, 1804, 1807, 1814, 1817-1818, 1821-1823, 1825-1827, 1829-1832, 1834-1835,1837, 1840, 1842-1845, 1847-1850, 1854-1858, 1861-1862, 1865, 1868-1869, 1871, 1877-1878, 1880, 1883, 1888, 1891-1893, 1895-1896,1898-1899, 1902-1904, 1907, 1909-1910, 1912, 1914-1915, 1917-1918, 1922, 1926-1928, 1933-1935, 1941, 1944-1948, 1950, 1952-1953,1955-1958, 1962, 1967, 1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996, 1998, 2000, 2004, 2006-2008, 2014-2016, 2020-2021,2023, 2027, 2029, 2031-2032, 2038, 2040-2042, 2044-2045, 2055, 2058, 2063, 2067, 2070, 2073, 2075, 2077, 2079-2080, 2084-2085,2088-2090, 2094, 2096-2099, 2102, 2105, 2107-2108, 2110-2112, 2118, 2121, 2125, 2128, 2130, 2132, 2135-2139, 2141, 2147-2150, 2152-2153,2156-2157, 2159-2161, 2164, 2167-2169, 2172-2173, 2177, 2185, 2188, 2190, 2192-2195, 2197, 2200-2205, 2210-2211, 2215-2216, 2223, 2226,2229, 2231-2232, 2234, 2238, 2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263, 2267-2268, 2273, 2275, 2277, 2280-2282, 2284, 2286,2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310, 2312-2314, 2316, 2320-2324, 2326, 2329, 2331, 2334-2336, 2338-2341,2343, 2345, 2348, 2351-2352, 2355-2356, 2359, 2362-2363, 2366, 2368, 2371-2372, 2375-2376, 2379, 2383-2384, 2386, 2389, 2393,2395-2397, 2401, 2403-2405, 2408, 2410, 2413-2415, 2417-2418, 2421-2424, 2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445, 2447, 2449,2452-2455, 2457-2459, 2461-2462, 2466-2470, 2473, 2475-2476, 2479-2480, 2482, 2485, 2489-2491, 2496, 2501-2502, 2504-2505, 2509-2510,2513, 2515, 2517, 2520-2522, 2524, 2526, 2530-2531, 2533-2537, 2553, 2559-2560, 2564, 2566-2568, 2570-2574, 2576-2577, 2579-2580,2585, 2587, 2589-2590, 2594-2595, 2597-2598, 2600, 2602-2604, 2608-2610, 2613-2615, 2621-2622, 2626, 2630-2631, 2634, 2639-2640,2642-2643, 2645, 2647-2651, 2653, 2655, 2657, 2659-2661, 2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682, 2687-2690,2692, 2694, 2697-2698, 2701, 2703-2704, 2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728, 2730-2732, 2734, 2737-2739, 2741,2747, 2752-2753, 2755, 2759, 2766-2767, 2771-2772, 2775, 2780-2781, 2783-2784, 2787, 2791, 2793, 2797, 2799, 2802, 2804, 2808-2809,2813-2815, 2817, 2823, 2828, 2832-2833, 2838, 2840, 2844-2845, 2848, 2850, 2856, 2858-2859, 2862-2864, 2868, 2871-2872, 2874, 2880,2883, 2886-2888, 2892-2894, 2896, 2898, 2900-2901, 2904, 2906, 2908, 2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934, 2936,2940-2943, 2945, 2948, 2952-2953, 2958, 2963, 2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992, 2997, 2999, 3004-3005, 3007,3010-3013, 3015, 3017, 3020, 3022, 3026, 3029, 3032-3034, 3039, 3042, 3045, 3049-3050, 3057, 3066-3067, 3069, 3071-3072, 3074-3075,3077, 3081, 3086, 3089, 3091, 3103-3106, 3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159, 3162, 3165-3167,3172, 3175, 3177, 3183, 3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3217, 3219, 3222, 3227-3229, 3231, 3235, 3239,3241, 3244, 3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270, 3274-3276, 3279-3280, 3283, 3287, 3290, 3292, 3294, 3296-3297,3301-3303, 3308, 3311, 3314-3317, 3319, 3322, 3330, 3332, 3335, 3339, 3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365,3369, 3375, 3378-3379, 3381-3382, 3384, 3386-3387, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424,3428-3430, 3434, 3437, 3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468, 3474, 3478-3479, 3481, 3483-3484, 3488, 3491, 3493,3495-3497, 3499-3500, 3507, 3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531, 3534-3535, 3538-3539, 3541, 3543, 3546-3548, 3550,3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572, 3575, 3577-3578, 3580-3581, 3583, 3587-3588, 3590-3592, 3595, 3600, 3603,3607, 3613-3614, 3618, 3621-3622, 3624-3625, 3636-3638, 3641, 3645, 3649-3650, 3654, 3659, 3663, 3668-3669, 3671-3674, 3676-3677,3680-3681, 3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721, 3724, 3726, 3730, 3734, 3736-3738,3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773, 3779, 3782-3785, 3793, 3796-3797, 3800-3801, 3803-3804,3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839, 3841, 3847, 3849-3851, 3858, 3860, 3862-3864, 3867, 3890, 3904, 3920, 3775,3836-3837, 3869, 3873, 3876-3878, 3881, 3893, 3897, 3899, 3901-3902, 3910-3912, 3916-3917, 3924, 3926-3927, 3934-3938, 3941-3944,3947-3948, 3951, 3959-3966, 3968-3969, 3977-3981, 3989-3996

The PF should announce "Take-off". The PF then applies power in as follows:




If cross wind is at or below 20 kt and there is no tail wind• From idle to 1.05 EPR / 50 % N1 by reference to the TLA indicator on the EPR / N1 gauge.• When the engine parameters have stabilized, to the FLX/MCT or TOGA detent as appropriate.

In case of tailwind or if cross wind is greater than 20 kt:• From idle to 1.05 EPR / 50 % N1 by reference to the TLA indicator on the EPR / N1 gauge.• Then, to FLX / TOGA, as required to reach take-off thrust by 40 kt groundspeed.

This procedure ensures that all engines will accelerate similarly. If not properly applied, this may leadto asymmetrical thrust increase, and, consequently, to severe directional control problem.The Electronic Engine Control (EEC) computer prevents the engine stabilizing between anapproximate range of 60 to 74 % N1, in order to protect against fan flutter. This range is called theKeep-Out-Zone, and the flight crew may notice a non-linear thrust response to thrust lever movement.If one lever is moved out of the Keep-Out-Zone before the other, a very slow movement of the leversmay lead to asymmetric engine acceleration.If the thrust levers are not set to the proper take-off detent, e.g. FLX instead of TOGA, a messagecomes up on the ECAM.

TAKEOFF ROLLIdent.: NO-050-00005478.0001001 / 03 JUL 08Criteria: SA�Applicable to: ALL

Once the thrust is set, the PF announces the indications on the FMA. The PNF must check that thethrust is set by 80 kt and must announce "Thrust Set".The Captain must keep his hand on the thrust levers when the thrust levers are set to TOGA/FLX notchand until V1.On a normal takeoff, to counteract the pitch up moment during thrust application, the PF should applyhalf forward (full forward in cross wind case) sidestick at the start of the takeoff roll until reaching 80 kt.At this point, the input should be gradually reduced to be zero by 100 kt.The PF should use pedals to keep the aircraft straight. The nosewheel steering authority decreasesat a pre-determined rate as the groundspeed increases (no more efficiency at 130 kt) and the rudderbecomes more effective. The use the tiller is not recommended during takeoff roll, because of its highefficiency, which might lead to aircraft overreaction.For crosswind takeoffs, routine use of into wind aileron is not necessary. In strong crosswindconditions, small lateral stick input may be used to maintain wings level, if deemed necessary due to




into wind wing reaction, but avoid using large deflections, resulting in excessive spoiler deploymentwhich increase the aircraft tendency to turn into the wind (due to high weight on wheels on the spoilerextended side), reduces lift and increases drag. Spoiler deflection becomes significant with more thana third sidestick deflection.As the aircraft lifts off, any lateral stick input applied will result in a roll rate demand, making aircraftlateral control more difficult. Wings must be level.In case of low visibility takeoff, visual cues are primary means to track the runway centerline. The PFDyaw bar provides an assistance in case of expected fog patches if ILS available.

TYPICAL AIRCRAFT ATTITUDE AT TAKEOFF AFTER LIFT-OFFIdent.: NO-050-00005479.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

At take off, the typical all engine operating attitude after lift-off is about 15 °.

ROTATIONIdent.: NO-050-00005480.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Rotation is conventional. During the takeoff roll and the rotation, the pilot flying scans rapidly theoutside references and the PFD. Until airborne, or at least until visual cues are lost, this scanningdepends on visibility conditions (the better the visibility, the higher the priority given to outsidereferences). Once airborne, the PF must then controls the pitch attitude on the PFD using FD bars inSRS mode which is then valid.Initiate the rotation with a smooth positive backward sidestick input (typically 1/3 to 1/2 backstick).Avoid aggressive and sharp inputs.The initial rotation rate is about 3 °/s.If the established pitch rate is not satisfactory, the pilot must make smooth corrections on the stick.He must avoid rapid and large corrections, which cause sharp reaction in pitch from the aircraft. If, toincrease the rotation rate, a further and late aft sidestick input is made around the time of lift-off, thepossibility of tailstrike increases significantly on A321.During rotation, the crew must not chase the FD pitch bar, since it does not give any pitch rate order,and might lead to overreaction.Once airborne only, the crew must refine the aircraft pitch attitude using the FD, which is thenrepresentative of the SRS orders. The fly-by-wire control laws change into flight normal law, withautomatic pitch trim active.




AIRCRAFT GEOMETRYIdent.: NO-050-00005481.0001001 / 26 MAR 08Criteria: 318-100�


Tail strike pitch attitudeL/G compressed L/G extended

15.7 ° 17.3 °




AIRCRAFT GEOMETRYIdent.: NO-050-00005481.0002001 / 26 MAR 08Criteria: 319-100�


Tail strike pitch attitudeTo be continued on next page




Continued from previous pageL/G compressed L/G extended

13.9 ° 15.5 °






Tail strike pitch attitudeTo be continued on next page




Continued from previous pageL/G compressed L/G extended

11.7 ° 13.5 °



Tail strike pitch attitudeL/G compressed L/G extended

9.7 ° 11.2 °

TAIL STRIKE AVOIDANCEIdent.: NO-050-00005482.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

INTRODUCTION

If tailstrike it is not a concern for the A318, the importance of this subject increases as fuselagelength increases. Therefore, it is particularly important for A321 operators.Tail strikes can cause extensive structural damage, which can jeopardize the flight and lead to heavymaintenance action. They most often occur in such adverse conditions as crosswind, turbulence,windshear, etc.




MAIN FACTORS

EARLY ROTATION

Early rotation occurs when rotation is initiated below the scheduled VR. The potential reasons forthis are:• The calculated VR is incorrect for the aircraft weight or flap configuration.• The PF commands rotation below VR due to gusts, windshear or an obstacle on the runway.

Whatever the cause of the early rotation, the result will be an increased pitch attitude at lift-off,and consequently a reduced tail clearance.

ROTATION TECHNIQUE

The recommendation given in the ROTATION TECHNIQUE paragraph should be applied.A fast rotation rate increases the risk of tailstrike, but a slow rate increases take-off distance. Therecommended rate is about 3 °/s, which reflects the average rates achieved during flight test, andis also the reference rate for performance calculations.

CONFIGURATION (NOT APPLICABLE TO A318)

When performance is limiting the takeoff weight, the flight crew uses TOGA thrust and selects theconfiguration that provides the highest takeoff weight.When the actual takeoff weight is lower than the permissible one, the flight crew uses FLEX TOthrust. For a given aircraft weight, a variety of flap configurations are possible. Usually, the flightcrew selects the configuration that provides the maximum FLEX temperature. This is done toprolong engine life. The first degrees of flexible thrust have an impact on maintenance costs about5 times higher than the last one.The configuration that provides the maximum FLEX temperature varies with the runway length.On short runways, CONF 3 usually provides the highest FLEX temperature, and the tail clearanceat lift off does not depends on the configuration.On medium or long runways, the second segment limitation becomes the limiting factor, andCONF 2 or CONF 1+F becomes the optimum configuration, in term of FLEX temperature.In these cases, the tail clearance at lift off depends on the configuration. The highest flapconfiguration gives the highest tailstrike margin.

TAKEOFF TRIM SETTING

The main purpose of the pitch trim setting for take-off is to provide consistent rotationcharacteristics. Take-off pitch trim is set manually via the pitch trim wheel.The aircraft performs a safe takeoff, provided the pitch trim setting is within the green band on thepitch trim wheel.




However, the pitch trim setting significantly affects the aircraft behaviour during rotation:• With a forward CG and the pitch trim set to the nose-down limit the pilots will feel an aircraft

"heavy to rotate" and aircraft rotation will be very slow in response to the normal take off stickdisplacement.

• With an aft CG and the pitch trim set to the nose-up limit the pilots will most probably have tocounteract an early autorotation until VR is reached.

In either case the pilot may have to modify his normal control input in order to achieve the desiredrotation rate, but should be cautious not to overreact.

CROSSWIND TAKEOFF

It is said in the TAKEOFF ROLL paragraph that care should be taken to avoid using largedeflection, resulting in excessive spoiler deployment. A direct effect of the reduction in lift due tothe extension of the spoilers on one wing will be a reduction in tail clearance and an increasedrisk of tailstrike.

OLEO INFLATION

The correct extension of the main landing gear shock absorber (and thus the nominal increase intail clearance during the rotation) relies on the correct inflation of the oleos.

ACTION IN CASE OF TAILSTRIKE

If a tailstrike occurs at take-off, flight at attitude requiring a pressurized cabin must be avoided and areturn to the originating airport should be performed for damage assessment.

MAXIMUM DEMONSTRATED CROSSWIND FOR TAKE-OFFIdent.: NO-050-00005483.0001001 / 28 MAY 08Criteria: SA�

7 Applicable to: MSN 0002-1598, 1600-1659, 1661-1938, 1940-1990, 1993-2016, 2018-2034, 2036-2050, 2052-2058, 2060-2070, 2072-2080,2082-2099, 2101-2108, 2110-2217, 2219-2275, 2277-2316, 2318-2327, 2329-2332, 2334-2343, 2345-2349, 2351-2357, 2359-2366, 2368-2376,2378-2393, 2395-2522, 2524-2543, 2545-2551, 2553-2574, 2576-2581, 2583-2600, 2602-2685, 2687-2749, 2751-2909, 2911-2917, 2919-2930,2932-2950, 2952-2954, 2956-2966, 2968-2971, 2973-3000, 3002-3008, 3010-3029, 3031-3037, 3039-3061, 3063-3091, 3093-3099, 3101-3109,3111-3162, 3164-3213, 3215, 3217-3219, 3221-3224, 3226-3237, 3239-3332, 3334-3362, 3364-3370, 3372-3389, 3391-3437, 3439-3468,3470-3508, 3510-3529, 3531-3584, 3586-3601, 3603-3605, 3607-3616, 3618-3634, 3636-3641, 3643-3750, 3752-3885, 3887-3931, 3933-3996

The maximum demonstrated crosswind at takeoff is 29 knots, with gusts up to 38 knots.

Ident.: NO-050-00005483.0002001 / 28 MAY 08Criteria: SA, A318�


The maximum demonstrated crosswind at takeoff is 39 knots (gusts included).




AP ENGAGEMENTIdent.: NO-050-00005484.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The AP can be engaged 5 s after take-off and above 100 ft RA.

VERTICAL PROFILEIdent.: NO-050-00005485.0001001 / 28 MAY 08Criteria: SA�Applicable to: MSN 0029, 0035-0038, 0043, 0052-0055, 0059, 0064-0065, 0068, 0073, 0084, 0091, 0098-0099, 0113-0114, 0119, 0122-0124,0126-0127, 0140-0142, 0149-0150, 0154, 0157, 0159, 0174-0175, 0180, 0183, 0205, 0210, 0221-0222, 0229, 0231-0233, 0242, 0248, 0252-0256,0259-0261, 0265, 0275-0277, 0279, 0283-0284, 0290, 0294-0296, 0299, 0301-0302, 0305, 0309-0311, 0316, 0320-0321, 0324, 0330, 0333,0341-0342, 0348-0350, 0353, 0359, 0361-0363, 0368-0371, 0376, 0378-0379, 0384, 0386, 0389-0392, 0398, 0402-0405, 0426, 0511

SRS engages when the thrust levers are set to the applicable detent for takeoff and will remainengaged until the acceleration altitude.

The SRS pitch command is the minimum of the following pitches:• Pitch required to fly V2 +10 in All Engine Operative case (AEO)• Pitch required to fly IAS at the time of failure (with minimum of V2 and maximum of V2+15) in One

Engine Inoperative case (OEI)• Maximum pitch attitude of 18 °• Pitch required to climb a 120 ft/min minimum vertical speed.

This explains why, during takeoff, the IAS which is actually flown in most cases is neither V2+10 (AEO)nor V2 (OEI).

Ident.: NO-050-00005485.0002001 / 28 MAY 08Criteria: 22-1015, P2316, SA�

9 Applicable to: MSN 0002-0021, 0031-0034, 0039-0042, 0044-0051, 0056-0058, 0061-0063, 0066-0067, 0069-0072, 0074-0083, 0085-0090,0093-0097, 0100-0112, 0115-0118, 0120-0121, 0125, 0128-0139, 0143-0148, 0151-0153, 0155-0156, 0158, 0160-0173, 0176-0179, 0181-0182,0184-0204, 0206-0209, 0211-0220, 0223-0228, 0230, 0234-0241, 0243-0247, 0249-0251, 0257-0258, 0262-0264, 0266-0274, 0278, 0280-0282,0285-0289, 0291-0293, 0297-0298, 0300, 0303-0304, 0306-0308, 0312-0315, 0317-0319, 0322-0323, 0325-0329, 0331-0332, 0334-0340,0343-0347, 0351-0352, 0354-0358, 0360, 0364-0367, 0372-0375, 0377, 0380-0383, 0385, 0387-0388, 0393-0396, 0399-0401, 0406-0425,0427-0510, 0512-3996

SRS engages when the thrust levers are set to the applicable detent for takeoff and will remainengaged until the acceleration altitude.

The SRS pitch command is the minimum of the following pitches:• Pitch required to fly V2 +10 in All Engine Operative case (AEO)• Pitch required to fly IAS at the time of failure (with minimum of V2 and maximum of V2+15) in One

Engine Inoperative case (OEI)• Maximum pitch attitude of 18 ° (22.5 ° in case of windshear)




• Pitch required to climb a 120 ft/min minimum vertical speed.

This explains why, during takeoff, the IAS which is actually flown in most cases is neither V2+10 (AEO)nor V2 (OEI).

LATERAL PROFILEIdent.: NO-050-00005486.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Under most circumstances, the crew can expect to follow the programmed SID. In this case, NAV isarmed on selecting the thrust levers to the applicable detent for take-off and engages once above 30 ftRA.

THRUST REDUCTION ALTITUDEIdent.: NO-050-00005487.0001001 / 28 MAY 08Criteria: SA�Applicable to: ALL

At the thrust reduction altitude, "LVR CLB" flashes on the FMA. When manual flying, lower slightly thenose, as applicable, to anticipate the pitch down FD order. Bring the thrust levers back to CLB detent.The A/THR is now active (A/THR on the FMA changes from blue to white).The FD pitch down order depends upon the amount of thrust decrease between TOGA or FLX andCLB.If takeoff was performed packs OFF, the packs will be selected back to ON after thrust reductionbecause of the potential resulting EGT increase. They will be preferably selected sequentially toimprove passenger's comfort.

ACCELERATION ALTITUDEIdent.: NO-050-00005488.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

At the acceleration altitude, the FD pitch mode changes from SRS to CLB or OP CLB mode. Thespeed target jumps:• Either to the managed target speed e.g. speed constraint, speed limit or ECON climb speed• Or to the preselected climb speed (entered by the pilot on the MCDU PERF CLB page before

takeoff).

If green dot speed is higher than the managed target speed (e.g. speed constraint 220 kt) displayedby the magenta triangle on the PFD speed scale, the AP/FD will guide the aircraft to green dot (as perthe general managed speed guidance rule). If required by ATC, the crew will select the adequate targetspeed (below green dot) on the FCU.




During takeoff phase, F and S speeds are the minimum speeds for retracting the surfaces:• At F speed, the aircraft accelerating (positive speed trend): retract to 1.• At S speed, the aircraft accelerating (positive speed trend): retract to 0.

If the engine start selector had been selected to IGN START for take-off, the PNF should confirm withthe PF when it may be deselected.

TAKE-OFF AT HEAVY WEIGHTIdent.: NO-050-00005489.0001001 / 25 APR 08Criteria: SA�Applicable to: ALL

If take-off is carried out at heavy weight, two protections may intervene:• The Automatic Retraction System (ARS)• The Alpha Lock function

THE AUTOMATIC RETRACTION SYSTEM

While in CONF 1+F and IAS reaches 210 kt (VFE CONF1+F is 215 kt), the ARS is activated. TheARS automatically retracts flaps to 0 °. The VFE displayed on the PFD change from VFE CONF1+Fto VFE CONF 1. As the aircraft accelerates above S speed, the flap lever can be selected to 0. If IASdecreases below VFE CONF1+F, the flaps will not extend back to 1+F.

THE ALPHA LOCK FUNCTION

The slats alpha/speed lock function will prevent slat retraction at high AOA or low speed at themoment the flap lever is moved from Flaps 1 to Flaps 0. "A. LOCK" pulses above the E/WD Slatindication. The inhibition is removed and the slats retract when both alpha and speed fall withinnormal values. This is a normal situation for take-off at heavy weight. If Alpha lock function istriggered, the crew will continue the scheduled acceleration, allowing further slats retraction.

IMMEDIATE TURN AFTER TAKE-OFFIdent.: NO-050-00005490.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Obstacle clearance, noise abatement, or departure procedures may require an immediate turn aftertake-off. Provided FD commands are followed accurately, the flaps and slats may be retracted usingthe normal procedure as FD orders provide bank angle limits with respect to speed and configuration.




LOW ALTITUDE LEVEL-OFFIdent.: NO-050-00005491.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

If the aircraft is required to level off below the acceleration altitude, ALT* engages and target speedgoes to initial climb speed. The "LVR CLB" message flashes on the FMA. In this case, the crew shouldexpect a faster than normal acceleration, and be prepared to retract the flaps and slats promptly.

NOISE ABATEMENT TAKE-OFFIdent.: NO-050-00005492.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Noise Abatement Procedures will not be conducted in conditions of significant turbulence or windshear.




noise abatement procedure


NORMAL OPERATIONSCLIMB


GENERALIdent.: NO-060-00005493.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

During the climb, the thrust levers are in the CL detent, the A/THR is active in thrust mode and theFADECs manage the thrust to a maximum value depending upon ambient conditions.

AP/FD CLIMB MODESIdent.: NO-060-00005494.0001001 / 26 MAR 08Criteria: P4320, P5983, SA�

1 Applicable to: MSN 0029, 0035-0039, 0042-0043, 0045-0059, 0064-0068, 0073-0077, 0080-0082, 0084-0085, 0087-0091, 0095-0099, 0103,0109, 0112-0114, 0119-0120, 0122-0124, 0126-0127, 0132, 0134, 0136, 0138-0143, 0146, 0148-0151, 0154, 0157-0159, 0163-0164, 0167-0170,0173-0177, 0179-0183, 0185, 0189-0191, 0193, 0195-0196, 0199, 0204-0205, 0207, 0210-0212, 0219, 0221-0225, 0229-0234, 0240-0243,0245-0257, 0259-0261, 0264-0266, 0274-0277, 0279-0280, 0283-0284, 0288-0296, 0299-0305, 0308-0317, 0320-0328, 0330-0336, 0338,0341-0345, 0347-0350, 0353-0354, 0356-0357, 0359, 0361-0365, 0368-0371, 0373-0376, 0378-0379, 0383-0386, 0389-0398, 0402-0407,0409, 0411, 0413-0416, 0419-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0490, 0492, 0496-0497,0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0534, 0537-0540, 0542-0543, 0546, 0549, 0551-0552,0554-0555, 0557-0558, 0561, 0565, 0568-0572, 0575, 0579-0582, 0584, 0587, 0589-0592, 0594, 0597, 0601, 0604-0607, 0611, 0613-0615,0617, 0619-0620, 0622, 0624, 0626, 0628, 0630-0634, 0638-0639, 0645, 0648-0650, 0655-0656, 0658-0659, 0661-0662, 0666-0667,0669-0672, 0675, 0677-0678, 0682-0683, 0685, 0688, 0691, 0693, 0695, 0697, 0702, 0711, 0714, 0719, 0721, 0726, 0728, 0731-0732,0736, 0739-0740, 0742-0743, 0746, 0751-0752, 0756-0759, 0762, 0768-0770, 0773, 0775-0776, 0779-0781, 0784-0785, 0787, 0791-0792,0795, 0797, 0800, 0802-0803, 0805, 0808, 0811-0814, 0816-0817, 0820, 0822-0824, 0826, 0829, 0831, 0834, 0836, 0839-0840, 0842, 0845,0851-0852, 0856-0857, 0865-0866, 0869, 0877, 0880, 0888, 0963, 1008, 1042, 1204, 1227

The AP/FD climb modes may be either• Managed• Selected

MANAGED

The managed AP/FD mode in climb is CLB. Its use is recommended as long as the aircraft iscleared along the F-PLN.

SELECTED

The selected AP/FD modes in climb are OP CLB, V/S and EXPED .OP CLB is to be used if ATC gives radar vector or clears the aircraft direct to a given FL without anyclimb constraints.The use of low values of V/S, e.g. less than 1 000 ft/min, may be appropriate for small altitudechanges as it makes the guidance smoother and needs less thrust variation.In areas of high traffic density, low values of vertical speed will reduce the possibility of nuisanceTCAS warnings.If the crew selects a high V/S, it may happen that the aircraft is unable to climb with this high V/Sand to maintain the target speed with Max Climb thrust, for performance reasons. In that case, theAP/FD will guide to the target V/S, and the A/THR will command up to Max Climb thrust, in order to




try to keep the target speed; but the aircraft will decelerate and its speed might reach VLS. WhenVLS is reached the AP/FD reverts to OP CLB and the aircraft accelerate to initial target speed.Whenever V/S is used, pilots should pay particular attention to the speed trend as V/S takesprecedence over speed requirements.The EXPED mode is used to climb with maximum vertical gradient i.e. the target speedbecomes green dot. Its use should be avoided above FL 250.The crew should be aware that altitude constraints in the MCDU F-PLN page are observed onlywhen the climb is managed, i.e. when CLB is displayed on the FMA. Any other vertical mode willdisregard any altitude constraints.A likely scenario would be, when the FCU altitude is set above an altitude constraint and the pilotselects V/S when below that constraint to avoid a potential TCAS TA. In this case, the aircraft willdisregard the altitude constraint.

Ident.: NO-060-00005494.0002001 / 26 MAR 08Criteria: 22-1072, P4320, SA�

2 Applicable to: MSN 0031, 0034, 0040-0041, 0069-0072, 0078, 0083, 0086, 0093-0094, 0104, 0110-0111, 0116-0118, 0121, 0125, 0135,0137, 0147, 0152-0153, 0160-0162, 0165-0166, 0171-0172, 0178, 0192, 0194, 0197-0198, 0200-0202, 0206, 0208-0209, 0213, 0216-0218,0258, 0262-0263, 0267-0269, 0272-0273, 0281-0282, 0297-0298, 0306-0307, 0318-0319, 0329, 0339-0340, 0346, 0351, 0355, 0358, 0360,0366-0367, 0372, 0380-0382, 0387-0388, 0399-0401, 0408, 0410, 0412, 0417-0418, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488,0493-0495, 0502, 0505, 0513-0520, 0522, 0524, 0526, 0532-0533, 0535, 0541, 0545, 0548, 0550, 0553, 0556, 0559-0560, 0562-0564,0566-0567, 0573-0574, 0576-0578, 0583, 0585-0586, 0588, 0593, 0595-0596, 0599, 0603, 0609-0610, 0612, 0616, 0621, 0623, 0627, 0629,0635-0636, 0640-0643, 0646, 0651-0654, 0657, 0663-0665, 0668, 0673-0674, 0676, 0679-0681, 0684, 0686-0687, 0689-0690, 0692, 0694,0696, 0698-0701, 0703-0710, 0712-0713, 0715-0718, 0720, 0722-0725, 0727, 0729-0730, 0733-0735, 0737-0738, 0741, 0744-0745, 0747-0750,0754-0755, 0760-0761, 0763-0767, 0771-0772, 0774, 0778, 0782-0783, 0786, 0788-0790, 0793-0794, 0798-0799, 0801, 0804, 0806-0807,0809-0810, 0815, 0818-0819, 0821, 0825, 0827-0828, 0830, 0832-0833, 0835, 0837-0838, 0841, 0843-0844, 0846-0850, 0853-0855,0858-0864, 0867-0868, 0870-0876, 0878-0879, 0881-0887, 0889-0937, 0939-0962, 0964-0984, 0986-0997, 0999, 1001-1007, 1009-1019,1021-1024, 1026-1035, 1037-1041, 1043-1132, 1134-1136, 1138-1149, 1152-1188, 1191-1200, 1202-1203, 1205-1215, 1217-1226, 1228-1266,1268-1270, 1272-1298, 1300-1343, 1345-1386, 1388-1403, 1405-1414, 1416-1443, 1445-1448, 1450-1457, 1459-1470, 1472-1475, 1477,1479-1501, 1503-1504, 1506-1523, 1525-1598, 1600-1615, 1617-1621, 1623-1639, 1641-1644, 1646-1657, 1659, 1661-1676, 1678-1690,1692-1698, 1700-1732, 1734-1793, 1795-1858, 1860-1872, 1874-1877, 1880-1884, 1886-1893, 1895-1899, 1901-1923, 1925-1927, 1929-1937,1940-1948, 1950, 1954-1955, 1957-1966, 1968-1976, 1978-1990, 1993-2014, 2016, 2018, 2020, 2022, 2027, 2029, 2031, 2034, 2036, 2038,2040, 2042, 2044, 2046, 2048-2049, 2054, 2056, 2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2104, 2137, 2143, 2157, 2225, 2242, 2248,2252, 2311, 2381, 2391, 2472, 2488, 2563, 2599


MANAGED


SELECTED

The selected AP/FD modes in climb are OP CLB, V/S and EXPED .OP CLB is to be used if ATC gives radar vector or clears the aircraft direct to a given FL without anyclimb constraints.




The use of low values of V/S, e.g. less than 1 000 ft/min, may be appropriate for small altitudechanges as it makes the guidance smoother and needs less thrust variation.In areas of high traffic density, low values of vertical speed will reduce the possibility of nuisanceTCAS warnings.If the crew selects a high V/S, it may happen that the aircraft is unable to climb with this high V/Sand to maintain the target speed with Max Climb thrust, for performance reasons. In that case, theAP/FD will guide to the target V/S, and the A/THR will command up to Max Climb thrust, in order totry to keep the target speed; but the aircraft will decelerate and its speed might reach VLS. WhenVLS is reached the AP will pitch the aircraft down so as to fly a V/S, which allows maintaining VLS.Whenever V/S is used, pilots should pay particular attention to the speed trend as V/S takesprecedence over speed requirements.The EXPED mode is used to climb with maximum vertical gradient i.e. the target speedbecomes green dot. Its use should be avoided above FL 250.The crew should be aware that altitude constraints in the MCDU F-PLN page are observed onlywhen the climb is managed, i.e. when CLB is displayed on the FMA. Any other vertical mode willdisregard any altitude constraints.A likely scenario would be, when the FCU altitude is set above an altitude constraint and the pilotselects V/S when below that constraint to avoid a potential TCAS TA. In this case, the aircraft willdisregard the altitude constraint.

Ident.: NO-060-00005494.0005001 / 26 MAR 08Criteria: 22-1072, 22-1123, P4320, P7790, SA�

3 Applicable to: MSN 0002, 0005-0014, 0019-0020, 0044, 0061-0063, 0100-0101, 0108, 0128-0131, 0133, 0144-0145, 0155-0156, 0184,0186-0188, 0214, 0226-0228, 0235-0236, 0239, 0270, 0278, 0285-0287, 0337, 0352, 0377, 0491, 0498, 0509, 0521, 0529, 0544, 0598,0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0777, 0796, 0938, 0985, 0998, 1000, 1020, 1025, 1036, 1133, 1137, 1150-1151, 1189-1190,1201, 1216, 1267, 1271, 1299, 1344, 1387, 1404, 1415, 1444, 1449, 1458, 1471, 1476, 1478, 1502, 1505, 1524, 1599, 1616, 1622, 1640, 1645,1658, 1660, 1677, 1691, 1699, 1733, 1794, 1859, 1873, 1878-1879, 1885, 1894, 1900, 1924, 1928, 1938-1939, 1949, 1951-1953, 1956, 1967,1977, 1991, 2015, 2017, 2019, 2021, 2023-2026, 2028, 2030, 2032-2033, 2035, 2037, 2039, 2041, 2043, 2045, 2047, 2050-2053, 2055, 2057,2059-2060, 2062, 2064, 2066-2067, 2069, 2071-2072, 2074, 2076-2103, 2105-2136, 2138-2142, 2144-2156, 2158-2224, 2226-2241, 2243-2247,2249-2251, 2253-2310, 2312-2380, 2382-2390, 2392-2471, 2473-2487, 2489-2562, 2564-2598, 2600-3996


MANAGED


SELECTED

The selected AP/FD modes in climb are OP CLB, V/S and EXPED .OP CLB is to be used if ATC gives radar vector or clears the aircraft direct to a given FL without anyclimb constraints.




The use of low values of V/S, e.g. less than 1 000 ft/min, may be appropriate for small altitudechanges as it makes the guidance smoother and needs less thrust variation.In areas of high traffic density, low values of vertical speed will reduce the possibility of nuisanceTCAS warnings.If the crew selects a high V/S, it may happen that the aircraft is unable to climb with this high V/Sand to maintain the target speed with Max Climb thrust, for performance reasons. In that case, theAP/FD will guide to the target V/S, and the A/THR will command up to Max Climb thrust, in order totry to keep the target speed; but the aircraft will decelerate and its speed might reach VLS. WhenVLS is reached the AP will pitch the aircraft down so as to fly a V/S, which allows maintaining VLS.A triple click is generated.Whenever V/S is used, pilots should pay particular attention to the speed trend as V/S takesprecedence over speed requirements.The EXPED mode is used to climb with maximum vertical gradient i.e. the target speedbecomes green dot. Its use should be avoided above FL 250.The crew should be aware that altitude constraints in the MCDU F-PLN page are observed onlywhen the climb is managed, i.e. when CLB is displayed on the FMA. Any other vertical mode willdisregard any altitude constraints.A likely scenario would be, when the FCU altitude is set above an altitude constraint and the pilotselects V/S when below that constraint to avoid a potential TCAS TA. In this case, the aircraft willdisregard the altitude constraint.

Ident.: NO-060-00005494.0004001 / 16 JUN 08Criteria: 22-1123, SA�

4 Applicable to: MSN 0003, 0016, 0021, 0033, 0102, 0115, 0203, 0215, 0220, 0237, 0244


MANAGED


SELECTED

The selected AP/FD modes in climb are OP CLB, V/S and EXPED .OP CLB is to be used if ATC gives radar vector or clears the aircraft direct to a given FL without anyclimb constraints.The use of low values of V/S, e.g. less than 1 000 ft/min, may be appropriate for small altitudechanges as it makes the guidance smoother and needs less thrust variation.In areas of high traffic density, low values of vertical speed will reduce the possibility of nuisanceTCAS warnings.




If the crew selects a high V/S, it may happen that the aircraft is unable to climb with this high V/Sand to maintain the target speed with Max Climb thrust, for performance reasons. In that case, theAP/FD will guide to the target V/S, and the A/THR will command up to Max Climb thrust, in order totry to keep the target speed; but the aircraft will decelerate and its speed might reach VLS. WhenVLS is reached the AP/FD reverts to OP CLB and the aircraft accelerate to initial target speed. Atriple click is generated.Whenever V/S is used, pilots should pay particular attention to the speed trend as V/S takesprecedence over speed requirements.The EXPED mode is used to climb with maximum vertical gradient i.e. the target speedbecomes green dot. Its use should be avoided above FL 250.The crew should be aware that altitude constraints in the MCDU F-PLN page are observed onlywhen the climb is managed, i.e. when CLB is displayed on the FMA. Any other vertical mode willdisregard any altitude constraints.A likely scenario would be, when the FCU altitude is set above an altitude constraint and the pilotselects V/S when below that constraint to avoid a potential TCAS TA. In this case, the aircraft willdisregard the altitude constraint.

SPEED CONSIDERATIONSIdent.: NO-060-00005495.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The climb speed may be either:• Managed• Selected

MANAGED

The managed climb speed, computed by the FMGS, provides the most economical climb profileas it takes into account weight, actual and predicted winds, ISA deviation and Cost Index (CI). Themanaged climb speed also takes into account any speed constraints, e.g. the default speed limitwhich is 250 kt up to 10 000 ft.

SELECTED

If necessary, the climb speed can be either pre-selected on ground prior to take-off on the MCDUPERF CLIMB page or selected on the FCU as required.On ground, prior take-off, speed target at acceleration altitude can be pre-selected on the MCDUPERF CLIMB page. It is to be used when the F-PLN has a sharp turn after take-off, when high angleof climb is required or for ATC clearance compliance.Once airborne, the speed can be selected on FCU to achieve the maximum rate of climb or themaximum gradient of climb.




The speed to achieve the maximum rate of climb, i.e. to reach a given altitude in the shortest time,lies between ECON climb speed and green dot. As there is no indication of this speed on the PFD, agood rule of thumb is to use turbulence speed to achieve maximum rate.The speed to achieve the maximum gradient of climb, i.e. to reach a given altitude in a shortestdistance, is green dot. The MCDU PERF CLB page displays the time and distance required toachieve the selected altitude by climbing at green dot speed. Avoid reducing to green dot at highaltitude, particularly at heavy weight, as it can take a long time to accelerate to ECON mach.Pilots should be aware that it is possible to select and fly a speed below green dot but there wouldbe no operational benefit in doing this.When selected speed is used, the predictions on the F-PLN page assume the selected speedis kept till the next planned speed modification, e.g. 250 kt /10 000 ft, where managed speed issupposed to be resumed. Consequently, the FM predictions remain meaningful.When IAS is selected in lower altitude, there is an automatic change to Mach at a specific crossoveraltitude.Finally, as selected speed does not provide the optimum climb profile, it should only be used whenoperationally required, e.g. ATC constraint or weather.

VERTICAL PERFORMANCE PREDICTIONSIdent.: NO-060-00005496.0001001 / 27 MAY 08Criteria: SA�Applicable to: ALL

The MCDU PROG page provides the crew with the MAX REC ALT and with the OPT ALT information(See cruise section). This information is to be used to rapidly answer to ATC: "CAN YOU CLIMB TO FLXXX?"The MCDU PERF CLB page provides predictions to a given FL in terms of time and distance assumingCLB mode. This FL is defaulted to the FCU target altitude or it may be manually inserted. The levelarrow on the ND assumes the current AP engaged mode. This information is to be used to rapidlyanswer to ATC: "CAN YOU MAKE FL XXX by ZZZ waypoint?". The crew will use a PD (Place/Distance), i.e. ZZZ,-10 waypoint if the question is "CAN YOU MAKE FL XXX , 10 nm before ZZZpoint?"

LATERAL NAVIGATIONIdent.: NO-060-00005497.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

If the aircraft is following the programmed SID, the AP/FD should be in NAV. If ATC vectors the aircraft,HDG will be used until a time when clearance is given to either resume the SID or track direct to aspecific waypoint. In either case, the crew must ensure that the waypoints are properly sequenced.




The crew should keep in mind that the use of HDG mode e.g. following ATC radar vectors, will revertCLB to OP CLB and any altitude constraints in the MCDU F-PLN page will not be observed unlessthey are selected on the FCU.

10 000 FT FLOW PATTERNIdent.: NO-060-00005498.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

10 000 ft FLOW PATTERN

EFIS Option:The PF will select CSTR for grid MORAThe PNF will select ARPT


NORMAL OPERATIONSCRUISE


PREFACEIdent.: NO-070-00005499.0001001 / 26 MAR 08Criteria: SA�

1 Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0113-0114, 0163-0166,0168-0169, 0178-0182, 0189-0190, 0193-0195, 0198, 0221, 0225, 0230, 0232, 0243, 0247, 0249-0252, 0256-0257, 0259-0261, 0275-0276,0280, 0289, 0291-0292, 0294-0296, 0304, 0308, 0314, 0316-0317, 0320-0322, 0326-0327, 0332, 0334-0336, 0338, 0343, 0347, 0349,0351, 0353-0354, 0357, 0361-0363, 0366, 0368-0369, 0371, 0373, 0376, 0379, 0386, 0391-0394, 0396-0398, 0405-0406, 0411, 0414-0416,0422-0425, 0428-0432, 0437, 0440-0441, 0443-0444, 0446-0449, 0451, 0453, 0455, 0461, 0467, 0469, 0471, 0476, 0478, 0480

Once the cruise flight level displayed on the MCDU PROG page is reached, the cruise Mach number istargeted and cruise fuel consumption is optimized.


2 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112, 0115-0162, 0167,0170-0177, 0183-0188, 0191-0192, 0196-0197, 0199-0220, 0222-0224, 0226-0229, 0231, 0233-0242, 0244-0246, 0248, 0253-0255, 0258,0262-0274, 0277-0279, 0281-0288, 0290, 0293, 0297-0303, 0305-0307, 0309-0313, 0315, 0318-0319, 0323-0325, 0328-0331, 0333, 0337,0339-0342, 0344-0346, 0348, 0350, 0352, 0355-0356, 0358-0360, 0364-0365, 0367, 0370, 0372, 0375, 0377-0378, 0380-0385, 0387-0390,0395, 0399-0404, 0407-0410, 0412-0413, 0417-0421, 0426-0427, 0434-0436, 0438-0439, 0442, 0445, 0450, 0452, 0454, 0456-0460,0462-0466, 0468, 0470, 0472-0475, 0477, 0479, 0482-3996

Once the cruise flight level is reached, "ALT CRZ" is displayed on the FMA. The cruise Mach number istargeted and cruise fuel consumption is optimized.




FMS USEIdent.: NO-070-00005500.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


CRUISE FL

If the aircraft is cleared to a lower cruise flight level than the pre-planned cruise flight level displayedon MCDU PROG page, the cruise Mach number will not be targeted. The crew will update theMCDU PROG page accordingly.When at cruise FL, the AP altitude control is soft. This means that the AP will allow small altitudevariation around the cruise altitude (typically ± 50 ft) to keep cruise Mach before a readjustment ofthrust occurs. This optimizes the fuel consumption in cruise.

WIND AND TEMPERATURE

When reaching cruise FL, the crew will ensure that the wind and temperatures are correctly enteredand the lateral and vertical F-PLN reflect the CFP. Wind entries should be made at waypoints whenthere is a difference of either 30 ° or 30 kt for the wind data and 5 °C for temperature deviation. Thiswill ensure that the FMS fuel and time predictions are as accurate as possible.




Ident.: NO-070-00005500.0002001 / 26 MAY 08Criteria: 22-1089, 22-1090, 22-1103, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1163, 22-1176, 22-1180, 22-1193, 22-1197,22-1209, 22-1217, 22-1218, 22-1219, 22-1233, 22-1235, 22-1240, P7372, P7373, P7519, P7520, P7666, P7706, P7707, SA�


CRUISE FL

If the aircraft is cleared to a lower cruise flight level than the pre-planned cruise flight level displayedon MCDU PROG page, the cruise Mach number will not be targeted. The crew will update theMCDU PROG page accordingly.When at cruise FL, the AP altitude control is soft. This means that the AP will allow small altitudevariation around the cruise altitude (typically ± 50 ft) to keep cruise Mach before a readjustment ofthrust occurs. This optimizes the fuel consumption in cruise.

WIND AND TEMPERATURE

When reaching cruise FL, the crew will ensure that the wind and temperatures are correctly enteredand the lateral and vertical F-PLN reflect the CFP. Wind entries should be made at waypoints whenthere is a difference of either 30 ° or 30 kt for the wind data and 5 °C for temperature deviation.These entries should be made for as many levels as possible to reflect the actual wind andtemperature profile. This will ensure that the FMS fuel and time predictions are as accurate aspossible and provide an accurate OPT FL computation.

STEP CLIMB

If there is a STEP in the F-PLN, the crew will ensure that the wind is properly set at the first waypointbeyond the step (D on the following example) at both initial FL and step FL.




If at D waypoint, the CFP provides the wind at FL 350 but not at FL 310, it is recommended to insertthe same wind at FL 310 as the one at FL 350. This is due to wind propagation rules, which mightaffect the optimum FL computation.

ETP

ETP function should be used to assist the crew in making a decision should an en-route diversion berequired. Suitable airport pairs should be entered on the ETP page and the FMS will then calculatethe ETP. Each time an ETP is sequenced, the crew should insert the next suitable diversion airfield.

The SEC F-PLN is a useful tool and should be used practically. The ETP should be inserted in theSEC F-PLN as a PD (Place/Distance) and the route to diversion airfield should be finalized. Byprogramming a potential en-route diversion, the crew would reduce their workload should a failureoccur. This is particularly true when terrain considerations apply to the intended diversion route.When an ETP is sequenced, the crew will• Access the ETP page• Insert the next applicable diversion airfield with associated wind• Read new ETP• Insert new ETP as a PD• Copy active on the SEC F-PLN• Insert the new diversion as New Dest in the SEC F-PLN from new ETP




The DATA/Stored Routes function in the MCDU can be used to store up to five possible diversionroutes. These routes can be entered into the SEC F-PLN using the SEC INIT prompt. This promptwill only be available if the SEC F-PLN is deleted. Refer to FCOM/DSC-22_20-60-40 USING THESECONDARY FLIGHT PLAN FUNCTION for further information.

CLOSEST AIRPORT

For diversion purpose, the crew can also use the CLOSEST AIRPORT page which providesvaluable fuel/time estimates to the four closest airports from the aircraft position, as well as toan airport the crew may define. The fuel and time predictions are a function of the average windbetween the aircraft and the airport.




FMS USE: MISCELLANEOUSIdent.: NO-070-00005501.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


If ATC modifies the routing, the crew will revise the F-PLN. Once achieved and if printer is installed, thecrew may perform a new F-PLN print.If there is weather, the crew will use the OFFSET function which can be accessed from a lateralrevision at PPOS. The crew will determine how many NM are required to avoid the weather. Oncecleared by ATC, the crew will insert the offset.




Ident.: NO-070-00005501.0002001 / 26 MAY 08Criteria: 22-1089, 22-1090, 22-1163, 22-1233, 22-1235, P7519, P7520, SA�

6 Applicable to: MSN 0134, 0136, 0143, 0146, 0158, 0173, 0176-0177, 0196, 0199, 0207, 0219, 0223-0224, 0240-0241, 0264, 0274, 0300, 0312,0323, 0328, 0365, 0383, 0501, 0507, 0531, 0658, 0669, 0685, 0910, 0913, 0941, 0961, 0976, 0992, 1002, 1010, 1021, 1027, 1047, 1053, 1059,1066-1067, 1073, 1087, 1092, 1096, 1099, 1101, 1103, 1107, 1113, 1119, 1123, 1125, 1130, 1137, 1139-1140, 1143, 1150, 1152, 1156-1159, 1173,1179, 1183-1185, 1188-1189, 1195, 1198, 1200, 1208, 1212-1213, 1219, 1221, 1229, 1233, 1235, 1238, 1240-1242, 1244, 1246, 1250-1251, 1253,1255-1257, 1259, 1262, 1270, 1276, 1280, 1285, 1288, 1292, 1300, 1302-1304, 1306, 1308-1309, 1318, 1320, 1322, 1327, 1332-1335, 1339,1349, 1351-1353, 1355, 1364-1368, 1376-1377, 1381, 1383, 1385-1387, 1390, 1394, 1396, 1398, 1400, 1402, 1405, 1407-1408, 1411, 1413,1416, 1429-1430, 1437-1438, 1441, 1443, 1446, 1451-1452, 1454, 1458, 1461, 1464, 1467-1468, 1470, 1478, 1482, 1484-1486, 1491, 1493,1497, 1503-1504, 1506, 1509, 1512, 1516, 1518, 1523, 1526, 1528, 1530, 1540-1541, 1544, 1546, 1548, 1550-1551, 1553-1554, 1556-1557,1562, 1564, 1568, 1571-1572, 1575, 1577-1578, 1580, 1587-1589, 1591-1593, 1595-1599, 1601-1603, 1605, 1607-1608, 1610-1615, 1618-1619,1623-1626, 1628-1632, 1634, 1637-1638, 1642, 1650, 1652, 1657, 1663, 1668, 1672-1673, 1675-1676, 1678, 1682, 1686, 1695, 1703,1705-1707, 1712, 1717-1721, 1725-1727, 1730, 1735, 1739, 1742, 1747-1751, 1756-1757, 1762-1763, 1765, 1767, 1769, 1771-1772, 1775-1778,1780, 1783-1788, 1791, 1794-1795, 1797-1798, 1801-1802, 1804-1808, 1811, 1817-1818, 1823, 1825-1827, 1831-1832, 1835, 1837-1838, 1843,1846, 1848-1849, 1852, 1854-1858, 1860-1862, 1864, 1866-1868, 1872, 1874, 1877-1878, 1880-1882, 1886-1889, 1891, 1896, 1898, 1903-1906,1908-1909, 1911, 1913-1917, 1920-1921, 1925, 1927, 1929-1934, 1936-1937, 1940-1942, 1944-1948, 1950-1956, 1960-1961, 1964-1968,1970-1975, 1977-1979, 1981, 1983-1986, 1988-1989, 1994-1995, 1998-2001, 2003-2009, 2011, 2014-2015, 2018, 2020-2022, 2024, 2027,2031, 2034, 2036-2037, 2042-2044, 2046, 2048-2050, 2052-2056, 2060-2063, 2065-2069, 2072, 2075, 2078, 2080, 2084-2085, 2089-2091,2093, 2096, 2099, 2102, 2105-2106, 2108, 2112, 2114, 2116-2120, 2123-2126, 2128-2134, 2136, 2141, 2144-2155, 2159-2160, 2162-2163, 2165,2167-2185, 2187, 2191-2192, 2196-2197, 2199-2203, 2205-2206, 2208, 2210, 2212, 2214-2215, 2217, 2219-2225, 2227, 2229-2235, 2237-2239,2242-2246, 2248-2251, 2256-2257, 2259, 2262-2266, 2268-2275, 2280-2286, 2289, 2292-2295, 2297-2301, 2304, 2307-2309, 2311, 2314-2316,2319, 2321-2322, 2325-2330, 2333-2334, 2336-2339, 2342-2343, 2345, 2347, 2352-2358, 2360-2361, 2364-2365, 2367-2368, 2370-2372,2374-2375, 2377-2381, 2384-2388, 2391, 2393-2395, 2398-2399, 2401-2403, 2407-2409, 2411-2413, 2415-2416, 2418-2421, 2423-2424,2426-2428, 2432-2440, 2442-2447, 2449-2451, 2453-2455, 2457, 2460-2461, 2463, 2469-2473, 2475-2479, 2481, 2484-2496, 2498-2508,2511-2516, 2519-2523, 2525-2528, 2530-2533, 2535, 2537-2538, 2540-2556, 2558-2560, 2562-2563, 2565, 2567, 2569, 2571-2580,2583-2592, 2594, 2596, 2598-2600, 2602-2606, 2608-2610, 2614, 2616, 2620-2623, 2625-2627, 2634-2638, 2640, 2642-2643, 2646-2647,2649-2652, 2657-2659, 2661, 2663-2664, 2666-2667, 2670-2671, 2673-2675, 2677-2681, 2687-2689, 2691-2693, 2695, 2698, 2701-2704,2708-2711, 2713-2715, 2717-2719, 2723-2725, 2727-2730, 2734-2737, 2740-2745, 2748, 2752, 2754-2759, 2761, 2765-2767, 2769-2773,2776-2798, 2800-2805, 2807, 2809-2812, 2814-2815, 2817-2819, 2821-2825, 2827, 2829-2832, 2834, 2843, 2845, 2847-2848, 2850-2852,2854-2856, 2858-2862, 2864, 2866, 2868, 2870-2873, 2875-2877, 2880, 2884, 2886-2890, 2892-2894, 2896-2901, 2903-2904, 2906, 2912,2915-2917, 2919-2921, 2923-2924, 2927-2929, 2933-2934, 2936, 2940-2942, 2945-2950, 2952-2953, 2957, 2959-2960, 2962-2963, 2965,2969-2971, 2977-2979, 2982-2984, 2986-2988, 2992-2994, 2996, 2998-2999, 3002-3003, 3007, 3010, 3015-3017, 3020, 3025-3026, 3029,3031-3032, 3034-3037, 3039-3043, 3045, 3047-3048, 3052-3054, 3057-3061, 3063, 3067, 3069, 3072-3073, 3075, 3077-3078, 3082-3085,3088-3091, 3094-3095, 3097, 3099, 3101-3103, 3105, 3109, 3111-3113, 3118-3120, 3122-3123, 3125-3127, 3129, 3133-3137, 3141, 3143-3145,3147-3148, 3150-3152, 3155-3157, 3165-3166, 3168-3169, 3174-3177, 3179-3181, 3184-3186, 3189-3191, 3195, 3200, 3203-3204, 3207-3209,3211, 3217, 3222, 3226, 3228-3231, 3237, 3239-3241, 3246, 3248, 3250-3251, 3253, 3255, 3257-3258, 3263, 3266-3267, 3269-3270,3272, 3275-3276, 3278-3281, 3283-3284, 3287, 3292-3294, 3296, 3298, 3302-3304, 3311, 3313, 3318-3322, 3324-3325, 3332-3334, 3336,3341-3342, 3345, 3347-3350, 3354, 3359, 3361, 3373-3374, 3376-3378, 3380-3381, 3384, 3391, 3393, 3395-3396, 3398, 3400, 3405-3406,3408-3411, 3413, 3416-3418, 3425-3426, 3428-3430, 3432-3433, 3436, 3442-3443, 3445, 3450-3452, 3458-3460, 3463, 3465-3467, 3472,3474-3475, 3479, 3487-3488, 3491, 3493, 3495, 3501, 3503, 3507, 3510-3511, 3513, 3517-3518, 3522, 3525, 3529, 3531, 3535, 3537-3540,3542, 3544-3545, 3547, 3552, 3554-3556, 3558, 3562, 3565-3567, 3569, 3571-3572, 3574, 3577, 3581, 3587-3588, 3590, 3594-3595, 3603,3608, 3617, 3622, 3624, 3627, 3630-3632, 3634, 3637, 3640, 3644-3647, 3651, 3654, 3656, 3658-3660, 3662-3664, 3668, 3670-3675, 3681,3683-3686, 3688, 3691, 3693, 3699, 3702, 3705, 3707, 3710-3711, 3713, 3717-3720, 3724, 3727, 3733-3736, 3738, 3741-3744, 3746-3748,3750, 3754-3755, 3757, 3760-3764, 3767, 3770-3772, 3774, 3778-3781, 3783-3784, 3786-3790, 3794, 3799-3801, 3803-3805, 3807-3808,3810-3812, 3816-3817, 3823-3824, 3832, 3835, 3843-3845, 3847, 3854, 3860-3861, 3867-3871, 3888-3890, 3892, 2706, 2837-2839, 3819,3826, 3837-3838, 3856-3857, 3877, 3882, 3894, 3899, 3902, 3905, 3908-3910, 3913, 3916-3917, 3919-3920, 3922-3923, 3927, 3933-3934,3938-3939, 3941, 3946-3948, 3951-3954, 3959, 3968, 3972, 3981

If ATC requires a position report, the crew will use the REPORT page which can be accessed fromPROG page.If ATC modifies the routing, the crew will revise the F-PLN. Once achieved and if printer is installed, thecrew may perform a new F-PLN print.




ATC requires a report on a given radial, the crew will use the FIX INFO page which can be accessedfrom a lateral revision on F-PLN page at PPOS.If ATC requires a report at a given time, the crew will insert a time marker pseudo waypoint.If there is weather, the crew will use the OFFSET function which can be accessed from a lateralrevision at PPOS. The crew will determine how many NM are required to avoid the weather. Oncecleared by ATC, the crew will insert the offset.If ATC gives a DIR TO clearance to a waypoint far from present position, the crew will use the ABEAMfacility. This facility allows both a better crew orientation and the previously entered winds to be stillconsidered.




Ident.: NO-070-00005501.0003001 / 26 MAR 08Criteria: 22-1089, 22-1090, 22-1103, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1176, 22-1180, 22-1193, 22-1197, 22-1209, 22-1217,22-1218, 22-1219, 22-1240, P7372, P7373, P7519, P7520, P7666, P7706, P7707, SA�

7 Applicable to: MSN 0002-0021, 0031-0034, 0040-0041, 0044, 0052-0055, 0061-0067, 0076-0077, 0081-0082, 0091, 0098-0102, 0108, 0112,0115, 0118-0119, 0121, 0123-0125, 0128-0131, 0133, 0144-0145, 0152-0153, 0155-0156, 0160, 0165-0166, 0171, 0178, 0184, 0186-0188,0192, 0194, 0197-0198, 0203-0206, 0208, 0211, 0213-0215, 0220, 0226-0228, 0235-0239, 0244, 0262-0263, 0270-0273, 0278, 0281-0282,0285-0287, 0297-0299, 0306-0307, 0317-0319, 0322, 0329, 0337, 0339-0340, 0351-0352, 0355, 0358, 0360, 0366-0367, 0370, 0372, 0377,0380-0381, 0387-0388, 0390, 0399-0400, 0402, 0408, 0410, 0417-0418, 0448, 0455, 0471, 0491, 0498, 0509, 0511, 0521, 0527, 0529, 0544,0584, 0598, 0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0680, 0687, 0715, 0725, 0764, 0766, 0777-0778, 0786, 0796, 0801-0802,0807, 0818, 0830, 0832, 0844, 0846, 0861, 0863, 0868-0869, 0880, 0885, 0890, 0896, 0903-0904, 0907, 0911, 0922-0923, 0929, 0938,0958, 0962, 0964, 0972, 0975, 0981, 0985, 0988, 0994, 0996-0998, 1000, 1011, 1019-1020, 1025, 1033, 1036-1038, 1040, 1042, 1044,1046, 1048, 1051-1052, 1055, 1058, 1061-1062, 1065, 1069, 1071, 1077-1078, 1080, 1082, 1084, 1089-1091, 1095, 1097, 1102, 1109, 1112,1114-1115, 1118, 1121-1122, 1126, 1129, 1131-1136, 1141-1142, 1147-1149, 1151, 1155, 1160-1162, 1164, 1167, 1169-1170, 1172, 1175-1176,1182, 1187, 1190-1191, 1193-1194, 1197, 1201, 1203-1205, 1214-1216, 1222, 1224-1225, 1227, 1230, 1232, 1236, 1239, 1245, 1249, 1254,1258, 1260-1261, 1264-1265, 1267-1269, 1271, 1273, 1275, 1277-1279, 1283, 1287, 1289, 1294-1295, 1297-1299, 1301, 1305, 1310-1311,1313-1315, 1317, 1319, 1324-1326, 1328-1329, 1331, 1336-1338, 1340, 1342, 1344, 1346, 1348, 1354, 1356, 1358, 1360, 1369, 1371, 1378,1380, 1382, 1384, 1388-1389, 1391-1393, 1403-1404, 1406, 1410, 1412, 1414-1415, 1417, 1419, 1423, 1425, 1428, 1431, 1433-1434, 1436, 1440,1442, 1444-1445, 1447, 1449, 1453, 1455-1456, 1462-1463, 1465-1466, 1471-1472, 1476, 1479, 1481, 1483, 1488, 1490, 1492, 1494, 1496,1498-1502, 1505, 1510-1511, 1513, 1515, 1517, 1519-1521, 1524-1525, 1527, 1529, 1531, 1534-1537, 1539, 1543, 1547, 1549, 1552, 1558, 1560,1563, 1565-1567, 1570, 1574, 1576, 1579, 1582-1583, 1590, 1594, 1604, 1606, 1616, 1621-1622, 1633, 1636, 1640-1641, 1643-1646, 1648,1651, 1656, 1658-1662, 1665-1666, 1670, 1677, 1683-1685, 1687, 1689-1691, 1693, 1696, 1699-1701, 1704, 1708-1711, 1714-1715, 1722-1724,1733-1734, 1738, 1740, 1743-1746, 1752, 1754, 1758-1761, 1764, 1766, 1770, 1773-1774, 1779, 1781-1782, 1789-1790, 1792, 1796, 1800,1803, 1810, 1812-1815, 1819-1820, 1824, 1828-1829, 1833, 1839, 1841, 1844, 1850-1851, 1853, 1859, 1863, 1869-1871, 1873, 1875-1876,1879, 1883-1885, 1890, 1893-1895, 1897, 1899-1901, 1907, 1910, 1912, 1918, 1922-1924, 1926, 1928, 1935, 1938-1939, 1943, 1949,1957-1959, 1962-1963, 1969, 1976, 1980, 1982, 1990-1993, 1996-1997, 2002, 2010, 2012-2013, 2016-2017, 2019, 2023, 2026, 2028-2030,2032-2033, 2035, 2038-2041, 2045, 2047, 2051, 2057, 2059, 2064, 2070-2071, 2073-2074, 2076-2077, 2079, 2081-2083, 2086-2088, 2092,2094-2095, 2097-2098, 2100-2101, 2103, 2107, 2109-2110, 2113, 2121-2122, 2127, 2135, 2137-2140, 2142, 2156-2158, 2161, 2164, 2166, 2186,2188-2190, 2193-2195, 2198, 2204, 2207, 2209, 2211, 2213, 2216, 2218, 2226, 2228, 2236, 2240-2241, 2247, 2253-2255, 2258, 2260-2261,2267, 2276-2279, 2287-2288, 2290-2291, 2296, 2302-2303, 2305-2306, 2310, 2312-2313, 2317-2318, 2320, 2323-2324, 2331-2332, 2335,2340-2341, 2344, 2346, 2348-2351, 2359, 2362-2363, 2366, 2369, 2373, 2376, 2382-2383, 2389-2390, 2392, 2396-2397, 2400, 2404-2406,2410, 2414, 2417, 2422, 2425, 2429-2431, 2441, 2448, 2452, 2456, 2458-2459, 2462, 2464-2468, 2474, 2480, 2482-2483, 2497, 2509-2510,2517-2518, 2524, 2529, 2534, 2536, 2539, 2557, 2561, 2564, 2566, 2568, 2570, 2581-2582, 2593, 2595, 2597, 2601, 2607, 2611-2613,2615, 2617-2619, 2624, 2628-2633, 2639, 2641, 2644-2645, 2648, 2653-2656, 2660, 2662, 2665, 2668-2669, 2672, 2676, 2682-2686,2690, 2694, 2696-2697, 2699-2700, 2705, 2707, 2712, 2716, 2720-2721, 2726, 2731-2733, 2738-2739, 2746-2747, 2749-2751, 2753, 2760,2762-2764, 2768, 2774-2775, 2799, 2806, 2808, 2813, 2816, 2820, 2826, 2828, 2833, 2835-2836, 2840-2842, 2844, 2846, 2849, 2853,2857, 2863, 2865, 2867, 2869, 2874, 2878-2879, 2881-2883, 2885, 2891, 2895, 2902, 2905, 2907-2911, 2913-2914, 2918, 2922, 2925-2926,2930-2932, 2935, 2937-2939, 2943-2944, 2951, 2954-2956, 2958, 2961, 2964, 2966-2968, 2972-2976, 2980-2981, 2985, 2989-2991,2995, 2997, 3000-3001, 3004-3006, 3008-3009, 3011-3014, 3018-3019, 3021-3024, 3027-3028, 3030, 3033, 3038, 3044, 3046, 3049-3051,3055-3056, 3062, 3064-3066, 3068, 3070-3071, 3074, 3076, 3079-3081, 3086-3087, 3092-3093, 3096, 3098, 3100, 3104, 3106-3108, 3110,3114-3117, 3121, 3124, 3128, 3130-3132, 3138-3140, 3142, 3146, 3149, 3153-3154, 3158-3164, 3167, 3170-3173, 3178, 3182-3183, 3187-3188,3192-3194, 3196-3199, 3201-3202, 3205-3206, 3210, 3212-3216, 3218-3221, 3223-3225, 3227, 3232-3236, 3238, 3242-3245, 3247, 3249,3252, 3254, 3256, 3259-3262, 3264-3265, 3268, 3271, 3273-3274, 3277, 3282, 3285-3286, 3288-3291, 3295, 3297, 3299-3301, 3305-3310,3312, 3314-3317, 3323, 3326-3331, 3335, 3337-3340, 3343-3344, 3346, 3351-3353, 3355-3358, 3360, 3362-3372, 3375, 3379, 3382-3383,3385-3390, 3392, 3394, 3397, 3399, 3401-3404, 3407, 3412, 3414-3415, 3419-3424, 3427, 3431, 3434-3435, 3437-3441, 3444, 3446-3449,3453-3457, 3461-3462, 3464, 3468-3471, 3473, 3476-3478, 3480-3486, 3489-3490, 3492, 3494, 3496-3500, 3502, 3504-3506, 3508-3509,3512, 3514-3516, 3519-3521, 3523-3524, 3526-3528, 3530, 3532-3534, 3536, 3541, 3543, 3546, 3548-3551, 3553, 3557, 3559-3561,3563-3564, 3568, 3570, 3573, 3575-3576, 3578-3580, 3582-3586, 3589, 3596-3602, 3604-3607, 3609-3616, 3618-3621, 3623, 3625-3626,3628-3629, 3633, 3635-3636, 3641-3643, 3648-3650, 3652-3653, 3655, 3657, 3661, 3665-3667, 3669, 3676-3680, 3682, 3687, 3689-3690,3692, 3694-3698, 3700-3701, 3703-3704, 3706, 3708-3709, 3712, 3714-3716, 3721-3723, 3725-3726, 3728-3732, 3737, 3739-3740, 3745,3749, 3751-3753, 3756, 3765-3766, 3768-3769, 3773, 3782, 3785, 3791-3793, 3795-3798, 3802, 3806, 3809, 3813-3815, 3820-3822,3839-3841, 3858-3859, 3862-3866, 3878-3881, 3883-3887, 3891, 3903-3904, 3943-3945, 3591-3593, 3638-3639, 3758-3759, 3775-3777, 3818,3825, 3827-3831, 3833-3834, 3836, 3846, 3848-3853, 3855, 3872-3876, 3893, 3895-3898, 3900-3901, 3906-3907, 3911-3912, 3915, 3918,3921, 3924-3926, 3928-3932, 3935-3937, 3940, 3949-3950, 3955-3956, 3960-3967, 3969-3971, 3977, 3983-3996

If ATC modifies the routing, the crew will revise the F-PLN. Once achieved and if printer is installed, thecrew may perform a new F-PLN print.




If there is weather, the crew will use the OFFSET function which can be accessed from a lateralrevision at PPOS. The crew will determine how many NM are required to avoid the weather. Oncecleared by ATC, the crew will insert the offset.If ATC gives a DIR TO clearance to a waypoint far from present position, the crew will use the ABEAMfacility. This facility allows both a better crew orientation and the previously entered winds to be stillconsidered.

COST INDEXIdent.: NO-070-00005502.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The Cost Index (CI) is used to take into account the relationship between fuel and time related costs inorder to minimize the trip cost. The CI is calculated by the airline for each sector. From an operationalpoint of view, the CI affects the speeds (ECON SPEED/MACH) and cruise altitude (OPT ALT). CI=0corresponds to maximum range whereas the CI=999 corresponds to minimum time.The CI is a strategic parameter which applies to the whole flight. However, the CI can be modified bythe crew in flight for valid strategic operational reasons. For example, if the crew needs to reduce thespeed for the entire flight to comply with curfew requirements or fuel management requirements (XTRAgets close to 0), then it is appropriate to reduce the CI.The SEC F-PLN can be used to check the predictions associated with new CI. If they are satisfactory,the crew will then modify the CI in the primary The SEC F-PLN can be used to check the predictionsassociated with new CI. If they are satisfactory, the crew will then modify the CI in the primary F-PLN.However, the crew should be aware that any modification of the CI would affect trip cost. However, thecrew should be aware that any modification of the CI would affect trip cost.




SPEED CONSIDERATIONSIdent.: NO-070-00005503.0001001 / 26 MAR 08Criteria: P3560, P6193, P7519, P7520, P7706, P7707, SA�

8 Applicable to: MSN 0029, 0035-0039, 0042-0043, 0045-0051, 0056-0059, 0068-0075, 0078-0080, 0083-0086, 0089-0090, 0093-0097,0103-0104, 0109-0111, 0113-0114, 0116-0117, 0120, 0122, 0126-0127, 0132, 0135, 0137-0142, 0147-0151, 0154, 0157, 0159, 0161-0164,0167-0170, 0172, 0174-0175, 0179-0183, 0185, 0189-0191, 0193, 0195, 0200-0202, 0209-0210, 0212, 0216-0218, 0221-0222, 0225, 0229-0234,0242-0243, 0245-0261, 0265-0269, 0275-0277, 0279-0280, 0283-0284, 0288-0296, 0301-0305, 0308-0311, 0313-0316, 0320-0321, 0324-0327,0330-0336, 0338, 0341-0350, 0353-0354, 0356-0357, 0359, 0361-0364, 0368-0369, 0371, 0373-0376, 0378-0379, 0382, 0384-0386, 0389,0391-0398, 0401, 0403-0407, 0409, 0411-0416, 0419-0447, 0449-0454, 0456-0470, 0472-0490, 0492-0497, 0499-0500, 0502-0506, 0508, 0510,0512-0520, 0522-0526, 0528, 0530, 0532-0543, 0545-0564, 0566-0568, 0570-0574, 0576-0579, 0581-0583, 0585-0597, 0599, 0601-0607,0609-0617, 0619-0623, 0627, 0629, 0631-0636, 0638-0643, 0645-0646, 0648-0657, 0662-0666, 0668, 0670-0676, 0678-0679, 0681-0684,0688-0689, 0691-0695, 0697, 0699-0703, 0707, 0711, 0713-0714, 0716-0717, 0719, 0721, 0723-0724, 0726-0744, 0746-0747, 0749-0758,0760-0763, 0765, 0767-0770, 0772-0776, 0779-0780, 0782, 0784-0785, 0790-0791, 0793-0795, 0797, 0799-0800, 0803, 0805, 0808-0809,0811-0817, 0819-0824, 0826-0829, 0831, 0833-0834, 0836-0842, 0845, 0848, 0851, 0853-0854, 0856-0857, 0860, 0865-0866, 0870, 0872,0874-0879, 0883-0884, 0886-0889, 0891-0892, 0894, 0897, 0899, 0901-0902, 0905-0906, 0909, 0912, 0914-0921, 0924-0928, 0930-0933,0935, 0937, 0939-0940, 0943, 0945, 0951, 0953, 0955-0957, 0959-0960, 0963, 0967, 0969, 0971, 0973, 0977-0979, 0982-0984, 0986-0987,0991, 0993, 0999, 1001, 1003, 1005, 1007-1009, 1013, 1015-1016, 1018, 1023-1024, 1029, 1032, 1034, 1041, 1043, 1049-1050, 1056,1063-1064, 1072, 1074-1076, 1079, 1083, 1085, 1088, 1093, 1098, 1100, 1106, 1108, 1110-1111, 1116-1117, 1120, 1127, 1144, 1154, 1165-1166,1178, 1180-1181, 1196, 1202, 1206, 1223, 1228, 1231, 1234, 1247, 1274, 1281, 1284, 1307, 1316, 1323, 1345, 1347, 1350, 1362, 1373-1375,1379, 1395, 1397, 1399, 1422, 1561, 1635, 1655, 1674, 1681, 1694, 1698, 1713, 1716, 1736, 1793, 1809, 1834, 1836, 1892, 1902, 2058, 2104,2115, 2143, 2252

The cruise speed may be either:• Managed• Selected

MANAGED

When the cruise altitude is reached, the A/THR operates in SPEED/MACH mode. The optimumcruise Mach number is automatically targeted. Its value depends on:• CI• Cruise flight level• Temperature deviation• Weight• Headwind component.

The crew should be aware that the optimum Mach number will vary according to the abovementioned parameters, e.g. it will increase with an increasing headwind, e.g. +50 kt head windequates to M +0.01.

SELECTED

Should ATC require a specific cruise speed or turbulence penetration is required, the pilot mustselect the cruise speed on the FCU. FMS predictions are updated accordingly until reachingeither the next step climb or top of descent, where the programmed speeds apply again. The FMSpredictions are therefore realistic.




At high altitude, the speed should not be reduced below GREEN DOT as this may create a situationwhere it is impossible to maintain speed and/or altitude as the increased drag may exceed theavailable thrust.

Ident.: NO-070-00005503.0002001 / 26 MAR 08Criteria: 22-1059, 22-1089, 22-1090, 22-1103, 22-1109, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1163, 22-1176, 22-1180,22-1193, 22-1197, 22-1209, 22-1217, 22-1218, 22-1219, 22-1233, 22-1235, 22-1240, P3560, P6193, P7372, P7373, P7519, P7520, P7666, P7706,P7707, SA�

9 Applicable to: MSN 0002-0021, 0031-0034, 0040-0041, 0044, 0052-0055, 0061-0067, 0076-0077, 0081-0082, 0087-0088, 0091, 0098-0102,0108, 0112, 0115, 0118-0119, 0121, 0123-0125, 0128-0131, 0133-0134, 0136, 0143-0146, 0152-0153, 0155-0156, 0158, 0160, 0165-0166, 0171,0173, 0176-0178, 0184, 0186-0188, 0192, 0194, 0196-0199, 0203-0208, 0211, 0213-0215, 0219-0220, 0223-0224, 0226-0228, 0235-0241, 0244,0262-0264, 0270-0274, 0278, 0281-0282, 0285-0287, 0297-0300, 0306-0307, 0312, 0317-0319, 0322-0323, 0328-0329, 0337, 0339-0340,0351-0352, 0355, 0358, 0360, 0365-0367, 0370, 0372, 0377, 0380-0381, 0383, 0387-0388, 0390, 0399-0400, 0402, 0408, 0410, 0417-0418,0448, 0455, 0471, 0491, 0498, 0501, 0507, 0509, 0511, 0521, 0527, 0529, 0531, 0544, 0565, 0569, 0575, 0580, 0584, 0598, 0600, 0608,0618, 0624-0626, 0628, 0630, 0637, 0644, 0647, 0658-0661, 0667, 0669, 0677, 0680, 0685-0687, 0690, 0696, 0698, 0704-0706, 0709-0710,0712, 0715, 0718, 0720, 0722, 0725, 0745, 0748, 0759, 0764, 0766, 0771, 0777-0778, 0781, 0783, 0786-0788, 0792, 0796, 0798, 0801-0802,0804, 0806-0807, 0810, 0818, 0825, 0830, 0832, 0835, 0843-0844, 0846-0847, 0849-0850, 0852, 0855, 0858-0859, 0861-0864, 0867-0869,0871, 0873, 0880-0882, 0885, 0890, 0893, 0895-0896, 0898, 0900, 0903-0904, 0907-0908, 0910-0911, 0913, 0922-0923, 0929, 0934, 0936,0938, 0941-0942, 0944, 0946-0950, 0952, 0954, 0958, 0961-0962, 0964-0966, 0968, 0970, 0972, 0974-0976, 0980-0981, 0985, 0988-0990,0992, 0994-0998, 1000, 1002, 1004, 1006, 1010-1012, 1014, 1017, 1019-1022, 1025-1028, 1030-1031, 1033, 1035-1040, 1042, 1044-1048,1051-1055, 1057-1062, 1065-1071, 1073, 1077-1078, 1080-1082, 1084, 1086-1087, 1089-1092, 1094-1097, 1099, 1101-1105, 1107, 1109,1112-1115, 1118-1119, 1121-1126, 1128-1143, 1145-1153, 1155-1164, 1167-1177, 1179, 1182-1195, 1197-1201, 1203-1205, 1207-1222, 1224-1227,1229-1230, 1232-1233, 1235-1246, 1248-1273, 1275-1280, 1282-1283, 1285-1306, 1308-1315, 1317-1322, 1324-1344, 1346, 1348-1349,1351-1361, 1363-1372, 1376-1378, 1380-1394, 1396, 1398, 1400-1421, 1423-1560, 1562-1634, 1636-1654, 1656-1673, 1675-1680, 1682-1693,1695-1697, 1699-1712, 1714-1715, 1717-1735, 1737-1792, 1794-1808, 1810-1833, 1835, 1837-1891, 1893-1901, 1903-2057, 2059-2103,2105-2114, 2116-2142, 2144-2251, 2253-3996

The cruise speed may be either:• Managed• Selected

MANAGED

When the cruise altitude is reached, the A/THR operates in SPEED/MACH mode. The optimumcruise Mach number is automatically targeted. Its value depends on:• CI• Cruise flight level• Temperature deviation• Weight• Headwind component.

The crew should be aware that the optimum Mach number will vary according to the abovementioned parameters, e.g. it will increase with an increasing headwind, e.g. +50 kt head windequates to M +0.01.Should ATC require a specific time over a waypoint, the crew can perform a vertical revision on thatwaypoint and enter a time constraint. The managed Mach number would be modified accordinglyto achieve this constraint. If the constraint can be met within a tolerance, a magenta asterix will be




displayed on the MCDU; if the constraint cannot be met, an amber asterix will be displayed. Oncethe constrained waypoint is sequenced, the ECON Mach is resumed.

SELECTED

Should ATC require a specific cruise speed or turbulence penetration is required, the pilot mustselect the cruise speed on the FCU. FMS predictions are updated accordingly until reachingeither the next step climb or top of descent, where the programmed speeds apply again. The FMSpredictions are therefore realistic.At high altitude, the speed should not be reduced below GREEN DOT as this may create a situationwhere it is impossible to maintain speed and/or altitude as the increased drag may exceed theavailable thrust.

ALTITUDE CONSIDERATIONSIdent.: NO-070-00005504.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The MCDU PROG page displays:• REC MAX FL• OPT FL.

REC MAX FL

REC MAX FL reflects the present engine and wing performance and does not take into account thecost aspect. It provides a 0.3 gbuffet margin. If the crew inserts a FL higher than REC MAX into theMCDU, it will be accepted only if it provides a buffet margin greater than 0.2 g. Otherwise, it will berejected and the message "CRZ ABOVE MAX FL" will appear on the MCDU scratchpad. Unlessthere are overriding operational considerations, e.g. either to accept a cruise FL higher than RECMAX or to be held significantly lower for a long period, REC MAX should be considered as the uppercruise limit.

OPT FL

OPT FL displayed on the MCDU is the cruise altitude for minimum cost when ECON MACH is flownand should be followed whenever possible. It is important to note that the OPT FL displayed on thePROG page is meaningful only if the wind and temperature profile has been accurately entered.The crew should be aware that flying at a level other than the OPT FL would adversely affect the tripcost.For each Mach number, there will be a different OPT FL. Should an FMGS failure occur, the crewshould refer to the FCOM or QRH to determine the OPT FL. FCOM and QRH charts are onlyprovided for two different Mach numbers.




STEP CLIMBIdent.: NO-070-00005505.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


Since the optimum altitude increases as fuel is consumed during the flight, from a cost point of view,it is preferable to climb to a higher cruise altitude when the aircraft weight permits. This technique,referred to as a Step Climb, is typically accomplished by initially climbing approximately 2 000 ft abovethe optimum altitude and then cruising at that flight level until approximately 4 000 ft below optimum.The MCDU STEP ALT page may be called a vertical revision from the MCDU F-PLN page or from theMCDU PERF CRZ page. Step climb can either be planned at waypoint (STEP AT) or be optimum steppoint calculated by the FMGS (ALT). If predictions are satisfactory in term of time and fuel saving, thecrew will insert it in F-PLN provided it is compatible with ATC.It may be advantageous to request an initial cruise altitude above optimum if altitude changes aredifficult to obtain on specific routes. This minimizes the possibility of being held at a low altitude andhigh fuel consumption condition for long periods of time. The requested/cleared cruise altitude shouldbe compared to the REC MAX altitude. Before accepting an altitude above optimum, the crew shoulddetermine that it will continue to be acceptable considering the projected flight conditions such asturbulence, standing waves or temperature change.




OPT FL follow up

The diagram above shows three step climb strategies with respect to OPT and REC MAX FL. Strategy1 provides the best trip cost, followed by 2 then 3.

Ident.: NO-070-00005505.0002001 / 26 MAR 08Criteria: 22-1089, 22-1090, 22-1103, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1163, 22-1176, 22-1180, 22-1193, 22-1197,22-1209, 22-1217, 22-1218, 22-1219, 22-1233, 22-1235, 22-1240, P7372, P7373, P7519, P7520, P7666, P7706, P7707, SA�


Since the optimum altitude increases as fuel is consumed during the flight, from a cost point of view,it is preferable to climb to a higher cruise altitude when the aircraft weight permits. This technique,




referred to as a Step Climb, is typically accomplished by initially climbing approximately 2 000 ft abovethe optimum altitude and then cruising at that flight level until approximately 4 000 ft below optimum.The MCDU STEP ALT page may be called a vertical revision from the MCDU F-PLN page or from theMCDU PERF CRZ page. Step climb can either be planned at waypoint (STEP AT) or be optimum steppoint calculated by the FMGS (ALT). If predictions are satisfactory in term of time and fuel saving, thecrew will insert it in F-PLN provided it is compatible with ATC.The OPT STEP computation will be accurate if vertical wind profile has been properly entered. Referto FMS USE of this section. Refer to FCOM/PER-CRZ-AEO-ALT-20 WIND ALTITUDE TRADE FORCONSTANT SPECIFIC RANGE to provide valuable tables to assess the effect of the vertical windprofile on the optimum cruise flight level.It may be advantageous to request an initial cruise altitude above optimum if altitude changes aredifficult to obtain on specific routes. This minimizes the possibility of being held at a low altitude andhigh fuel consumption condition for long periods of time. The requested/cleared cruise altitude shouldbe compared to the REC MAX altitude. Before accepting an altitude above optimum, the crew shoulddetermine that it will continue to be acceptable considering the projected flight conditions such asturbulence, standing waves or temperature change.

OPT FL follow up

The diagram above shows three step climb strategies with respect to OPT and REC MAX FL. Strategy1 provides the best trip cost, followed by 2 then 3.




EFFECT OF ALTITUDE ON FUEL CONSUMPTIONIdent.: NO-070-00005506.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The selected cruise altitude should normally be as close to optimum as possible. As deviation fromoptimum cruise altitude increases, performance economy decreases. The following table provideaverage specific range penalty when not flying at optimum altitude.

FIGURESIdent.: NO-070-00005507.0001001 / 26 MAR 08Criteria: G-CFM56-5B8, CFM56-5B8/3, 318-100�Applicable to: MSN 1660, 1939, 1991, 2017, 2035, 2051, 2059, 2071, 2081, 2100, 2109, 2218, 2276, 2317, 2328, 2333, 2344, 2350, 2358,2367, 2377, 2394, 2523, 2544, 2552, 2575, 2582, 2601, 2686, 2750, 2918, 2931, 2951, 2955, 2967, 2972, 3009, 3038, 3092, 3110, 3163, 3220,3225

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT –6000 ft0.7 % 1.6 % 5 % 10 %

Specific range penalty when not flying at optimum altitude

Ident.: NO-070-00005507.0002001 / 26 MAR 08Criteria: G-V2524-A5, 319-100�

12 Applicable to: MSN 0889, 0913, 0924, 0931, 0976, 1010, 1043, 1049, 1056, 1064, 1066, 1074, 1088, 1092, 1096, 1098, 1103, 1111, 1113, 1116,1139-1140, 1159, 1178, 1223, 1228, 1281, 1323, 1350, 1373-1375, 1395, 1397, 1406, 1410, 1463, 1490, 1527, 1534, 1547, 1552, 1563, 1565,1575-1576, 1608, 1643, 1698, 1703, 1727, 1729, 1758, 1768, 1790, 1801, 1826, 1831, 1837, 1844, 1855, 1880, 1893, 1912, 1934, 1947, 1952,1955, 1962, 2023, 2032, 2089, 2096, 2200, 2203, 2232, 2273, 2277, 2295-2296, 2302, 2304, 2321, 2335, 2339, 2362, 2371, 2383, 2396, 2404,2408, 2414, 2424, 2426, 2431, 2433, 2435, 2444, 2452, 2458, 2467-2468, 2470, 2473, 2485, 2490, 2505, 2560, 2567-2568, 2570, 2572, 2574,2579, 2585, 2595, 2603, 2615, 2622, 2631, 2648, 2655, 2657, 2659-2660, 2666-2667, 2669, 2673, 2679, 2690, 2698, 2704, 2711, 2718, 2723,2738-2739, 2784, 2797, 2813, 2815, 2833, 2845, 2850, 2858, 2864, 2872, 2886-2888, 2892-2894, 2898, 2901, 2929, 2940, 2942, 2948, 2963,2969, 2976, 2978, 2983, 2997, 3007, 3011, 3017, 3020, 3026, 3032, 3057, 3104, 3128, 3142, 3144, 3165, 3172, 3193, 3248, 3252, 3258, 3269,3276, 3311, 3317, 3342, 3352, 3358, 3375, 3393, 3395, 3421, 3424, 3428, 3454, 3463, 3491, 3500, 3520, 3534, 3548, 3561, 3578, 3580, 3588,3590, 3595, 3614, 3663, 3671, 3685, 3694, 3710, 3757, 3759, 3768, 3770, 3772, 3779, 3801, 3803, 3832, 3839, 3841, 3860, 3890, 3638, 3911

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT – 6 000 ft1 % 3 % 7.2 % 12.2 %





Ident.: NO-070-00005507.0003001 / 26 MAR 08Criteria: G-CFM56-5A1, 320-200�

13 Applicable to: MSN 0029-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0086, 0093-0094, 0100-0112, 0115-0130, 0133-0162,0167, 0170-0177, 0183-0185, 0188, 0191-0192, 0196-0197, 0199-0224, 0226-0229, 0231-0234, 0236-0242, 0244-0246, 0248, 0253-0255, 0258,0262-0274, 0277-0278, 0281-0282, 0284-0287, 0290, 0293, 0297-0298, 0300-0303, 0306-0307, 0309-0312, 0318-0319, 0323-0324, 0328-0330,0333, 0337, 0341-0342, 0346, 0348, 0350, 0352, 0356, 0359, 0365, 0370-0371, 0377-0378, 0382-0384, 0390, 0395, 0401-0404, 0413, 0426,0482, 0491, 0501, 0507, 0511, 0531, 0534, 0549, 0554, 0615, 0622, 0658, 0662, 0669, 0671, 0685, 0726, 0958, 0975, 1187, 1337, 1365, 1367,1700, 1973, 2054, 2061, 2082, 2092

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT –6000 ft- 1.1 % 4.7 % 9.5 %



14 Applicable to: MSN 0425, 0435, 0439, 0442, 0448, 0450, 0452-0457, 0462-0465, 0470-0472, 0475, 0479, 0483, 0485, 0487, 0489, 0496,0500, 0503-0504, 0506, 0508, 0510, 0512, 0523, 0527, 0530, 0539-0540, 0542-0543, 0551, 0565, 0568, 0571, 0573, 0575, 0580, 0582, 0584,0587, 0589, 0592, 0613, 0638, 0640, 0655, 0659, 0661, 0667, 0676, 0678, 0683, 0702, 0709-0710, 0712, 0720, 0722, 0751, 0756, 0758, 0760,0762, 0770, 0780, 0784, 0791, 0803, 0805, 0812, 0816, 0820, 0822, 0824, 0826, 0834, 0836, 0842, 0849, 0851, 0856-0857, 0859, 0865-0866,0872, 0877, 0881, 0886, 0895, 0899-0900, 0918, 0927-0928, 0930, 0932, 0934, 0943, 0950, 0953, 0955, 0966, 0969, 0977, 0990, 1001, 1003,1014, 1032, 1035, 1039, 1050, 1057, 1075-1076, 1079, 1083, 1085, 1104-1105, 1110, 1117, 1123, 1128, 1143, 1146, 1156, 1158, 1163, 1166, 1173,1177, 1183, 1192, 1194, 1196, 1215, 1234-1235, 1240, 1246, 1248, 1251, 1253, 1257, 1266, 1270, 1272, 1274, 1280, 1282, 1284, 1290, 1302,1327, 1341, 1343, 1349, 1359, 1363, 1368, 1376, 1383, 1398, 1407, 1409, 1411, 1418-1419, 1422, 1424, 1427, 1432, 1435, 1446, 1452, 1459,1464, 1469, 1475, 1486, 1495, 1497, 1506, 1508, 1514, 1518, 1528, 1533, 1538, 1546, 1555, 1557, 1559, 1561, 1566, 1580, 1584, 1586, 1591,1593, 1595, 1609-1610, 1613, 1617, 1620-1621, 1628, 1631, 1644, 1648, 1650, 1652, 1661, 1663, 1665, 1669, 1672, 1680, 1682, 1687, 1689,1696-1697, 1702, 1705, 1708, 1710, 1715, 1721, 1723, 1728, 1732, 1739, 1741, 1749, 1754-1755, 1760, 1764, 1771, 1773, 1782, 1784-1785,1792, 1802, 1804, 1814, 1818, 1821-1823, 1825, 1827, 1829, 1832, 1835, 1840, 1842, 1845, 1847, 1849, 1856-1857, 1861-1862, 1865, 1868,1871, 1883, 1888, 1891, 1895-1896, 1898-1899, 1904, 1907, 1909-1910, 1914-1915, 1917-1918, 1922, 1927, 1933, 1935, 1944-1945, 1948,1957-1958, 1969, 1979, 1987, 1993, 1996, 1998, 2006, 2016, 2020, 2027, 2029, 2031, 2038, 2040, 2042, 2058, 2063, 2070, 2073, 2075, 2077,2079, 2085, 2088, 2090, 2094, 2097, 2099, 2108, 2112, 2121, 2125, 2128, 2130, 2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157,2159-2161, 2164, 2167-2169, 2173, 2177, 2185, 2193, 2195, 2197, 2201, 2204, 2210, 2215, 2223, 2229, 2231, 2238, 2246, 2254, 2257, 2259,2275, 2280, 2284, 2286, 2288, 2292, 2297, 2299, 2307, 2310, 2312, 2314, 2316, 2322, 2329, 2331, 2334, 2336, 2338, 2340, 2343, 2345, 2352,2356, 2359, 2366, 2368, 2372, 2376, 2384, 2386, 2393, 2395, 2397, 2401, 2403, 2405, 2413, 2415, 2417, 2422-2423, 2428, 2430, 2441, 2443,2445, 2447, 2449, 2453, 2455, 2457, 2459, 2461, 2475, 2479, 2482, 2489, 2491, 2496, 2502, 2504, 2509, 2513, 2515, 2520, 2522, 2524, 2526,2531, 2533, 2535, 2537, 2564, 2566, 2571, 2573, 2576-2577, 2580, 2587, 2589, 2594, 2598, 2600, 2602, 2604, 2608-2609, 2613, 2626, 2630,2640, 2642, 2645, 2647, 2649, 2651, 2661, 2663, 2670-2671, 2676, 2680, 2688-2689, 2692, 2701, 2703, 2710, 2714, 2717, 2724-2725, 2728,2731-2732, 2734, 2737, 2747, 2752-2753, 2755, 2766, 2772, 2781, 2783, 2787, 2802, 2804, 2808, 2814, 2817, 2828, 2832, 2838, 2840, 2844,2848, 2856, 2859, 2863, 2871, 2874, 2880, 2883, 2896, 2900, 2904, 2906, 2908, 2911, 2914, 2922, 2928, 2934, 2941, 2943, 2945, 2952-2953,2958, 2970, 2977, 2982, 2984, 2987, 2990, 2992, 3004, 3010, 3012, 3029, 3033, 3039, 3050, 3066, 3071-3072, 3074, 3086, 3089, 3091, 3105,3119, 3125, 3127, 3141, 3143, 3150, 3156, 3158-3159, 3162, 3166-3167, 3177, 3183, 3185, 3190, 3192, 3196, 3208, 3210, 3219, 3227-3228,3239, 3244, 3257, 3259, 3263-3264, 3270, 3275, 3287, 3296, 3301, 3303, 3308, 3314, 3316, 3330, 3332, 3335, 3341, 3348, 3351, 3354, 3357,3365, 3379, 3381, 3384, 3386, 3392, 3402, 3409, 3414, 3416, 3423, 3430, 3437, 3439, 3449, 3451, 3453, 3457, 3468, 3474, 3478-3479, 3481,3483-3484, 3488, 3495-3497, 3499, 3517, 3519, 3524, 3526, 3531, 3541, 3543, 3547, 3550, 3554, 3558, 3562, 3567, 3572, 3603, 3607, 3613,3618, 3621-3622, 3641, 3649-3650, 3654, 3659, 3668, 3674, 3676-3677, 3692-3693, 3697, 3703, 3707, 3709, 3713-3714, 3716, 3718-3719,3721, 3724, 3726, 3734, 3736, 3741, 3743, 3745, 3748, 3753, 3760, 3771, 3773, 3782-3783, 3785, 3793, 3800, 3804, 3807, 3811-3812, 3829,3850, 3863, 3904, 3937, 3591, 3775, 3797, 3837, 3873, 3877, 3902, 3910, 3912, 3917, 3927, 3935, 3941-3943, 3947, 3959, 3965, 3968, 3995

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT –6000 ft1.4 % 2.1 % 6.2 % 12 %





Ident.: NO-070-00005507.0005001 / 26 MAR 08Criteria: G-CFM56-5B2, CFM56-5B2/P, 321-100�Applicable to: MSN 0434, 0477, 0488, 0494-0495, 0513-0516, 0524, 0526, 0532, 0576, 0583, 0586, 0593, 0599, 0765, 0819, 0848, 0940,0959, 1220

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT –6000 ft2.3 % 1.4 % 4.6 % 15.2 %



15 Applicable to: MSN 0633, 0663, 0668, 0680, 0687, 0715, 0725, 0771, 0787, 0792, 0802, 0806, 0810-0811, 0835, 0855, 0864, 0878, 0908,0915, 0954, 0963, 0968, 0974, 0983, 0993, 1004, 1008, 1015, 1024, 1042, 1045, 1060, 1080, 1153, 1161, 1174, 1188, 1195, 1199, 1202, 1204,1207, 1214, 1218, 1227, 1260, 1273, 1276, 1293, 1333, 1366, 1408, 1421, 1428, 1433, 1438, 1487, 1596, 1614, 1636, 1670, 1690, 1695, 1707,1711, 1734, 1763, 1776, 1788, 1794, 1843, 1850, 1869, 1878, 1926, 1928, 1941, 1946, 1950, 1953, 1956, 1967, 1970, 1974, 1977, 1984, 1995,2021, 2041, 2045, 2055, 2067, 2080, 2105, 2107, 2110, 2190, 2211, 2216, 2226, 2234, 2247, 2255, 2261, 2267, 2290, 2303, 2305, 2320,2323-2324, 2351, 2363, 2410, 2462, 2476, 2480, 2521, 2530, 2536, 2553, 2590, 2610, 2653, 2682, 2687, 2713, 2730, 2741, 2759, 2767, 2793,2799, 2809, 2823, 2862, 2868, 2936, 2971, 2974, 2999, 3005, 3013, 3015, 3022, 3067, 3075, 3081, 3106, 3112, 3126, 3198, 3207, 3217, 3222,3229, 3235, 3241, 3251, 3254, 3265, 3274, 3283, 3290, 3294, 3297, 3315, 3339, 3350, 3355, 3360, 3369, 3382, 3387, 3397, 3405, 3429, 3434,3458-3459, 3462, 3493, 3507, 3512, 3522, 3525, 3527, 3539, 3546, 3552, 3566, 3575, 3583, 3587, 3592, 3600, 3625, 3636, 3645, 3669, 3681,3712, 3730, 3737, 3740, 3761, 3764, 3784, 3796, 3816, 3820, 3847, 3858, 3862, 3867, 3878, 3920, 3864, 3869, 3881, 3893, 3899, 3916, 3924,3926, 3934, 3936, 3938, 3944, 3948, 3951, 3960, 3964, 3966, 3969, 3977-3981, 3989-3993, 3996

OPT +2 000 ft OPT -2 000 ft OPT -4 000 ft2.4 % 1.5 % 4.9 %


Ident.: NO-070-00005507.0015001 / 26 MAR 08Criteria: P6310, 318-100�Applicable to: MSN 3001, 3030, 3062, 3214, 3216, 3371, 3390, 3438, 3469, 3509, 3585, 3602, 3606, 3635, 3642

OPT +2 000 ft OPT –2000 ft OPT –4000 ft OPT – 6 000 ft2 % 2 % 7 % 11 %


FUEL MONITORINGIdent.: NO-070-00005508.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The flight plan fuel burn from departure to destination is based on certain assumed conditions. Theseinclude gross weight, cruise altitude, route of flight, temperature, cruise wind and cruise speed. Actualfuel consumption should be compared with the flight plan fuel consumption at least once every 30 min.




The crew should be aware that many factors influence fuel consumption, such as actual flight level,cruise speed and unexpected meteorological conditions. These parameters should normally bereflected in the FMS.

The crew must keep in mind that• A significant deviation between planned and actual fuel figures without reason• An excessive fuel flow leading to a potential imbalance• An abnormal decrease in total fuel quantity (FOB+FU)

May indicate a fuel leak and the associated procedure should be applied.

FUEL TEMPERATUREIdent.: NO-070-00005509.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Fuel freeze refers to the formation of wax crystals suspended in the fuel, which can accumulate whenfuel temperature is below the freeze point (-47 °C for jet A1) and can prevent proper fuel feed to theengines.During normal operations, fuel temperature rarely decreases to the point that it becomes limiting.However, extended cruise operations increase the potential for fuel temperatures to reach the freezepoint. Fuel temperature will slowly reduce towards TAT. The rate of cooling of fuel can be expected tobe in the order of 3 °C per hour with a maximum of 12 °C per hour in the most extreme conditions.

If fuel temperature approaches the minimum allowed, the ECAM outputs a caution. Considerationshould be given to achieving a higher TAT:• Descending or diverting to a warmer air mass may be considered. Below the tropopause, a 4 000 ft

descent gives a 7 °C increase in TAT. In severe cases, a descent to as low as 25 000 ft may berequired.

• Increasing Mach number will also increase TAT. An increase of M 0.01 produces approximately0.7 °C increase in TAT.

In either case, up to 1 h may be required for fuel temperature to stabilise. The crew should consider thefuel penalty associated with either of these actions.

APPROACH PREPARATIONIdent.: NO-070-00005510.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The latest destination weather should be obtained approximately 15 min prior to descent and theFMGS programmed for the descent and arrival. During FMGS programming, the PF will be head down,so it is important that the PNF does not become involved in any tasks other than flying the aircraft.




The fuel predictions will be accurate if the F-PLN is correctly entered in terms of arrival, go-around andalternate routing.The FMGS will be programmed as follows:

F-PLN

Lateral:‐ Landing runway, STAR, Approach and Go-around procedure.‐ F-PLN to alternate.

Vertical:‐ Altitude and Speed constraints,‐ Compare vertical F-PLN on MCDU with approach chart

MCDU F-PLN page vs approach chart crosscheck




RAD NAV

Manually tune the VOR/DME and/or NDB if required. Check ILS ident, frequency and associatedcourse of destination airfield as required. It is not recommended manually forcing the ILS identifieras, in case of late runway change, the associated ILS would not be automatically tuned.

PROG

Insert VOR/DME or landing runway threshold of destination airfield in the BRG/DIST field asrequired.

PERF

PERF APPR:• Descent winds,• Destination airfield weather (QNH, Temperature and wind) The entered wind should be the

average wind given by the ATC or ATIS. Do not enter gust values, for example, if the wind is150 kt/20-25 kt, insert the lower speed 150 kt/20 kt (With managed speed mode in approach,ground speed mini-function will cope with the gusts).

• Minima (DH for CATII or CATIII approach and MDA for others approaches)• Landing configuration (wind shear anticipated or in case of failure).

PERF GO AROUND: Check thrust reduction and acceleration altitude.

FUEL PRED

Check estimated landing weight, EFOB and extra fuel.

SEC F-PLN

To cover contingencies e.g. runway change, circling or diversion.Once the FMGS has been programmed, the PNF should then cross check the information prior tothe Approach briefing.

APPROACH BRIEFINGIdent.: NO-070-00005511.0001001 / 26 MAY 08Criteria: SA�Applicable to: ALL

The main objective of the approach briefing is for the PF to inform the PNF of his intended course ofaction for the approach. The briefing should be practical and relevant to the actual weather conditionsexpected. It should be concise and conducted in a logical manner. It should be given at a time of lowworkload if possible, to enable the crew to concentrate on the content. It is very important that anymisunderstandings are resolved at this time.




PF briefing Associated cross checkAircraft type and technical status

NOTAMWeather

‐ Accessibility‐ Runway in use

Fuel

‐ Extra fuelFUEL PRED page

Descent

‐ TOD (time, position)‐ MORA, STAR, MSA‐ Altitude and speed constraints

F-PLN pageF-PLN page

Holding (if expected)

‐ Entry in holding pattern‐ MHA and MAX speed

Approach

‐ Approach type‐ Altitude and FAF identification‐ Glide path‐ MDA/DH‐ Missed approach procedure‐ Alternate considerations

‐ PERF APPR and ND‐ F-PLN‐ PFD/FMA‐ PERF APPR‐ F-PLN‐ F-PLN

Landing

‐ Runway condition, length and width‐ Tail strike awareness‐ Use of Auto brake‐ Expected taxi route

Radio aids RAD NAV


NORMAL OPERATIONSDESCENT


PREFACEIdent.: NO-080-00005512.0001001 / 28 NOV 08Criteria: SA�Applicable to: ALL

1 The PF will set preferably the MCDU PROG or PERF page as required (PROG page provides VDEVin NAV mode and BRG/DIST information, PERF DES page provides predictions down to any insertedaltitude in DES/OP DES modes) whereas the PNF will set the MCDU F-PLN page.In mountainous areas, the selection of TERR ON ND sw enhances the pilot awareness and can beused in any flight phase.If use of radar is required, consider selecting the radar display on the PF side and TERR on PNF sideonly.

COMPUTATION PRINCIPLESIdent.: NO-080-00005513.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

TOD AND PROFILE COMPUTATION

The FMGS calculates the Top Of Descent point (TOD) backwards from a position 1 000 ft on thefinal approach with speed at VAPP. It takes into account any descent speed and altitude constraintsand assumes managed speed is used. The first segment of the descent will always be idle segmentuntil the first altitude constraint is reached. Subsequent segments will be "geometric", i.e. thedescent will be flown at a specific angle, taking into account any subsequent constraints. If the STARincludes a holding pattern, it is not considered for TOD or fuel computation. The TOD is displayed onthe ND track as a white symbol:

descent path

The idle segment assumes a given managed speed flown with idle thrust plus a small amount ofthrust. This gives some flexibility to keep the aircraft on the descent path if engine anti-ice is used orif winds vary. This explains THR DES on the FMA.




The TOD computed by the FMS is quite reliable provided the flight plan is properly documenteddown to the approach.

MANAGED DESCENT SPEED PROFILE

The managed speed is equal to:• The ECON speed (which may have been modified by the crew on the PERF DES page, before

entering DESCENT phase), or• The speed constraint or limit when applicable.

GUIDANCE AND MONITORINGIdent.: NO-080-00005514.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

INTRODUCTION

To carry out the descent, the crew can use either the managed descent mode (DES) or the selecteddescent modes (OP DES or V/S). Both descent modes can be flown either with selected speed ormanaged speed.The modes and monitoring means are actually linked.The managed DES mode guides the aircraft along the FMS pre-computed descent profile, as longas it flies along the lateral F-PLN: i.e. DES mode is available if NAV is engaged. As a general rulewhen DES mode is used, the descent is monitored using VDEV called "yoyo" on PFD, or its digitalvalue on the PROG page, as well as the level arrow on the ND.The selected OP DES or V/S modes are used when HDG is selected or when ALT CSTR maybe disregarded or for various tactical purposes. As a general rule when OP DES or V/S modesare used, the descent is monitored using the Energy Circle, (displayed if HDG or TRK modes andindicating the required distance to descend, decelerate and land from present position) and the levelarrow on the ND. When the aircraft is not far away from the lateral F-PLN (small XTK), the yoyo onPFD is also a good indicator.

MANAGED DESCENT MODE

The managed descent profile from high altitude is approximately 2.5 °.As an estimation of the distance to touchdown is required to enable descent profile monitoring, it isimportant to ensure that the MCDU F-PLN plan page reflects the expected approach routing. Anygross errors noted in the descent profile are usually a result of incorrect routing entered in the MCDUor non-sequencing of F-PLN waypoints, giving a false distance to touchdown.

DESCENT INITIATION

To initiate a managed descent, the pilot will set the ATC cleared altitude on the FCU and pushthe ALT selector. DES mode engages and is annunciated on the FMA. If an early descent were




required by ATC, DES mode would give 1 000 ft/min rate of descent, until regaining the computedprofile.To avoid overshooting the computed descent path, it is preferable to push the FCU ALT selector afew miles prior to the calculated TOD. This method will ensure a controlled entry into the descentand is particularly useful in situations of high cruise Mach number or strong upper winds.If the descent is delayed, a "DECELERATE" message appears in white on the PFD and in amberon the MCDU. Speed should be reduced towards green dot, and when cleared for descent, thepilot will push for DES and push for managed speed. The speed reduction prior to descent willenable the aircraft to recover the computed profile more quickly as it accelerates to the manageddescent speed.

DESCENT PROFILE

When DES with managed speed is engaged, the AP/FD guides the aircraft along the pre-computed descent path determined by a number of factors such as altitude constraints, wind anddescent speed. However, as the actual conditions may differ from those planned, the DES modeoperates within a 20 kt speed range around the managed target speed to maintain the descentpath.

managed descent: speed target range principle

If the aircraft gets high on the computed descent path:

• The speed will increase towards the upper limit of the speed range, to keep the aircraft onthe path with IDLE thrust.

• If the speed reaches the upper limit, THR IDLE is maintained, but the autopilot does notallow the speed to increase any more, thus the VDEV will slowly increase.

• A path intercept point, which assumes half speedbrake extension, will be displayed on theND descent track.




• If speed brakes are not extended, the intercept point will move forward. If it gets closeto an altitude-constrained waypoint, then a message "AIR BRAKES" or "MORE DRAG",depending of the FMGS standard, will be displayed on the PFD and MCDU.

This technique allows an altitude constraint to be matched with minimum use of speedbrakes.When regaining the descent profile, the speedbrakes should be retracted to prevent the A/THR applying thrust against speedbrakes. If the speedbrakes are not retracted, the "SPDBRK" message on the ECAM memo becomes amber and "RETRACT SPEEBRAKES" isdisplayed in white on the PFD.

A/C above descent path

If the aircraft gets low on the computed descent path:The speed will decrease towards the lower limit of the speed range with idle thrust. When thelower speed limit is reached the A/THR will revert to SPEED/MACH mode and apply thrust tomaintain the descent path at this lower speed. The path intercept point will be displayed onthe ND, to indicate where the descent profile will be regained.

A/C below descent path

If selected speed is used:The descent profile remains unchanged. As the selected speed may differ from the speedtaken into account for pre-computed descent profile and speed deviation range does notapply, the aircraft may deviate from the descent profile e.g. if the pilot selects 275 kt with apre-computed descent profile assuming managed speed 300 kt, VDEV will increase.




SELECTED DESCENT

There are 2 modes for flying a selected descent, namely OP DES and V/S. These modes will beused for pilot tactical interventions.V/S mode is automatically selected when HDG or TRK mode is selected by the pilot, while in DESmode. Furthermore, in HDG or TRK mode, only V/S or OP DES modes are available for descent.To initiate a selected descent, the pilot should set the ATC cleared altitude on the FCU and pull theALT selector. OP DES mode engages and is annunciated on the FMA. In OP DES mode, the A/THRcommands THR IDLE and the speed is controlled by the THS.Speed may be either managed or selected. In managed speed, the descent speed is displayed onlyas a magenta target but there is no longer a speed target range since the pre-computed flight profiledoes not apply.The AP/FD will not consider any MCDU descent altitude constraints and will fly an unrestricteddescent down to the FCU selected altitude.If the crew wishes to steep the descent down, OP DES mode can be used, selecting a higher speed.Speedbrake is very effective in increasing descent rate but should be used with caution at highaltitude due to the associated increase in VLS.If the pilot wishes to shallow the descent path, V/S can be used. A/THR reverts to SPEED mode. Inthis configuration, the use of speedbrakes is not recommended to reduce speed, since this wouldlead to thrust increase and the speed would be maintained.

MODE REVERSIONIdent.: NO-080-00005515.0001001 / 26 MAR 08Criteria: P4320, P5983, SA�

2 Applicable to: MSN 0029, 0035-0039, 0042-0043, 0045-0059, 0064-0068, 0073-0077, 0080-0082, 0084-0085, 0087-0091, 0095-0099, 0103,0109, 0112-0114, 0119-0120, 0122-0124, 0126-0127, 0132, 0134, 0136, 0138-0143, 0146, 0148-0151, 0154, 0157-0159, 0163-0164, 0167-0170,0173-0177, 0179-0183, 0185, 0189-0191, 0193, 0195-0196, 0199, 0204-0205, 0207, 0210-0212, 0219, 0221-0225, 0229-0234, 0240-0243,0245-0257, 0259-0261, 0264-0266, 0274-0277, 0279-0280, 0283-0284, 0288-0296, 0299-0305, 0308-0317, 0320-0328, 0330-0336, 0338,0341-0345, 0347-0350, 0353-0354, 0356-0357, 0359, 0361-0365, 0368-0371, 0373-0376, 0378-0379, 0383-0386, 0389-0398, 0402-0407,0409, 0411, 0413-0416, 0419-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0490, 0492, 0496-0497,0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0534, 0537-0540, 0542-0543, 0546, 0549, 0551-0552,0554-0555, 0557-0558, 0561, 0565, 0568-0572, 0575, 0579-0582, 0584, 0587, 0589-0592, 0594, 0597, 0601, 0604-0607, 0611, 0613-0615,0617, 0619-0620, 0622, 0624, 0626, 0628, 0630-0634, 0638-0639, 0645, 0648-0650, 0655-0656, 0658-0659, 0661-0662, 0666-0667,0669-0672, 0675, 0677-0678, 0682-0683, 0685, 0688, 0691, 0693, 0695, 0697, 0702, 0711, 0714, 0719, 0721, 0726, 0728, 0731-0732,0736, 0739-0740, 0742-0743, 0746, 0751-0752, 0756-0759, 0762, 0768-0770, 0773, 0775-0776, 0779-0781, 0784-0785, 0787, 0791-0792,0795, 0797, 0800, 0802-0803, 0805, 0808, 0811-0814, 0816-0817, 0820, 0822-0824, 0826, 0829, 0831, 0834, 0836, 0839-0840, 0842, 0845,0851-0852, 0856-0857, 0865-0866, 0869, 0877, 0880, 0888, 0963, 1008, 1042, 1204, 1227

If a high V/S target is selected, the autopilot will pitch the aircraft down to fly the target V/S. Thus theaircraft will tend to accelerate, while A/THR commands idle thrust to try to keep the speed. When IASwill reach a speed close to VMO or VFE, the descent mode will revert to OP DES to regain the initialtarget speed.





3 Applicable to: MSN 0031, 0034, 0040-0041, 0069-0072, 0078, 0083, 0086, 0093-0094, 0104, 0110-0111, 0116-0118, 0121, 0125, 0135,0137, 0147, 0152-0153, 0160-0162, 0165-0166, 0171-0172, 0178, 0192, 0194, 0197-0198, 0200-0202, 0206, 0208-0209, 0213, 0216-0218,0258, 0262-0263, 0267-0269, 0272-0273, 0281-0282, 0297-0298, 0306-0307, 0318-0319, 0329, 0339-0340, 0346, 0351, 0355, 0358, 0360,0366-0367, 0372, 0380-0382, 0387-0388, 0399-0401, 0408, 0410, 0412, 0417-0418, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488,0493-0495, 0502, 0505, 0513-0520, 0522, 0524, 0526, 0532-0533, 0535, 0541, 0545, 0548, 0550, 0553, 0556, 0559-0560, 0562-0564,0566-0567, 0573-0574, 0576-0578, 0583, 0585-0586, 0588, 0593, 0595-0596, 0599, 0603, 0609-0610, 0612, 0616, 0621, 0623, 0627, 0629,0635-0636, 0640-0643, 0646, 0651-0654, 0657, 0663-0665, 0668, 0673-0674, 0676, 0679-0681, 0684, 0686-0687, 0689-0690, 0692, 0694,0696, 0698-0701, 0703-0710, 0712-0713, 0715-0718, 0720, 0722-0725, 0727, 0729-0730, 0733-0735, 0737-0738, 0741, 0744-0745, 0747-0750,0754-0755, 0760-0761, 0763-0767, 0771-0772, 0774, 0778, 0782-0783, 0786, 0788-0790, 0793-0794, 0798-0799, 0801, 0804, 0806-0807,0809-0810, 0815, 0818-0819, 0821, 0825, 0827-0828, 0830, 0832-0833, 0835, 0837-0838, 0841, 0843-0844, 0846-0850, 0853-0855,0858-0864, 0867-0868, 0870-0876, 0878-0879, 0881-0887, 0889-0937, 0939-0962, 0964-0984, 0986-0997, 0999, 1001-1007, 1009-1019,1021-1024, 1026-1035, 1037-1041, 1043-1132, 1134-1136, 1138-1149, 1152-1188, 1191-1200, 1202-1203, 1205-1215, 1217-1226, 1228-1266,1268-1270, 1272-1298, 1300-1343, 1345-1386, 1388-1403, 1405-1414, 1416-1443, 1445-1448, 1450-1457, 1459-1470, 1472-1475, 1477,1479-1501, 1503-1504, 1506-1523, 1525-1598, 1600-1615, 1617-1621, 1623-1639, 1641-1644, 1646-1657, 1659, 1661-1676, 1678-1690,1692-1698, 1700-1732, 1734-1793, 1795-1858, 1860-1872, 1874-1877, 1880-1884, 1886-1893, 1895-1899, 1901-1923, 1925-1927, 1929-1937,1940-1948, 1950, 1954-1955, 1957-1966, 1968-1976, 1978-1990, 1993-2014, 2016, 2018, 2020, 2022, 2027, 2029, 2031, 2034, 2036, 2038,2040, 2042, 2044, 2046, 2048-2049, 2054, 2056, 2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2104, 2137, 2143, 2157, 2225, 2242, 2248,2252, 2311, 2381, 2391, 2472, 2488, 2563, 2599

If a high V/S target is selected (or typically after a DES to V/S reversion), the autopilot will pitch theaircraft down to fly the target V/S. Thus the aircraft will tend to accelerate, while A/THR commands idlethrust to try to keep the speed. When IAS will reach a speed close to VMO or VFE, the autopilot willpitch the aircraft up, so as to fly a V/S allowing VMO or VFE to be maintained with idle thrust.

Ident.: NO-080-00005515.0005001 / 26 MAR 08Criteria: 22-1072, 22-1123, P4320, P7790, SA�

4 Applicable to: MSN 0002, 0005-0014, 0019-0020, 0044, 0061-0063, 0100-0101, 0108, 0128-0131, 0133, 0144-0145, 0155-0156, 0184,0186-0188, 0214, 0226-0228, 0235-0236, 0239, 0270, 0278, 0285-0287, 0337, 0352, 0377, 0491, 0498, 0509, 0521, 0529, 0544, 0598,0600, 0608, 0618, 0625, 0637, 0644, 0647, 0660, 0777, 0796, 0938, 0985, 0998, 1000, 1020, 1025, 1036, 1133, 1137, 1150-1151, 1189-1190,1201, 1216, 1267, 1271, 1299, 1344, 1387, 1404, 1415, 1444, 1449, 1458, 1471, 1476, 1478, 1502, 1505, 1524, 1599, 1616, 1622, 1640, 1645,1658, 1660, 1677, 1691, 1699, 1733, 1794, 1859, 1873, 1878-1879, 1885, 1894, 1900, 1924, 1928, 1938-1939, 1949, 1951-1953, 1956, 1967,1977, 1991, 2015, 2017, 2019, 2021, 2023-2026, 2028, 2030, 2032-2033, 2035, 2037, 2039, 2041, 2043, 2045, 2047, 2050-2053, 2055, 2057,2059-2060, 2062, 2064, 2066-2067, 2069, 2071-2072, 2074, 2076-2103, 2105-2136, 2138-2142, 2144-2156, 2158-2224, 2226-2241, 2243-2247,2249-2251, 2253-2310, 2312-2380, 2382-2390, 2392-2471, 2473-2487, 2489-2562, 2564-2598, 2600-3996

If a high V/S target is selected (or typically after a DES to V/S reversion), the autopilot will pitch theaircraft down to fly the target V/S. Thus the aircraft will tend to accelerate, while A/THR commands idlethrust to try to keep the speed. When IAS will reach a speed close to VMO or VFE, the autopilot willpitch the aircraft up, so as to fly a V/S allowing VMO or VFE to be maintained with idle thrust.Triple click will be triggered.

Ident.: NO-080-00005515.0006001 / 26 MAR 08Criteria: 22-1123, SA�

5 Applicable to: MSN 0003, 0016, 0021, 0033, 0102, 0115, 0203, 0215, 0220, 0237, 0244

If a high V/S target is selected, the autopilot will pitch the aircraft down to fly the target V/S. Thus theaircraft will tend to accelerate, while A/THR commands idle thrust to try to keep the speed. When IAS




will reach a speed close to VMO or VFE, the descent mode will revert to OP DES to regain the initialtarget speed.Triple click will be triggered.

DESCENT CONSTRAINTSIdent.: NO-080-00005516.0001001 / 26 MAR 08Criteria: SA�

6 Applicable to: MSN 0029, 0035-0039, 0042-0043, 0045-0051, 0056-0059, 0068-0075, 0078-0080, 0083-0090, 0093-0097, 0103-0104,0109-0111, 0113-0114, 0116-0117, 0120, 0122, 0126-0127, 0132, 0135, 0137-0142, 0147-0151, 0154, 0157, 0159, 0161-0164, 0167-0170, 0172,0174-0175, 0179-0183, 0185, 0189-0191, 0193, 0195, 0200-0202, 0209-0210, 0212, 0216-0218, 0221-0222, 0225, 0229-0234, 0242-0243,0245-0261, 0265-0269, 0275-0277, 0279-0280, 0283-0284, 0288-0296, 0301-0305, 0308-0311, 0313-0316, 0320-0321, 0324-0327, 0330-0336,0338, 0341-0350, 0353-0354, 0356-0357, 0359, 0361-0364, 0368-0369, 0371, 0373-0376, 0378-0379, 0382, 0384-0386, 0389, 0391-0398,0401, 0403-0407, 0409, 0411-0416, 0419-0447, 0449-0454, 0456-0470, 0472-0490, 0492-0497, 0499-0500, 0502-0506, 0508, 0510, 0512-0520,0522-0526, 0528, 0530, 0532-0543, 0545-0583, 0585-0597, 0599, 0601-0607, 0609-0617, 0619-0624, 0626-0636, 0638-0643, 0645-0646,0648-0657, 0659, 0661-0668, 0670-0679, 0681-0684, 0686, 0688-0714, 0716-0724, 0726-0763, 0765, 0767-0776, 0779-0785, 0787-0795,0797-0800, 0803-0806, 0808-0817, 0819-0829, 0831, 0833-0843, 0845, 0847-0860, 0862, 0864-0867, 0870-0879, 0881-0884, 0886-0889,0891-0895, 0897-0902, 0905-0906, 0908-0909, 0912, 0914-0921, 0924-0928, 0930-0937, 0939-0940, 0942-0957, 0959-0960, 0963, 0965-0971,0973-0974, 0977-0980, 0982-0984, 0986-0987, 0989-0991, 0993, 0995, 0999, 1001, 1003-1009, 1012-1018, 1022-1024, 1026, 1028-1032,1034-1035, 1039, 1041, 1043, 1045, 1049-1050, 1054, 1056-1057, 1060, 1063-1064, 1068, 1070, 1072, 1074-1076, 1079, 1081, 1083,1085-1086, 1088, 1093-1094, 1098, 1100, 1104-1106, 1108, 1110-1111, 1116-1117, 1120, 1124, 1127-1128, 1138, 1144-1146, 1153-1154, 1163,1165-1166, 1168, 1171, 1174, 1177-1178, 1180-1181, 1192, 1196, 1199, 1202, 1206-1207, 1209-1211, 1217-1218, 1220, 1223, 1226, 1228, 1231,1234, 1237, 1243, 1247-1248, 1252, 1263, 1266, 1272, 1274, 1281-1282, 1284, 1286, 1290-1291, 1293, 1296, 1307, 1312, 1316, 1321, 1323,1330, 1341, 1343, 1345, 1347, 1350, 1357, 1359, 1361-1363, 1370, 1372-1375, 1379, 1395, 1397, 1399, 1401, 1409, 1418, 1420-1422, 1424,1426-1427, 1432, 1435, 1439, 1448, 1450, 1457, 1459-1460, 1469, 1473-1475, 1477, 1480, 1487, 1489, 1495, 1507-1508, 1514, 1522, 1532-1533,1538, 1542, 1545, 1555, 1559, 1561, 1569, 1573, 1581, 1584-1586, 1600, 1609, 1617, 1620, 1627, 1635, 1639, 1647, 1649, 1653-1655, 1664,1667, 1669, 1671, 1674, 1679-1681, 1688, 1692, 1694, 1697-1698, 1702, 1713, 1716, 1728-1729, 1731-1732, 1736-1737, 1741, 1755, 1768, 1793,1799, 1809, 1816, 1821, 1834, 1836, 1840, 1842, 1845, 1847, 1865, 1892

Descent constraints may be automatically included in the route as part of an arrival procedure or theymay be manually entered through the MCDU F-PLN page. The aircraft will attempt to meet these aslong as DES mode is being used.The crew should be aware that an ATC "DIR TO" clearance automatically removes the requirement tocomply with the speed/altitude constraints assigned to the waypoints deleted from the F-PLN.Following the selection of HDG, DES mode will switch automatically to V/S, and altitude constraints willno longer be taken into account.




Ident.: NO-080-00005516.0002001 / 26 MAR 08Criteria: 22-1089, 22-1090, 22-1103, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1163, 22-1176, 22-1180, 22-1193, 22-1197,22-1209, 22-1217, 22-1218, 22-1219, 22-1233, 22-1235, 22-1240, P7372, P7373, P7519, P7520, P7666, SA�

7 Applicable to: MSN 0002-0021, 0031-0034, 0040-0041, 0044, 0052-0055, 0061-0067, 0076-0077, 0081-0082, 0091, 0098-0102, 0108, 0112,0115, 0118-0119, 0121, 0123-0125, 0128-0131, 0133-0134, 0136, 0143-0146, 0152-0153, 0155-0156, 0158, 0160, 0165-0166, 0171, 0173,0176-0178, 0184, 0186-0188, 0192, 0194, 0196-0199, 0203-0208, 0211, 0213-0215, 0219-0220, 0223-0224, 0226-0228, 0235-0241, 0244,0262-0264, 0270-0274, 0278, 0281-0282, 0285-0287, 0297-0300, 0306-0307, 0312, 0317-0319, 0322-0323, 0328-0329, 0337, 0339-0340,0351-0352, 0355, 0358, 0360, 0365-0367, 0370, 0372, 0377, 0380-0381, 0383, 0387-0388, 0390, 0399-0400, 0402, 0408, 0410, 0417-0418,0448, 0455, 0471, 0491, 0498, 0501, 0507, 0509, 0511, 0521, 0527, 0529, 0531, 0544, 0584, 0598, 0600, 0608, 0618, 0625, 0637, 0644, 0647,0658, 0660, 0669, 0680, 0685, 0687, 0715, 0725, 0764, 0766, 0777-0778, 0786, 0796, 0801-0802, 0807, 0818, 0830, 0832, 0844, 0846, 0861,0863, 0868-0869, 0880, 0885, 0890, 0896, 0903-0904, 0907, 0910-0911, 0913, 0922-0923, 0929, 0938, 0941, 0958, 0961-0962, 0964, 0972,0975-0976, 0981, 0985, 0988, 0992, 0994, 0996-0998, 1000, 1002, 1010-1011, 1019-1021, 1025, 1027, 1033, 1036-1038, 1040, 1042, 1044,1046-1048, 1051-1053, 1055, 1058-1059, 1061-1062, 1065-1067, 1069, 1071, 1073, 1077-1078, 1080, 1082, 1084, 1087, 1089-1092, 1095-1097,1099, 1101-1103, 1107, 1109, 1112-1115, 1118-1119, 1121-1123, 1125-1126, 1129-1137, 1139-1143, 1147-1152, 1155-1162, 1164, 1167, 1169-1170,1172-1173, 1175-1176, 1179, 1182-1191, 1193-1195, 1197-1198, 1200-1201, 1203-1205, 1208, 1212-1216, 1219, 1221-1222, 1224-1225, 1227,1229-1230, 1232-1233, 1235-1236, 1238-1242, 1244-1246, 1249-1251, 1253-1262, 1264-1265, 1267-1271, 1273, 1275-1280, 1283, 1285,1287-1289, 1292, 1294-1295, 1297-1306, 1308-1311, 1313-1315, 1317-1320, 1322, 1324-1329, 1331-1340, 1342, 1344, 1346, 1348-1349,1351-1356, 1358, 1360, 1364-1369, 1371, 1376-1378, 1380-1394, 1396, 1398, 1400, 1402-1408, 1410-1417, 1419, 1423, 1425, 1428-1431,1433-1434, 1436-1438, 1440-1447, 1449, 1451-1456, 1458, 1461-1468, 1470-1472, 1476, 1478-1479, 1481-1486, 1488, 1490-1494, 1496-1506,1509-1513, 1515-1521, 1523-1531, 1534-1537, 1539-1541, 1543-1544, 1546-1554, 1556-1558, 1560, 1562-1568, 1570-1572, 1574-1580,1582-1583, 1587-1599, 1601-1608, 1610-1616, 1618-1619, 1621-1626, 1628-1634, 1636-1638, 1640-1646, 1648, 1650-1652, 1656-1663,1665-1666, 1668, 1670, 1672-1673, 1675-1678, 1682-1687, 1689-1691, 1693, 1695-1696, 1699-1701, 1703-1712, 1714-1715, 1717-1727, 1730,1733-1735, 1738-1740, 1742-1754, 1756-1767, 1769-1792, 1794-1798, 1800-1808, 1810-1815, 1817-1820, 1823-1833, 1835, 1837-1839, 1841,1843-1844, 1846, 1848-1864, 1866-1891, 1893-3996

Descent constraints may be automatically included in the route as part of an arrival procedure or theymay be manually entered through the MCDU F-PLN page. The aircraft will attempt to meet these aslong as DES mode is being used.The crew should be aware that an ATC "DIR TO" clearance automatically removes the requirementto comply with the speed/altitude constraints assigned to the waypoints deleted from the F-PLN.However, if intermediate waypoints are relevant, e.g. for terrain awareness, then "DIR TO" withABEAMS may be an appropriate selection as constraints can be re-entered into these waypoints ifrequired.Following the selection of HDG, DES mode will switch automatically to V/S, and altitude constraints willno longer be taken into account.




10 000 FT FLOW PATTERNIdent.: NO-080-00005517.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

10 000 ft FLOW PATTERN


NORMAL OPERATIONSHOLDING


PREFACEIdent.: NO-090-00005518.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Whenever holding is anticipated, it is preferable to maintain cruise level and reduce speed to green dot,with ATC clearance, to minimize the holding requirement. As a rule of thumb, a M 0.05 decrease during1 h equates to 4 min hold. However, other operational constraints might make this option inappropriate.A holding pattern can be inserted at any point in the flight plan or may be included as part of the STAR.In either case, the holding pattern can be modified by the crew.

HOLDING SPEED AND CONFIGURATIONIdent.: NO-090-00005519.0001001 / 28 APR 08Criteria: SA�Applicable to: ALL

If a hold is to be flown, provided NAV mode is engaged and the speed is managed, an automaticspeed reduction will occur to achieve the Maximum Endurance speed when entering the holdingpattern. The Maximum Endurance speed is approximately equal to Green Dot and provides the lowesthourly fuel consumption.If the Maximum Endurance speed is greater than the ICAO or state maximum holding speed, the crewshould select flap 1 below 20 000 ft and fly S speed. Fuel consumption will be increased when holdingin anything other than clean configuration and Maximum Endurance speed.

IN THE HOLDING PATTERNIdent.: NO-090-00005520.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The holding pattern is not included in the descent path computation since the FMGS does not knowhow many patterns will be flown. When the holding fix is sequenced, the FMGS assumes that onlyone holding pattern will be flown and updates predictions accordingly. Once in the holding pattern, theVDEV indicates the vertical deviation between current aircraft altitude and the altitude at which theaircraft should cross the exit fix in order to be on the descent profile.The DES mode guides the aircraft down at -1 000 ft/min whilst in the holding pattern until reaching thecleared altitude or altitude constraint.

When in the holding pattern, LAST EXIT UTC/FUEL information is displayed on the MCDU HOLDpage. These predictions are based upon the fuel policy requirements specified on the MCDU FUELPRED page with no extra fuel, assuming the aircraft will divert. The crew should be aware that thisinformation is computed with defined assumptions e.g.:• Aircraft weight being equal to landing weight at primary destination


NORMAL OPERATIONSHOLDING


• Flight at FL 220 if distance to ALTN is less than 200 nm, otherwise FL 310 performed at maximumrange speed.

• Constant wind (as entered in alternate field of the DES WIND page).• Constant delta ISA (equal to delta ISA at primary destination)• Airway distance for a company route, otherwise direct distance.

Alternate airport may be modified using the MCDU ALTN airport page which can be accessed by alateral revision at destination.

To exit the holding pattern, the crew should select either:• IMM EXIT (The aircraft will return immediately to the hold fix, exit the holding pattern and resume its

navigation) or• HDG if radar vectors or• DIR TO if radar vectors or


NORMAL OPERATIONSAPPROACH GENERAL



This section covers general information applicable to all approach types. Techniques, which apply tospecific approach types, will be covered in dedicated chapters.All approaches are divided into three parts (initial, intermediate and final) where various drills have tobe achieved regardless of the approach type.

the approach parts and associated actions




INITIAL APPROACHIdent.: NO-100-00005522.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


NAVIGATION ACCURACY

Prior to any approach, a navigation accuracy check is to be carried out. On aircraft equipped withGPS however, no navigation accuracy check is required as long as GPS PRIMARY is available.Without GPS PRIMARY or if no GPS is installed, navigation accuracy check has to be carried out.The navigation accuracy determines which AP modes the crew should use and the type of display tobe shown on the ND.

THE FLYING REFERENCE

It is recommended to use the FD bars for ILS approaches and the FPV called "bird" with FPD fornon-precision or circling approach approaches.

APPROACH PHASE ACTIVATION

Activation of the approach phase will initiate a deceleration towards VAPP or the speed constraintinserted at FAF, whichever applies.When in NAV mode with managed speed, the approach phase activates automatically whensequencing the deceleration pseudo-waypoint . If an early deceleration is required, the approachphase can be activated on the MCDU PERF APPR page. When the approach phase is activated,the magenta target speed becomes VAPP.When in HDG mode, e.g. for radar vectoring, the crew will activate the approach phase manually.

There are two approach techniques:• The decelerated approach




• The stabilized approach

THE DECELERATED APPROACH

This technique refers to an approach where the aircraft reaches 1 000 ft in the landingconfiguration at VAPP. In most cases, this equates to the aircraft being in CONF 1 and at Sspeed at the FAF. This is the preferred technique for an ILS approach. The deceleration pseudo-waypoint assumes a decelerated approach technique.

THE STABILIZED APPROACH

This technique refers to an approach where the aircraft reaches the FAF in the landingconfiguration at VAPP. This technique is recommended for non-precision approaches. To get avaluable deceleration pseudo waypoint and to ensure a timely deceleration, the pilot should enterVAPP as a speed constraint at the FAF.

STABILIZED VERSUS DECELERATED APPROACH

F-PLN SEQUENCING

When in NAV mode, the F-PLN will sequence automatically. In HDG/TRK mode, the F-PLNwaypoints will sequence automatically only if the aircraft flies close to the programmed route.Correct F-PLN sequencing is important to ensure that the programmed missed approach route isavailable in case of go-around and to ensure correct predictions. A good cue to monitor the properF-PLN sequencing is the TO waypoint on the upper right side of the ND, which should remainmeaningful.If under radar vectors and automatic waypoint sequencing does not occur, the F-PLN will besequenced by either using the DIR TO RADIAL IN function or by deleting the FROM WPT on the F-PLN page until the next likely WPT to be over flown is displayed as the TO WPT on the ND.






NAVIGATION ACCURACY

Prior to any approach, a navigation accuracy check is to be carried out. On aircraft equipped withGPS however, no navigation accuracy check is required as long as GPS PRIMARY is available.Without GPS PRIMARY or if no GPS is installed, navigation accuracy check has to be carried out.The navigation accuracy determines which AP modes the crew should use and the type of display tobe shown on the ND.

THE FLYING REFERENCE

It is recommended to use the FD bars for ILS approaches and the FPV called "bird" with FPD fornon-precision or circling approach approaches.


Activation of the approach phase will initiate a deceleration towards VAPP or the speed constraintinserted at FAF, whichever applies.When in NAV mode with managed speed, the approach phase activates automatically whensequencing the deceleration pseudo-waypoint. If an early deceleration is required, the approachphase can be activated on the MCDU PERF APPR page. When the approach phase is activated,the magenta target speed becomes VAPP.When in HDG mode, e.g. for radar vectoring, the crew will activate the approach phase manually.

There are two approach techniques:• The decelerated approach




• The stabilized approach

THE DECELERATED APPROACH

This technique refers to an approach where the aircraft reaches 1 000 ft in the landingconfiguration at VAPP. In most cases, this equates to the aircraft being in CONF 1 and at Sspeed at the FAF. This is the preferred technique for an ILS approach. The deceleration pseudowaypoint assumes a decelerated approach technique.

THE STABILIZED APPROACH

This technique refers to an approach where the aircraft reaches the FAF in the landingconfiguration at VAPP. This technique is recommended for non-precision approaches. To get avaluable deceleration pseudo waypoint and to ensure a timely deceleration, the pilot should enterVAPP as a speed constraint at the FAF.

STABILIZED VERSUS DECELERATED APPROACH

F-PLN SEQUENCING

When in NAV mode, the F-PLN will sequence automatically. In HDG/TRK mode, the F-PLNwaypoints will sequence automatically only if the aircraft flies close to the programmed route.Correct F-PLN sequencing is important to ensure that the programmed missed approach route isavailable in case of go-around and to ensure correct predictions. A good cue to monitor the properF-PLN sequencing is the TO waypoint on the upper right side of the ND, which should remainmeaningful.If under radar vectors and automatic waypoint sequencing does not occur, the F-PLN will besequenced by either using the DIR TO RADIAL IN function or by deleting the FROM WPT on the F-PLN page until the next likely WPT to be over flown is displayed as the TO WPT on the ND.Using DIR TO or DIR TO RADIAL IN function arms the NAV mode. If NAV mode is not appropriate,pull the HDG knob to disarm it.




INTERMEDIATE APPROACHIdent.: NO-100-00005523.0001001 / 26 MAY 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


The purpose of the intermediate approach is to bring the aircraft at the proper speed, altitude andconfiguration at FAF.

DECELERATION AND CONFIGURATION CHANGE

Managed speed is recommended for the approach. Once the approach phase has been activated,the A/THR will guide aircraft speed towards the maneuvering speed of the current configuration,whenever higher than VAPP, e.g. green dot for CONFIG 0, S speed for CONFIG 1 etc.To achieve a constant deceleration and to minimize thrust variation, the crew should extend the nextconfiguration when reaching the next configuration maneuvering speed +10 kt (IAS must be lowerthan VFE next), e.g. when the speed reaches green dot +10 kt, the crew should select CONFIG 1.Using this technique, the mean deceleration rate will be approximately 10 kt/NM in level flight. Thisdeceleration rate will be twice i.e. 20 kt/NM, with the use of the speedbrakes.If selected speed is to be used to comply with ATC, the requested speed should be selected on theFCU. A speed below the manoeuvring speed of the present configuration may be selected providedit is above VLS. When the ATC speed constraint no longer applies, the pilot should push the FCUspeed selector to resume managed speed.When flying the intermediate approach in selected speed, the crew will activate the approach phase.This will ensure further proper speed deceleration when resuming managed speed; otherwise theaircraft will accelerate to the previous applicable descent phase speed.

In certain circumstances, e.g. tail wind or high weight, the deceleration rate may be insufficient. Inthis case, the landing gear may be lowered, preferably below 220 kt (to avoid gear doors overstress),




and before selection of Flap 2. Speedbrakes can also be used to increase the deceleration rate butthe crew should be aware of:• The increase in VLS with the use of speedbrakes• The limited effect at low speeds• The speed brake auto-retraction when selecting CONF 3 (A321 only) or CONF full. (Not

applicable for A318)

INTERCEPTION OF FINAL APPROACH COURSE

To ensure a smooth interception of final approach course, the aircraft ground speed should beappropriate, depending upon interception angle and distance to runway threshold. The pilot shouldrefer to applicable raw data (LOC, needles), XTK information on ND and wind component for theselection of an appropriate IAS.

If ATC provides radar vectors, the crew will sequence the F-PLN by checking that the TO WPT, onupper right hand corner of ND, is the most probable one and meaningful. This provides:• A comprehensive ND display• An assistance for lateral interception (XTK)• A meaningful vertical deviation• The go around route to be displayed.

When established on the LOC, a DIR TO should not be performed to sequence the F-PLN as thiswill result in the FMGS reverting to NAV mode. In this case, the LOC will have to be re-armed andre-captured, increasing workload unduly.The final approach course interception in NAV mode is possible if GPS is PRIMARY or if thenavigation accuracy check is positive.If ATC gives a new wind for landing, the crew will update it on MCDU PERF APPR page.Once cleared for the approach, the crew will press the APPR P/B to arm the approach modes whenapplicable.






The purpose of the intermediate approach is to bring the aircraft at the proper speed, altitude andconfiguration at FAF.

DECELERATION AND CONFIGURATION CHANGE

Managed speed is recommended for the approach. Once the approach phase has been activated,the A/THR will guide aircraft speed towards the maneuvering speed of the current configuration,whenever higher than VAPP, e.g. green dot for CONFIG 0, S speed for CONFIG 1 etc.To achieve a constant deceleration and to minimize thrust variation, the crew should extend the nextconfiguration when reaching the next configuration maneuvering speed +10 kt (IAS must be lowerthan VFE next), e.g. when the speed reaches green dot +10 kt, the crew should select CONFIG 1.Using this technique, the mean deceleration rate will be approximately 10 kt/NM in level flight. Thisdeceleration rate will be twice i.e. 20 kt/NM, with the use of the speedbrakes.If selected speed is to be used to comply with ATC, the requested speed should be selected on theFCU. A speed below the manoeuvring speed of the present configuration may be selected providedit is above VLS. When the ATC speed constraint no longer applies, the pilot should push the FCUspeed selector to resume managed speed.When flying the intermediate approach in selected speed, the crew will activate the approach phase.This will ensure further proper speed deceleration when resuming managed speed; otherwise theaircraft will accelerate to the previous applicable descent phase speed.

In certain circumstances, e.g. tail wind or high weight, the deceleration rate may be insufficient. Inthis case, the landing gear may be lowered, preferably below 220 kt (to avoid gear doors overstress),




and before selection of Flap 2. Speedbrakes can also be used to increase the deceleration rate butthe crew should be aware of:• The increase in VLS with the use of speedbrakes• The limited effect at low speeds• The speed brake auto-retraction when selecting the landing configuration. (Not applicable for

A318)


To ensure a smooth interception of final approach course, the aircraft ground speed should beappropriate, depending upon interception angle and distance to runway threshold. The pilot shouldrefer to applicable raw data (LOC, needles), XTK information on ND and wind component for theselection of an appropriate IAS.

If ATC provides radar vectors, the crew will use the DIR TO RADIAL IN-BND facility. This ensures:• A proper F-PLN sequencing• A comprehensive ND display• An assistance for lateral interception• The VDEV to be computed on reasonable distance assumptions.

However, considerations should be given the following:• A radial is to be inserted in the MCDU. In the following example, the final approach course is 90 °

corresponding to radial 270 °.• Deceleration will not occur automatically as long as lateral mode is HDG

When established on the LOC, a DIR TO should not be performed to sequence the F-PLN as thiswill result in the FMGS reverting to NAV mode. In this case, the LOC will have to be re-armed andre-captured, increasing workload unduly.The final approach course interception in NAV mode is possible if GPS is PRIMARY or if thenavigation accuracy check is positive.

use of DIR TO radial in facility

If ATC gives a new wind for landing, the crew will update it on MCDU PERF APPR page.Once cleared for the approach, the crew will press the APPR P/B to arm the approach modes whenapplicable.




FINAL APPROACHIdent.: NO-100-00005524.0001001 / 02 JUL 08Criteria: SA�Applicable to: ALL

FINAL APPROACH MODE ENGAGEMENT MONITORING

The crew will monitor the engagement of G/S* for ILS approach, FINAL for fully managed NPA orwill select the Final Path Angle (FPA) reaching FAF for selected NPA. If the capture or engagementis abnormal, the pilot will either use an appropriate selected mode or take over manually.

FINAL APPROACH MONITORING

The final approach is to be monitored through available data. Those data depends on the approachtype and the result of the navigation accuracy check.

Approach type Navigation accuracy check Data to be monitoredILS - LOC, GS deviation, DME and/or OM

Managed NPA GPS primary VDEV, XTK and F-PLNManaged NPA Non GPS PRIMARY VDEV, XTK, Needles, DME and ALTSelected NPA Accuracy check negative Needles, DME and ALT, Time

USE OF A/THR

The pilot should use the A/THR for approaches as it provides accurate speed control. The pilot willkeep the hand on the thrust levers so as to be prepared to react if needed.During final approach, the managed target speed moves along the speed scale as a function of windvariation. The pilot should ideally check the reasonableness of the target speed by referring to GSon the top left on ND. If the A/THR performance is unsatisfactory, the pilot should disconnect it andcontrol the thrust manually.If the pilot is going to perform the landing using manual thrust, the A/THR should be disconnected by1 000 ft on the final approach.

GO-AROUND ALTITUDE SETTING

When established on final approach, the go-around altitude must be set on FCU. This can be doneat any time when G/S or FINAL mode engages. However, on a selected Non Precision Approach,i.e. when either FPA or V/S is used, the missed approach altitude must only be set when the currentaircraft altitude is below the missed approach altitude, in order to avoid unwanted ALT*.

TRAJECTORY STABILIZATION

The first prerequisite for safe final approach and landing is to stabilize the aircraft on the finalapproach flight path laterally and longitudinally, in landing configuration, at VAPP speed, i.e:• Only small corrections are necessary to rectify minor deviations from stabilized conditions




• The thrust is stabilized, usually above idle, to maintain the target approach speed along thedesired final approach path

Airbus policy requires that stabilized conditions be reached at 1 000 ft above airfield elevation in IMCand 500 ft above airfield elevation in VMC.If, for any reason, one flight parameter deviates from stabilized conditions, the PNF will make acallout as stated below:

Exceedance and associated PNF calloutParameter Exceedance CalloutIAS VAPP +10 kt / -5 kt "SPEED"V/S < -1 000 ft/min "SINK RATE"Pitch attitude +10 ° / -2.5 °(1) "PITCH"Bank angle 7 ° "BANK"

Localizer 1/4 dot PFD "LOCALIZER"ILS only

Glide slopeExcess Deviation

1 dot PFD "GLIDE SLOPE"Course Excess deviation: ½ dot on PFD (or 2.5 °

(VOR)/5 ° (ADF))“COURSE”

NPA onlyAltitude at check points Deviation “ xFT HIGH (LOW)”

(1) The pitch attitude upper threshold becomes +7.5 ° or A321.

Following a PNF flight parameter exceedance call out, the suitable PF response will be:• Acknowledge the PNF callout, for proper crew coordination purposes• Take immediate corrective action to control the exceeded parameter back into the defined

stabilized conditions• Assess whether stabilized conditions will be recovered early enough prior to landing, otherwise

initiate a go-around.

REACHING THE MINIMA

Decision to land or go-around must be made at MDA/DH at the latest. Reaching the MDA/DH, atMINIMUM call out:• If appropriate visual reference can be maintained and the aircraft is properly established, continue

and land.• If not, go-around.

The MDA/DH should not be set as target altitude on the FCU. If the MDA/DH were inserted onthe FCU, this would cause a spurious ALT* when approaching MDA/DH, resulting in the approachbecoming destabilised at a critical stage.

AP DISCONNECTION

During the final approach with the AP engaged, the aircraft will be stabilised. Therefore, whendisconnecting the AP for a manual landing, the pilot should avoid the temptation to make largeinputs on the sidestick.




The pilot should disconnect the autopilot early enough to resume manual control of the aircraft andto evaluate the drift before flare. During crosswind conditions, the pilot should avoid any tendency todrift downwind.

Some common errors include:‐ Descending below the final path, and/or‐ reducing the drift too early.

VAPPIdent.: NO-100-00005525.0001001 / 26 MAR 08Criteria: 22-1077, 22-1089, 22-1103, 22-1116, 22-1130, 22-1152, 22-1163, 22-1176, 22-1180, 22-1197, 22-1218, 22-1233, P4089, P6025, P7519,P7666, P7706, SA�

5 Applicable to: MSN 0002-0068, 0073-0077, 0080-0082, 0084-0085, 0087-0091, 0095-0103, 0108-0109, 0112-0115, 0118-0134, 0136,0138-0146, 0148-0160, 0163-0171, 0173-0199, 0203-0208, 0210-0215, 0219-0266, 0270-0345, 0347-0363, 0365-0381, 0383-0384, 0386-0400,0402-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0492, 0496-0497, 0499-0501, 0503-0504,0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0534, 0537, 0539-0540, 0542-0543, 0549, 0551, 0554, 0556, 0558, 0561, 0565,0568-0569, 0571, 0573, 0575, 0579-0580, 0582, 0584, 0587, 0589-0590, 0592, 0594, 0601, 0605, 0607, 0611, 0613, 0615, 0617, 0619, 0622,0624, 0626, 0628, 0630, 0638, 0640, 0645, 0648, 0650, 0653, 0655, 0657-0659, 0661-0662, 0665, 0667, 0669, 0671, 0676, 0678, 0683, 0685,0696, 0698, 0702, 0704-0710, 0712, 0714, 0716, 0718, 0720, 0722, 0724, 0726, 0730, 0733, 0735, 0737, 0739, 0741, 0743, 0745, 0747, 0749,0751, 0754, 0758, 0760, 0762, 0764, 0766, 0770, 0772, 0778, 0780, 0786, 0791, 0795, 0799, 0801, 0803, 0805, 0807, 0814, 0818, 0820,0822, 0824, 0826, 0828, 0830, 0832, 0834, 0836, 0838-0839, 0842, 0846, 0849, 0851, 0854, 0856-0857, 0859, 0865-0866, 0872, 0874, 0876,0879, 0881, 0883, 0886, 0888, 0892, 0895, 0897, 0899-0900, 0902-0903, 0907, 0909, 0911-0912, 0914, 0916, 0918-0919, 0921, 0923, 0925,0927-0928, 0932, 0937, 0939, 0943, 0950, 0953, 0955, 0958, 0962, 0964, 0966-0967, 0969, 0973, 0975, 0977-0978, 0981, 0984, 0986, 0988,0990, 0992, 0994, 0996, 1001, 1003, 1005, 1007, 1009, 1011, 1013, 1037, 1047, 1059, 1063, 1067, 1087, 1099, 1101, 1119, 1200, 1208, 1221,1229, 1255, 1262, 1288, 1292, 1318, 1347, 1379, 1396, 1430, 1454, 1461, 1484, 1516, 1530, 1535, 1540, 1550, 1633, 1641, 1646, 1655, 1674,1694, 1736, 1789, 1793, 1809, 1812, 1973, 2054, 2061, 2082, 2092, 2104, 2143, 2225, 2242, 2248, 2347, 2391, 2998, 3099, 3147-3148, 3189

The approach speed (VAPP) is defined by the crew to perform the safest approach. It is function ofgross weight, configuration, headwind, A/THR ON/OFF, icing and downburst.

In most cases, the FMGC provides valuable VAPP on MCDU PERF APPR page, once tower wind andFLAP3 or FLAP FULL landing configuration has been inserted (VAPPfmgc = VLS +5 kt + 1/3 towerhead wind component on landing RWY in the F-PLN}).The crew can insert a lower VAPP on the MCDU APPR page, down to VLS, if landing is performedwith A/THR OFF, with no wind, no downburst and no icing.He can insert a higher VAPP in case of strong suspected downburst, but this increment is limited to15 kt above VLS.In case of strong or gusty crosswind greater than 20 kt, VAPP should be at least VLS +5 kt; the 5 ktincrement above VLS may be increased up to 15 kt at the flight crew's discretion




The crew will bear in mind that the wind entered in MCDU PERF APPR page considers the winddirection to be in the same reference as the runway direction e. g. if airport is magnetic referenced,the crew will insert magnetic wind. The wind direction provided by ATIS and tower is given in the samereference as the runway direction whereas the wind provided by VOLMET, METAR or TAF is alwaystrue referenced.VAPP is computed at predicted landing weight while the aircraft is in CRZ or DES phase. Once theapproach phase is activated, VAPP is computed using current gross weight.Managed speed should be used for final approach as it provides Ground Speed mini (GS mini)guidance, even when the VAPP has been manually inserted.

Ident.: NO-100-00005525.0004001 / 26 MAR 08Criteria: 22-1057, 22-1089, 22-1090, 22-1103, 22-1109, 22-1116, 22-1124, 22-1130, 22-1152, 22-1153, 22-1161, 22-1193, 22-1197, 22-1209,22-1217, 22-1219, 22-1235, 22-1240, K2113, K3154, P4089, P7519, P7520, P7666, P7706, P7707, SA�

6 Applicable to: MSN 0069-0072, 0078, 0083, 0086, 0093-0094, 0104, 0110-0111, 0116-0117, 0135, 0137, 0147, 0161-0162, 0172, 0200-0202,0209, 0216-0218, 0267-0269, 0346, 0364, 0382, 0385, 0401, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502,0505, 0509, 0513-0522, 0524, 0526, 0529, 0532-0533, 0535, 0538, 0541, 0544-0548, 0550, 0552-0553, 0555, 0557, 0559-0560, 0562-0564,0566-0567, 0570, 0572, 0574, 0576-0578, 0581, 0583, 0585-0586, 0588, 0591, 0593, 0595-0600, 0603-0604, 0606, 0608-0610, 0612, 0614,0616, 0618, 0620-0621, 0623, 0625, 0627, 0629, 0631-0637, 0639, 0641-0644, 0646-0647, 0649, 0651-0652, 0654, 0656, 0660, 0663-0664,0666, 0668, 0670, 0672-0675, 0677, 0679-0682, 0684, 0686-0695, 0697, 0699-0701, 0703, 0711, 0713, 0715, 0717, 0719, 0721, 0723, 0725,0727-0729, 0731-0732, 0734, 0736, 0738, 0740, 0742, 0744, 0746, 0748, 0750, 0752, 0755-0757, 0759, 0761, 0763, 0765, 0767-0769, 0771,0773-0777, 0779, 0781-0785, 0787-0790, 0792-0794, 0796-0798, 0800, 0802, 0804, 0806, 0808-0813, 0815-0817, 0819, 0821, 0823, 0825,0827, 0829, 0831, 0833, 0835, 0837, 0840-0841, 0843-0845, 0847-0848, 0850, 0852-0853, 0855, 0858, 0860-0864, 0867-0871, 0873, 0875,0877-0878, 0880, 0882, 0884-0885, 0887, 0889-0891, 0893-0894, 0896, 0898, 0901, 0904-0906, 0908, 0910, 0913, 0915, 0917, 0920, 0922,0924, 0926, 0929-0931, 0933-0936, 0938, 0940-0942, 0944-0949, 0951-0952, 0954, 0956-0957, 0959-0961, 0963, 0965, 0968, 0970-0972,0974, 0976, 0979-0980, 0982-0983, 0985, 0987, 0989, 0991, 0993, 0995, 0997-1000, 1002, 1004, 1006, 1008, 1010, 1012, 1014-1036,1038-1046, 1048-1058, 1060-1062, 1064-1066, 1068-1086, 1088-1098, 1100, 1102-1118, 1120-1199, 1201-1207, 1209-1220, 1222-1228,1230-1254, 1256-1261, 1263-1287, 1289-1291, 1293-1317, 1319-1346, 1348-1378, 1380-1395, 1397-1429, 1431-1453, 1455-1460, 1462-1483,1485-1515, 1517-1529, 1531-1534, 1536-1539, 1541-1549, 1551-1632, 1634-1640, 1642-1645, 1647-1654, 1656-1673, 1675-1693, 1695-1735,1737-1788, 1790-1792, 1794-1808, 1810-1811, 1814-1972, 1974-2053, 2055-2060, 2062-2081, 2083-2091, 2093-2103, 2105-2142, 2144-2224,2226-2241, 2243-2247, 2249-2346, 2348-2390, 2392-2997, 2999-3098, 3100-3146, 3149-3188, 3190-3996

The approach speed (VAPP) is defined by the crew to perform the safest approach. It is function ofgross weight, configuration, headwind, A/THR ON/OFF, icing and downburst.

In most cases, the FMGC provides valuable VAPP on MCDU PERF APPR page, once tower wind andFLAP3 or FLAP FULL landing configuration has been inserted (VAPPfmgc = VLS + MAX of {5 kt, 1/3tower head wind component on landing RWY in the F-PLN}).The crew can insert a lower VAPP on the MCDU APPR page, down to VLS, if landing is performedwith A/THR OFF, with no wind, no downburst and no icing.He can insert a higher VAPP in case of strong suspected downburst, but this increment is limited to15 kt above VLS.




In case of strong or gusty crosswind greater than 20 kt, VAPP should be at least VLS +5 kt; the 5 ktincrement above VLS may be increased up to 15 kt at the flight crew's discretion.The crew will bear in mind that the wind entered in MCDU PERF APPR page considers the winddirection to be in the same reference as the runway direction e. g. if airport is magnetic referenced,the crew will insert magnetic wind. The wind direction provided by ATIS and tower is given in the samereference as the runway direction whereas the wind provided by VOLMET, METAR or TAF is alwaystrue referenced.VAPP is computed at predicted landing weight while the aircraft is in CRZ or DES phase. Once theapproach phase is activated, VAPP is computed using current gross weight.Managed speed should be used for final approach as it provides Ground Speed mini (GS mini)guidance, even when the VAPP has been manually inserted.

GROUND SPEED MINIIdent.: NO-100-00005526.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


PURPOSE

The purpose of the ground speed mini function is to keep the aircraft energy level above a minimumvalue, whatever the wind variations or gusts.This allows an efficient management of the thrust in gusts or longitudinal shears. Thrust variesin the right sense, but in a smaller range (± 15 % N1) in gusty situations, which explains why it isrecommended in such situations.It provides additional but rational safety margins in shears.It allows pilots "to understand what is going on" in perturbed approaches by monitoring the targetspeed magenta bugs: when target goes up = head wind gust.




COMPUTATION

This minimum energy level is the energy the aircraft will have at landing with the expected towerwind; it is materialized by the ground speed of the aircraft at that time which is called GS mini:

GS mini = VAPP - Tower head wind component

In order to achieve that goal, the aircraft ground speed should never drop below GS mini in theapproach, while the winds are changing. Thus the aircraft IAS must vary while flying down, in orderto cope with the gusts or wind changes. In order to make this possible for the pilot or for the A/THR,the FMGS continuously computes an IAS target speed, which ensures that the aircraft ground speedis at least equal to GS mini; the FMGS uses the instantaneous wind component experienced by theaircraft:

IAS Target Speed = GS mini + Current headwind component

This target speed is limited by VAPP in case of tailwind or if instantaneous wind is lower than thetower wind.

example






PURPOSE

The purpose of the ground speed mini function is to keep the aircraft energy level above a minimumvalue, whatever the wind variations or gusts.This allows an efficient management of the thrust in gusts or longitudinal shears. Thrust variesin the right sense, but in a smaller range (± 15 % N1) in gusty situations, which explains why it isrecommended in such situations.It provides additional but rational safety margins in shears.It allows pilots "to understand what is going on" in perturbed approaches by monitoring the targetspeed magenta bugs: when target goes up = head wind gust.

COMPUTATION

This minimum energy level is the energy the aircraft will have at landing with the expected towerwind; it is materialized by the ground speed of the aircraft at that time which is called GS mini:

GS mini = VAPP - Tower head wind component

In order to achieve that goal, the aircraft ground speed should never drop below GS mini in theapproach, while the winds are changing. Thus the aircraft IAS must vary while flying down, in orderto cope with the gusts or wind changes. In order to make this possible for the pilot or for the A/THR,the FMGS continuously computes an IAS target speed, which ensures that the aircraft ground speedis at least equal to GS mini; the FMGS uses the instantaneous wind component experienced by theaircraft:

IAS Target Speed = GS mini + Current headwind component




This target speed is limited by VFE -5 in case of very strong gusts, by VAPP in case of tailwind or ifinstantaneous wind is lower than the tower wind.

example

STEEP APPROACHIdent.: NO-100-00005527.0001001 / 26 MAR 08Criteria: P9032�

9 Applicable to: MSN 3617, 3932

INTRODUCTION

A steep approach is defined as a Flight Path Angle (FPA) greater than -4.5 °. For the A318 aircraft,steep approaches have been certified up to -5.5 ° FPA and may be performed during an ILS CAT1approach, a non Precision Approach (NPA), or a visual approach.




LIMITATIONS

The only limitations are:• Max tail wind component of 5 kt at 2 000 ft, 9 kt at sea level• Max crosswind component of 26 kt (gusts included)

BEFORE DESCENT

Prior to the Top Of Descent (TOD), the flight crew will press the STEEP APPR pushbutton on theoverhead panel. This arms the steep approach function and checks the reliability of the computersrequired for the steep approach. The STEEP APPR ECAM green memo is displayed on the EWD.A stabilized approach will be programmed by inserting this modified VAPP at FAF on the MCDUFPLN page.

The VLS must be increased by 8 kt in order to compensate for the extension of spoilers 3 and 4. Theflight crew will thus manually enter the increased VAPP on the MCDU PERF APPR page, keeping inmind that:• This 8 kt increase on VAPP will be performed only after the wind has been entered.• VAPP will be updated by the crew in case of any significant wind change during the approach.

The PFD automatically display the increased VLS when the steep approach is active.

The standard approach briefing will take into account the approach particularities and highlight thefollowing aspect in particular:• Use of the STEEP APPR pushbutton• Required landing configuration and steep approach activation• Approach speed• Callouts• Simultaneous flare and thrust reduction• Go around• Failures

INITIAL/INTERMEDIATE APPROACH

When the gear is DOWN, flaps position is FULL and SPEED BRAKE lever at FULL, the flightcontrols laws, FG (AP and A/THR), EGPWS, EIS, FAC and FWC are all automatically configured forsteep approach. Steep approach function is now active.As long as the steep approach is not active, the SPEED BRAKE lever acts on spoilers 2+3+4.As soon as the steep approach is active, the speed brake lever acts only on spoilers 2+3. As aconsequence, any SPEED BRAKE lever activation during the flap extension to FULL position mayinduce a slight pitch variation.The roll capacity is maintained due to the retuning of the lateral flight control law.The ECAM LDG memo will be displayed when flaps are equal to or above configuration 2. Thispermits the landing checklist to be completed prior to beginning the final approach. The crew will




simultaneously check the STEEP APPR green memo (in the right memo zone) and the LDG memo(in the left memo zone). The landing checklist will be amended accordingly:ECAM MEMO . STEEP APPR, LDG NO BLUE

FINAL APPROACH

Engine thrust on a -5.5 ° profile, that is configured for a steep approach (i.e. with spoilers 3 and 4extended) is similar to the engines thrust on a -3 ° descent profile that is configured for a standardaircraft approach. This permits some pitch adjustment to get back on the descent profile withoutspeed increase.The stabilized approach is the preferred technique. However, a slight speed excess (e.g. 20 kt) canbe recovered while established on the -5.5 ° final profile.When the steep approach function is active, the computers and displays are tuned to take intoaccount the steep descent profile particularities. Any warnings received during the final approach(e.g. "SINK RATE" GPWS aural warning) must be considered as significant.

FLARE

The aircraft speed must be within the standard range from VAPP -5 kt to VAPP +10 kt. If not, a go-around must be initiated.

The flare height is the key point to perform a safe landing without penalizing the landing distanceperformance. To help the crew to calibrate the flare height, additional call outs based on RA areprovided:• STBY call outs triggers at 117 ft and 90 ft to remind the crew to maintain the aircraft descent path

whilst getting the crew mentally prepared to flare.• FLARE call triggers at 63 ft to remind the PF to initiate the flare.




• When the 60 ft RA display on the PFD appears, the PNF calls systematically "FLARE" (as a backup call out).

The crew will bear in mind that any GPWS alert e.g. GLIDE SLOPE will override STBY or FLAREauto call out. Therefore, the importance of the FLARE call out made by PNF at 60 ft RA must beemphasized.Due to the average pilot reaction time, the flare itself is usually initiated at around 55 ft.The side stick input for the flare is conventional, therefore greater aft sidestick input is required toarrest the vertical speed.The thrust levers are retarded to idle when initiating the flare.Just before reaching the flare height (RA signal), spoilers 3 and 4 retract to an intermediate position.This position helps to break the trajectory while maintaining a sufficient level of drag to avoid anyballooning effect. This partial retraction of the spoilers is totally transparent for the pilot.At 50 ft, the flight control law switches from normal law to flare law. The flare is normally initiatedabove 50 ft (i.e. in normal law). This provides in the first stage of the flare, if required, a good pitchauthority to break the aircraft path. However, the flare technique remains quite conventional.

ROLL OUT

The ground spoilers automatically deploy at touch down.

GO-AROUND

The go-around procedure is conventional:• The engine acceleration capability is similar to a standard approach.• Spoilers 3 and 4 automatically retract when the flight crew sets TOGA. The flight crew will confirm

the spoilers retraction by setting the SPEED BRAKE lever to RET position.

PERFORMANCE

The actual landing distance is calculated from the screen height (i.e. 55 ft for A318 in steepapproach) to a complete stop. The distance corresponding to the flight phase is reduced due toa higher descent gradient. The distance corresponding to the ground phase is increased due tothe 8 kt increase on VAPP. Therefore, landing distance performance in steep approach is slightlygreater than a 3 ° approach.

FAILURE

Two additional F/CTL alerts are provided with the steep approach capability: "F/CTL STEEP APPRLOST" or "F/CTL STEEP APPR FAULT".If one of these two F/CTL alerts is triggered below 2 000 ft, the flight crew must perform a go-aroundunless it is safer for the flight crew to perform an immediate landing.


NORMAL OPERATIONSILS APPROACH


PREFACEIdent.: NO-110-00005529.0001001 / 26 MAY 08Criteria: SA�Applicable to: ALL

This chapter deals with some characteristics of the ILS approach. Recommendations mentioned inAPPROACH GENERAL chapter apply.For CAT1 ILS, the crew will insert DA/DH values into MDA (or MDH if QFE function is available) field onthe MCDU PERF APPR page, since these values are baro referenced.For CATII or CATIII ILS, the crew will insert DH into DH field on MCDU PERF APPR page, since thisvalue is a radio altitude referenced.

INITIAL APPROACHIdent.: NO-110-00005531.0001001 / 17 JUN 08Criteria: 34-1162, 34-1167, P3345, P5168, P6183, SA�

1 Applicable to: MSN 0029-0031, 0034-0042, 0045-0059, 0064-0086, 0089-0099, 0103-0104, 0109-0112, 0116-0127, 0132, 0135, 0137-0142,0147-0154, 0157, 0159-0169, 0171-0172, 0174-0175, 0178-0183, 0185, 0189-0195, 0197-0198, 0200-0202, 0205-0206, 0208-0210, 0216-0218,0221-0222, 0225, 0229-0234, 0242-0243, 0247-0263, 0265, 0267-0269, 0272-0273, 0275-0277, 0279-0284, 0288-0299, 0301-0302, 0304-0311,0313-0322, 0324, 0326-0327, 0329-0336, 0338-0347, 0349-0351, 0353-0355, 0357-0363, 0366-0373, 0376, 0378-0382, 0384, 0386-0399,0401-0408, 0410-0411, 0414-0432, 0435-0457, 0460-0465, 0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0490, 0492, 0496,0499-0500, 0503-0504, 0506, 0508, 0510-0512, 0523, 0525, 0527-0528, 0538-0540, 0542-0543, 0546, 0551, 0555-0556, 0558, 0561, 0568,0571-0572, 0579, 0584, 0587, 0589-0590, 0592, 0594, 0601, 0605-0607, 0611, 0613, 0617, 0619, 0624, 0626, 0628, 0630, 0634, 0636,0638-0640, 0645, 0648-0650, 0655-0656, 0670-0672, 0676, 0678, 0682-0683, 0686, 0688, 0690-0691, 0693, 0695, 0697, 0702, 0707,0711, 0714, 0716, 0719, 0721, 0724, 0726, 0728, 0730-0733, 0735-0736, 0740-0742, 0746-0748, 0751-0752, 0756-0757, 0759-0760, 0762,0766, 0769-0770, 0772-0773, 0778-0780, 0783-0786, 0788, 0791, 0795, 0798-0801, 0803-0804, 0807, 0813-0814, 0817-0818, 0820, 0822,0824-0826, 0828-0832, 0834, 0836, 0840, 0842-0843, 0845-0847, 0850-0851, 0856-0858, 0862, 0865-0867, 0871, 0873-0874, 0876, 0879,0882-0883, 0886, 0888-0889, 0893, 0898, 0902-0903, 0907, 0911-0912, 0916, 0918, 0921, 0923-0925, 0931, 0937, 0944, 0948, 0952-0953,0955, 0962, 0964-0965, 0978, 0980-0981, 0989, 0996, 1001, 1003, 1011, 1022, 1032, 1037, 1043, 1049-1050, 1056, 1058, 1062, 1064,1075-1076, 1079, 1083, 1085, 1088, 1110-1111, 1116-1117, 1129, 1149, 1164, 1166-1167, 1178, 1191, 1223, 1230, 1234, 1249, 1274, 1281, 1284,1323-1325, 1346, 1350, 1373-1375, 1392, 1395, 1397, 1414, 1434, 1453, 1456, 1483, 1498, 1501, 1520, 1535, 1543, 1549, 1567, 1570, 1582,1633, 1641, 1646, 1659, 1662, 1683, 1685, 1693, 1709, 1714, 1738, 1746, 1752, 1766, 1774, 1789, 1796, 1800, 1810, 1812, 1815, 1819-1820,1824, 1833, 1839, 1870, 1875, 1897, 1923, 1959, 1976, 1982, 1990, 2002, 2013, 2026, 2028, 2039, 2047, 2082, 2087, 2092, 2095, 2369, 2373,2464, 2474, 2618, 2641

NAVIGATION ACCURACY

The navigation accuracy will be monitored throughout the approach and the crew will be prepared tomodify the approach strategy if required. If NAV ACCURACY DOWNGRAD message is displayed onND, the crew will use raw data to crosscheck navigation accuracy.Navigation accuracy determines which autopilot modes the flight crew should use, and the type ofdisplays to be shown on the ND.

NDNAVIGATION ACCURACYPF PNF

AP/FD mode

NAV ACCUR HIGHNAV ACCUR HIGH

ARC or ROSE NAV with navaid raw data NAV





Continued from previous pageNAV ACCUR LOW and NAVACCURACY check ≤1 nm

GPS PRIMARY LOST and NAV ACCURLOW and NAV ACCURACY check > 1 nm

Aircraft flying within un-reliable radio navaid area

ROSE ILS ARC or ROSE NAVor ROSE ILS withnavaid raw data

HDG or TRK

FLYING REFERENCE

The crew will select HDG V/S on the FCU i.e. "bird" off.


For a standard ILS, the crew should plan a decelerated approach. However, if the G/S angle isgreater than 3.5 ° or if forecast tail wind at landing exceeds 10 kt (if permitted by the AFM), astabilized approach is recommended.If FAF is at or below 2 000 ft AGL and if deceleration is carried out using selected speed, the crewshould plan a deceleration in order to be able to select CONFIG. 2 one dot below the G/S.

MISCELLANEOUS

The ILS or LS PB is to be checked pressed in the first stage of the approach. The crew will checkthat• LOC and GS scales and deviations are displayed on PFD• IDENT is properly displayed on the PFD. If no or wrong ident displayed, the crew will check the

audio ident.




Ident.: NO-110-00005531.0006001 / 17 JUN 08Criteria: 34-1119, 34-1132, 34-1143, 34-1155, 34-1162, 34-1186, 34-1207, 34-1208, 34-1232, 34-1406, 34-1424, 34-1425, P3345, P4085, P4391,P5168, P6054, P6183, SA�

2 Applicable to: MSN 0002-0021, 0033, 0043-0044, 0061-0063, 0087-0088, 0100-0102, 0108, 0113-0115, 0128-0131, 0133-0134, 0136,0143-0146, 0155-0156, 0158, 0170, 0173, 0176-0177, 0184, 0186-0188, 0196, 0199, 0203-0204, 0207, 0211-0215, 0219-0220, 0223-0224,0226-0228, 0235-0241, 0244-0246, 0264, 0266, 0270, 0274, 0278, 0285-0287, 0300, 0303, 0312, 0323, 0325, 0328, 0337, 0348, 0352, 0356,0364-0365, 0375, 0377, 0383, 0385, 0400, 0409, 0412-0413, 0434, 0458-0459, 0466, 0468, 0473-0474, 0477, 0484, 0488, 0491, 0493-0495,0497-0498, 0501-0502, 0505, 0507, 0509, 0513-0522, 0524, 0526, 0529-0537, 0541, 0544-0545, 0548-0550, 0552-0554, 0557, 0559-0560,0562-0567, 0569-0570, 0573-0578, 0580-0583, 0585-0586, 0588, 0591, 0593, 0595-0600, 0603-0604, 0608-0610, 0612, 0614-0616, 0618,0620-0623, 0625, 0627, 0629, 0631-0633, 0635, 0637, 0641-0644, 0646-0647, 0651-0654, 0657-0669, 0673-0675, 0677, 0679-0681,0684-0685, 0687, 0689, 0692, 0694, 0696, 0698-0701, 0703-0706, 0709-0710, 0712-0713, 0715, 0717-0718, 0720, 0722-0723, 0725, 0727,0729, 0734, 0737-0739, 0743-0745, 0749-0750, 0754-0755, 0758, 0761, 0763-0765, 0767-0768, 0771, 0774-0777, 0781-0782, 0787, 0790,0792-0794, 0796-0797, 0802, 0805-0806, 0808-0812, 0815-0816, 0819, 0821, 0823, 0827, 0833, 0835, 0837-0839, 0841, 0844, 0848-0849,0852-0855, 0859-0861, 0863-0864, 0868-0870, 0872, 0875, 0877-0878, 0880-0881, 0884-0885, 0887, 0890-0892, 0894-0897, 0899-0901,0904-0906, 0908-0910, 0913-0915, 0917, 0919-0920, 0922, 0926-0930, 0932-0936, 0938-0943, 0945-0947, 0949-0951, 0954, 0956-0961, 0963,0966-0977, 0979, 0982-0988, 0990-0995, 0997-1000, 1002, 1004-1010, 1012-1021, 1023-1031, 1033-1036, 1038-1042, 1044-1048, 1051-1055,1057, 1059-1061, 1063, 1065-1074, 1077-1078, 1080-1082, 1084, 1086-1087, 1089-1109, 1112-1115, 1118-1128, 1130-1148, 1150-1163, 1165,1168-1177, 1179-1190, 1192-1222, 1224-1229, 1231-1233, 1235-1248, 1250-1273, 1275-1280, 1282-1283, 1285-1322, 1326-1345, 1347-1349,1351-1372, 1376-1391, 1393-1394, 1396, 1398-1413, 1415-1433, 1435-1452, 1454-1455, 1457-1482, 1484-1497, 1499-1500, 1502-1519,1521-1534, 1536-1542, 1544-1548, 1550-1566, 1568-1569, 1571-1581, 1583-1632, 1634-1640, 1642-1645, 1647-1658, 1660-1661, 1663-1682,1684, 1686-1692, 1694-1708, 1710-1713, 1715-1737, 1739-1745, 1747-1751, 1753-1765, 1767-1773, 1775-1788, 1790-1795, 1797-1799,1801-1809, 1811, 1814, 1816-1818, 1821-1823, 1825-1832, 1834-1838, 1840-1869, 1871-1874, 1876-1896, 1898-1922, 1924-1958, 1960-1975,1977-1981, 1983-1989, 1991-2001, 2003-2012, 2014-2024, 2027, 2029-2038, 2040-2046, 2048-2081, 2083-2086, 2088-2091, 2093-2094,2096-2368, 2370-2372, 2374-2463, 2465-2473, 2475-2617, 2619-2640, 2642-3996

NAVIGATION ACCURACY

When GPS PRIMARY is available, no NAV ACCURACY monitoring is required. When GPSPRIMARY is lost the crew will check on MCDU PROG page that the required navigation accuracy isappropriate. If NAV ACCURACY DOWNGRAD is displayed, the crew will use raw data for navigationaccuracy check. The navigation accuracy determines which AP modes the crew should use and thetype of display to be shown on the ND.

NDNAVIGATION ACCURACYPF PNF

AP/FD mode

GPS PRIMARYNAV ACCUR HIGH

NAV ACCUR LOW and NAVACCURACY check ≤1 nm

ARC or ROSE NAV with navaid raw data NAV

GPS PRIMARY LOST and NAV ACCURLOW and NAV ACCURACY check >1 nm

GPS PRIMARY LOST and Aircraft fly-ing within unreliable radio navaid area

ROSE ILS ARC or ROSE NAVor ROSE ILS withnavaid raw data

HDG or TRK

FLYING REFERENCE

The crew will select HDG V/S on the FCU i.e. "bird" off.





For a standard ILS, the crew should plan a decelerated approach. However, if the G/S angle isgreater than 3.5 ° or if forecast tail wind at landing exceeds 10 kt (if permitted by the AFM), astabilized approach is recommended.If FAF is at or below 2 000 ft AGL and if deceleration is carried out using selected speed, the crewshould plan a deceleration in order to be able to select CONFIG. 2 one dot below the G/S.

MISCELLANEOUS

The ILS or LS PB is to be checked pressed in the first stage of the approach. The crew will checkthat• LOC and GS scales and deviations are displayed on PFD• IDENT is properly displayed on the PFD. If no or wrong ident displayed, the crew will check the

audio ident.

INTERMEDIATE APPROACHIdent.: NO-110-00005533.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL


When cleared for the ILS, the APPR pb should be pressed. This arms the approach mode andLOC and GS are displayed in blue on the FMA. At this stage the second AP, if available, should beselected.If the ATC clears for a LOC capture only, the crew will press LOC p/b on the FCU.If the ATC clears for approach at a significant distance, e.g. 30 nm, the crew should be aware thatthe G/S may be perturbed and CAT 1 will be displayed on FMA till a valid Radio Altimeter signal isreceived.

FINAL APPROACHIdent.: NO-110-00005534.0001001 / 03 JUL 08Criteria: SA�Applicable to: ALL

GLIDE SLOPE INTERCEPTION FROM ABOVE

The following procedure should only be applied when established on the localizer. There are anumber of factors which might lead to a glide slope interception from above. In such a case, thecrew must react without delay to ensure the aircraft is configured for landing before 1 000 ft AAL.In order to get the best rate of descent when cleared by ATC and below the limiting speeds, thecrew should lower the landing gear and select CONF 2. Speedbrakes may also be used, notingthe considerations detailed in the sub-section "Deceleration and configuration change" earlier in




this chapter. The recommended target speed for this procedure is VFE 2 - 5 kt. When cleared tointercept the glide slope, the crew should:• Press the APPR pb on FCU and confirm G/S is armed.• Select the FCU altitude above aircraft altitude to avoid unwanted ALT*.• Select V/S 1 500 ft/min initially. V/S in excess of 2 000 ft/min will result in the speed increasing

towards VFE

A/C high above G/S - recommended g/s capture technique

It is vital to use V/S rather than OP DES to ensure that the A/THR is in speed mode rather thanIDLE mode. The rate of descent will be carefully monitored to avoid exceeding VFE . Whenapproaching the G/S, G/S*will engage. The crew will monitor the capture with raw data (pitch andG/S deviation). The go-around altitude will be set on the FCU and speed reduced so as to beconfigured for landing by 1 000 ft.In such a situation, taking into account the ground obstacles and if ATC permits, it may beappropriate to carry out a 360 °turn before resuming the approach.

MISCELLANEOUS

Close to the ground, avoid large down corrections. Give priority to attitude and sink rate. (Refer toNO-160 TAIL STRIKE AVOIDANCE).In case of a double receiver failure, the red LOC/GS flags are displayed, ILS scales are removed,the AP trips off and the FDs revert to HDG/VS mode.In case of an ILS ground transmitter failure, the AP/FD with LOC/GS modes will remain ON. This isbecause such a failure is commonly transient. In such a case, ILS scales and FD bars are flashing.If R/A height is below 200 ft, the red LAND warning is triggered. If this failure lasts more than severalseconds or in case of AUTOLAND warning, the crew must perform a go-around.

ILS RAW DATAIdent.: NO-110-00005536.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

INITIAL APPROACH

FLYING REFERENCE

The "bird" is to be used as the flying reference.





The approach technique is the stabilized approach.

INTERMEDIATE APPROACH

The TRK index will be set to the ILS course and, once established on the LOC, the tail of the birdshould be coincident with the TRK index. This method allows accurate LOC tracking taking intoaccount the drift.Should the LOC deviate, the pilot will fly the bird in the direction of the LOC index, and when re-established on the LOC, set the tail of the bird on the TRK index again. If there is further LOCdeviation, a slight IRS drift should be suspected. The bird is computed out of IRS data. Thus, it maybe affected by IRS data drift amongst other TRK. A typical TRK error at the end of the flight is 1 ° to2 °.The ILS course pointer and the TRK diamond are also displayed on PFD compass.

FINAL APPROACH

When ½ dot below the G/S, the pilot should initiate the interception of the G/S by smoothly flying theFPV down to the glide path angle. The bird almost sitting on the -5 ° pitch scale on PFD, provides a-3 ° flight path angle. Should the G/S deviate, the pilot will make small corrections in the direction ofthe deviation and when re-established on the G/S, reset the bird to the G/S angle.


NORMAL OPERATIONSNON PRECISION APPROACH



This chapter deals with some characteristics of the Non Precision Approach (NPA). Recommendationsmentioned Refer to NO-100 PREFACE.

NPA are defined as:• VOR approach• NDB approach• LOC, LOC-BC approach• R-NAV approach.

APPROACH STRATEGYIdent.: NO-120-00005540.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The overall strategy of NPA completion is to fly it "ILS alike" with the same mental image orrepresentation and similar procedure. Instead of being referred to an ILS beam, the AP/FD guidancemodes and associated monitoring data are referred to the FMS F-PLN consolidated by raw data. LOConly approach is the exception where LOC mode and localizer scale are to be used. This explains whythe crew must ensure that the FMS data is correct, e.g. FMS accuracy, F-PLN (lateral and vertical) andproper leg sequencing.The use of AP is recommended for all non-precision approaches as it reduces crew workload andfacilitates monitoring the procedure and flight path.

LIMITATIONSIdent.: NO-120-00005541.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Lateral and vertical managed guidance (FINAL APP) can be used provided the following conditions aremet:• The approach is defined in the navigation database• The approach has been crosschecked by the crew with the published procedure• The final approach is not modified by the crew.

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the followingmodes: FINAL APP, NAV V/S, NAV/FPA. Only FD use is permitted (Refer to FCOM/LIM-22-10 USE OF




NAV AND FINAL APP MODES FOR NON-PRECISION APPROACH). In others words, if the use of theautopilot is preferred, its use will be limited to TRK/FPA or HDG/VS modes.

INITIAL APPROACHIdent.: NO-120-00005543.0001001 / 05 DEC 08Criteria: 34-1162, 34-1167, P3345, P5168, P6183, SA�

1 Applicable to: MSN 0029-0031, 0034-0042, 0045-0059, 0064-0086, 0089-0099, 0103-0104, 0109-0112, 0116-0127, 0132, 0135, 0137-0142,0147-0154, 0157, 0159-0169, 0171-0172, 0174-0175, 0178-0183, 0185, 0189-0195, 0197-0198, 0200-0202, 0205-0206, 0208-0210, 0216-0218,0221-0222, 0225, 0229-0234, 0242-0243, 0247-0263, 0265, 0267-0269, 0272-0273, 0275-0277, 0279-0284, 0288-0299, 0301-0302, 0304-0311,0313-0322, 0324, 0326-0327, 0329-0336, 0338-0347, 0349-0351, 0353-0355, 0357-0363, 0366-0373, 0376, 0378-0382, 0384, 0386-0399,0401-0408, 0410-0411, 0414-0432, 0435-0457, 0460-0465, 0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487, 0489-0490, 0492, 0496,0499-0500, 0503-0504, 0506, 0508, 0510-0512, 0523, 0525, 0527-0528, 0538-0540, 0542-0543, 0546, 0551, 0555-0556, 0558, 0561, 0568,0571-0572, 0579, 0584, 0587, 0589-0590, 0592, 0594, 0601, 0605-0607, 0611, 0613, 0617, 0619, 0624, 0626, 0628, 0630, 0634, 0636,0638-0640, 0645, 0648-0650, 0655-0656, 0670-0672, 0676, 0678, 0682-0683, 0686, 0688, 0690-0691, 0693, 0695, 0697, 0702, 0707,0711, 0714, 0716, 0719, 0721, 0724, 0726, 0728, 0730-0733, 0735-0736, 0740-0742, 0746-0748, 0751-0752, 0756-0757, 0759-0760, 0762,0766, 0769-0770, 0772-0773, 0778-0780, 0783-0786, 0788, 0791, 0795, 0798-0801, 0803-0804, 0807, 0813-0814, 0817-0818, 0820, 0822,0824-0826, 0828-0832, 0834, 0836, 0840, 0842-0843, 0845-0847, 0850-0851, 0856-0858, 0862, 0865-0867, 0871, 0873-0874, 0876, 0879,0882-0883, 0886, 0888-0889, 0893, 0898, 0902-0903, 0907, 0911-0912, 0916, 0918, 0921, 0923-0925, 0931, 0937, 0944, 0948, 0952-0953,0955, 0962, 0964-0965, 0978, 0980-0981, 0989, 0996, 1001, 1003, 1011, 1022, 1032, 1037, 1043, 1049-1050, 1056, 1058, 1062, 1064,1075-1076, 1079, 1083, 1085, 1088, 1110-1111, 1116-1117, 1129, 1149, 1164, 1166-1167, 1178, 1191, 1223, 1230, 1234, 1249, 1274, 1281, 1284,1323-1325, 1346, 1350, 1373-1375, 1392, 1395, 1397, 1414, 1434, 1453, 1456, 1483, 1498, 1501, 1520, 1535, 1543, 1549, 1567, 1570, 1582,1633, 1641, 1646, 1659, 1662, 1683, 1685, 1693, 1709, 1714, 1738, 1746, 1752, 1766, 1774, 1789, 1796, 1800, 1810, 1812, 1815, 1819-1820,1824, 1833, 1839, 1870, 1875, 1897, 1923, 1959, 1976, 1982, 1990, 2002, 2013, 2026, 2028, 2039, 2047, 2082, 2087, 2092, 2095, 2369, 2373,2464, 2474, 2618, 2641

2 NAVIGATION ACCURACY

The navigation accuracy check is most essential since it determines• The AP/FD guidance mode to be used• The ND display mode to be used• Which raw data which are to be used.

NDNAVIGATION ACCURACY Approach guidancePF PNF

AP/FD mode

NAV ACCUR HIGHNAV ACCUR LOW and NAVACCURACY checK ≤1 nm

Managed(3)

or SelectedARC or ROSE NAV (1)

with navaid raw dataNAV-FPA or APP-

NAV/FINAL (3)

NAV ACCUR LOW and NAVACCURACY check > 1 nm

GPS PRIMARY LOST and aircraft flyingwithin unreliable radio navaid area

Selected ROSE VOR (2) ARC or ROSENAV or ROSEVOR (2) with

navaid raw data

TRK-FPA

(1) For VOR approach, one pilot may select ROSE VOR(2) For LOC approach, select ROSE ILS(3) The managed vertical guidance can be used provided the above limitations are observed.




Should a NAV ACCY DNGRADED message is displayed before a managed non-precision approach,the crew should proceed as follow:• Cross-check the navigation accuracy with raw data• If positive, continue managed approach. See (*)• If negative, revert to selected approach with raw data.

(*) If HIGH accuracy is lost on one FMGC, the approach can be continued with the AP/FDassociated to the other FMGC.

FLYING REFERENCE

The "bird" is to be used as the flying reference


The stabilized approach technique is recommended. The crew will set VAPP as a speed constraintat FAF in order to get a meaningful deceleration pseudo waypoint.

Ident.: NO-120-00005543.0002001 / 05 DEC 08Criteria: 34-1119, 34-1132, 34-1143, 34-1155, 34-1162, 34-1186, 34-1207, 34-1208, 34-1232, 34-1406, 34-1424, 34-1425, P3345, P4085, P4391,P5168, P6054, P6183, SA�

3 Applicable to: MSN 0002-0021, 0033, 0043-0044, 0061-0063, 0087-0088, 0100-0102, 0108, 0113-0115, 0128-0131, 0133-0134, 0136,0143-0146, 0155-0156, 0158, 0170, 0173, 0176-0177, 0184, 0186-0188, 0196, 0199, 0203-0204, 0207, 0211-0215, 0219-0220, 0223-0224,0226-0228, 0235-0241, 0244-0246, 0264, 0266, 0270, 0274, 0278, 0285-0287, 0300, 0303, 0312, 0323, 0325, 0328, 0337, 0348, 0352, 0356,0364-0365, 0375, 0377, 0383, 0385, 0400, 0409, 0412-0413, 0434, 0458-0459, 0466, 0468, 0473-0474, 0477, 0484, 0488, 0491, 0493-0495,0497-0498, 0501-0502, 0505, 0507, 0509, 0513-0522, 0524, 0526, 0529-0537, 0541, 0544-0545, 0548-0550, 0552-0554, 0557, 0559-0560,0562-0567, 0569-0570, 0573-0578, 0580-0583, 0585-0586, 0588, 0591, 0593, 0595-0600, 0603-0604, 0608-0610, 0612, 0614-0616, 0618,0620-0623, 0625, 0627, 0629, 0631-0633, 0635, 0637, 0641-0644, 0646-0647, 0651-0654, 0657-0669, 0673-0675, 0677, 0679-0681,0684-0685, 0687, 0689, 0692, 0694, 0696, 0698-0701, 0703-0706, 0709-0710, 0712-0713, 0715, 0717-0718, 0720, 0722-0723, 0725, 0727,0729, 0734, 0737-0739, 0743-0745, 0749-0750, 0754-0755, 0758, 0761, 0763-0765, 0767-0768, 0771, 0774-0777, 0781-0782, 0787, 0790,0792-0794, 0796-0797, 0802, 0805-0806, 0808-0812, 0815-0816, 0819, 0821, 0823, 0827, 0833, 0835, 0837-0839, 0841, 0844, 0848-0849,0852-0855, 0859-0861, 0863-0864, 0868-0870, 0872, 0875, 0877-0878, 0880-0881, 0884-0885, 0887, 0890-0892, 0894-0897, 0899-0901,0904-0906, 0908-0910, 0913-0915, 0917, 0919-0920, 0922, 0926-0930, 0932-0936, 0938-0943, 0945-0947, 0949-0951, 0954, 0956-0961, 0963,0966-0977, 0979, 0982-0988, 0990-0995, 0997-1000, 1002, 1004-1010, 1012-1021, 1023-1031, 1033-1036, 1038-1042, 1044-1048, 1051-1055,1057, 1059-1061, 1063, 1065-1074, 1077-1078, 1080-1082, 1084, 1086-1087, 1089-1109, 1112-1115, 1118-1128, 1130-1148, 1150-1163, 1165,1168-1177, 1179-1190, 1192-1222, 1224-1229, 1231-1233, 1235-1248, 1250-1273, 1275-1280, 1282-1283, 1285-1322, 1326-1345, 1347-1349,1351-1372, 1376-1391, 1393-1394, 1396, 1398-1413, 1415-1433, 1435-1452, 1454-1455, 1457-1482, 1484-1497, 1499-1500, 1502-1519,1521-1534, 1536-1542, 1544-1548, 1550-1566, 1568-1569, 1571-1581, 1583-1632, 1634-1640, 1642-1645, 1647-1658, 1660-1661, 1663-1682,1684, 1686-1692, 1694-1708, 1710-1713, 1715-1737, 1739-1745, 1747-1751, 1753-1765, 1767-1773, 1775-1788, 1790-1795, 1797-1799,1801-1809, 1811, 1814, 1816-1818, 1821-1823, 1825-1832, 1834-1838, 1840-1869, 1871-1874, 1876-1896, 1898-1922, 1924-1958, 1960-1975,1977-1981, 1983-1989, 1991-2001, 2003-2012, 2014-2024, 2027, 2029-2038, 2040-2046, 2048-2081, 2083-2086, 2088-2091, 2093-2094,2096-2368, 2370-2372, 2374-2463, 2465-2473, 2475-2617, 2619-2640, 2642-3996

4 NAVIGATION ACCURACY

The navigation accuracy check is most essential since it determines• The AP/FD guidance mode to be used• The ND display mode to be used• Which raw data which are to be used.




NDNAVIGATION ACCURACY Approach guidancePF PNF

AP/FD mode

GPS PRIMARYNAV ACCUR HIGH

NAV ACCUR LOW and NAVACCURACY checK ≤1 nm

Managed (3)

or SelectedARC or ROSE NAV (1)

with navaid raw dataNAV-FPA or APP-

NAV/FINAL (3)

GPS PRIMARY LOST andNAV ACCUR LOW and NAVACCURACY check > 1 nm

GPS PRIMARY LOST and aircraft flyingwithin unreliable radio navaid area

Selected ROSE VOR (2) ARC or ROSENAV or ROSE

VOR (2)withnavaid raw data

TRK-FPA

(1) For VOR approach, one pilot may select ROSE VOR(2) For LOC approach, select ROSE ILS(3) The managed vertical guidance can be used provided the approach coding in the navigation database has been

validated.

Should a NAV ACCY DNGRADED or a GPS PRIMARY LOST message is displayed before amanaged non-precision approach, the crew should proceed as follow:

Message VOR, ADF, VOR/DME approach GPS approachGPS PRIMARY LOST Interrupt the approach

NAV ACCY DNGRADEDCross-check the navigation accuracy:

If positive, continuemanaged approach (1)

If negative, revert to select-ed approach with raw data.

-

(1) If HIGH accuracy is lost on one FMGC, the approach can be continued with the AP/FD associated to the other FMGC.

FLYING REFERENCE

The "bird" is to be used as the flying reference


The stabilized approach technique is recommended. The crew will set VAPP as a speed constraintat FAF in order to get a meaningful deceleration pseudo waypoint.




INTERMEDIATE APPROACHIdent.: NO-120-00005545.0001001 / 26 MAR 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�



It is essential to have a correct F-PLN in order to ensure proper final approach guidance. Indeedthe NAV and APPR NAV modes are always guiding the aircraft along the F-PLN active leg and themanaged vertical mode ensures VDEV =0, VDEV, being computed along the remaining F-PLN todestination. Hence, the crew will monitor the proper sequencing of the F-PLN, more specifically ifHDG mode is selected, by checking that the TO WPT, on upper right hand corner of ND, is the mostprobable one and meaningful.

F-PLN sequence in approach

When ATC gives radar vector and clears for final approach course interception, the crew will:‐ For managed approach

• Select HDG according to ATC• Select APPR p/b on FCU• Check on FMA the final approach mode engagement




If the green solid line intercepts the F-PLN active leg (1), this creates an INTERCPT point withfinal approach axis. APP NAV will engage when intercepting the final approach course.If the green solid line intercepts the PRE NAV engagement path (2), APP NAV engages whenintercepting the final approach course. The PRE NAV engagement path is at least 1 nm and maybe longer depending on aircraft speed.HDG or TRK may be used to smooth the final approach course interception. When close to thefinal approach course, DIR TO function may be used.If the green solid line does not intercept the PRE NAV engagement path (3), APP NAV will notengage.XTK is related to the beam and the ND gives a comprehensive display.Additionally, the VDEV becomes active and represents the vertical deviation, which may includea level segment. The VDEV/brick scale will only be displayed if ILS or LS pb is not pressed. If theILS or LS pb is pressed by mistake, the V/DEV will flash in amber on the PFD.

‐ For selected approach• Select appropriate TRK on FCU in order to establish final course tracking with reference to raw

data. When established on the final course, the selected track will compensate for drift.

The final approach course interception will be monitored through applicable raw data.







It is essential to have a correct F-PLN in order to ensure proper final approach guidance. Indeedthe NAV and APPR NAV modes are always guiding the aircraft along the F-PLN active leg and themanaged vertical mode ensures VDEV =0, VDEV, being computed along the remaining F-PLN todestination. Hence, the crew will monitor the proper sequencing of the F-PLN, more specifically ifHDG mode is selected, by checking that the TO WPT, on upper right hand corner of ND, is the mostprobable one and meaningful.

F-PLN sequence in approach

If ATC gives radar vectors for final approach course interception, the crew will use DIR TO FAFwith RADIAL INBND facility. This creates an ILS alike beam which will be intercepted by NAV andAPPR NAV modes. Additionally, the VDEV is realistic, XTK is related to the beam and the ND givesa comprehensive display.




F-PLN in approach

When cleared for final approach course interception, the pilot will either‐ For managed approach

Press APPR p/b on FCU. On the FMA, APP NAV becomes active and FINAL becomes armed.The VDEV or "brick" scale becomes active and represents the vertical deviation, which mayinclude a level segment. The VDEV/brick scale will only be displayed if ILS or LS pb is notpressed. If the ILS or LS pb is pressed by mistake, the V/DEV will flash in amber on the PFD

‐ For selected approachSelect adequate TRK on FCU in order to establish final course tracking with reference to rawdata. When established on the final course, the selected track will compensate for drift.

The final approach course interception will be monitored through applicable raw data.

FINAL APPROACHIdent.: NO-120-00005546.0001001 / 26 MAR 08Criteria: SA�

7 Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0113-0114, 0163-0166,0168-0169, 0178-0182, 0189-0190, 0193-0195, 0198, 0221, 0225, 0230, 0232, 0243, 0247, 0249-0252, 0256-0257, 0259-0261, 0275-0276,0280, 0289, 0291-0292, 0294-0296, 0304, 0308, 0314, 0316-0317, 0320-0322, 0326-0327, 0332, 0334-0336, 0338, 0343, 0347, 0349,0351, 0353-0354, 0357, 0361-0363, 0366, 0368-0369, 0371, 0373, 0376, 0379, 0386, 0391-0394, 0396-0398, 0405-0406, 0411, 0414-0416,0422-0425, 0428-0432, 0437, 0440-0441, 0443-0444, 0446-0449, 0451, 0453, 0455, 0461, 0467, 0469, 0471, 0476, 0478, 0480

It is essential that the crew does not modify the final approach in the MCDU FPLN page.

The final approach will be flown either• Managed or• Selected

MANAGED

For a managed approach, APP NAV FINAL becomes active and the FM manages both lateral andvertical guidance. The crew will monitor the final approach using• Start of descent blue symbol on ND• FMA on PFD• VDEV, XTK, F-PLN on ND with GPS PRIMARY




• VDEV, XTK, F-PLN confirmed by needles, distance/altitude

If APP NAV FINAL does not engage at start of descent, the crew will select FPA convergent to thefinal path so as to fly with VDEV=0. Once VDEV=0, the crew may try to re-engage APPR.In some NPAs, the final approach flies an "idle descent" segment from one altitude constraint toanother, followed by a level segment. This is materialized by a magenta level off symbol on NDfollowed by a blue start of descent.

Final approach trajectory with idle descent segment

SELECTED

For a selected approach, the Final Path Angle (FPA) should be preset on the FCU 1 nm prior to theFAF at the latest. A smooth interception of the final approach path can be achieved by pulling theFPA selector 0.2 nm prior to the FAF.If GPS is PRIMARY, the crew will monitor VDEV, XTK and F-PLN. Additionally, for VOR or ADFapproaches, the crew will monitor raw data.


8 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112, 0115-0162, 0167,0170-0177, 0183-0188, 0191-0192, 0196-0197, 0199-0220, 0222-0224, 0226-0229, 0231, 0233-0242, 0244-0246, 0248, 0253-0255, 0258,0262-0274, 0277-0279, 0281-0288, 0290, 0293, 0297-0303, 0305-0307, 0309-0313, 0315, 0318-0319, 0323-0325, 0328-0331, 0333, 0337,0339-0342, 0344-0346, 0348, 0350, 0352, 0355-0356, 0358-0360, 0364-0365, 0367, 0370, 0372, 0375, 0377-0378, 0380-0385, 0387-0390,0395, 0399-0404, 0407-0410, 0412-0413, 0417-0421, 0426-0427, 0434-0436, 0438-0439, 0442, 0445, 0450, 0452, 0454, 0456-0460,0462-0466, 0468, 0470, 0472-0475, 0477, 0479, 0482-3996

It is essential that the crew does not modify the final approach in the MCDU FPLN page.

The final approach will be flown either• Managed or• Selected




MANAGED

For a managed approach, FINAL APP becomes active and the FM manages both lateral andvertical guidance. The crew will monitor the final approach using• Start of descent blue symbol on ND• FMA on PFD• VDEV, XTK, F-PLN on ND with GPS PRIMARY• VDEV, XTK, F-PLN confirmed by needles, distance/altitude

If FINAL APPR does not engage at start of descent, the crew will select FPA convergent to the finalpath so as to fly with VDEV=0. Once VDEV=0, the crew may try to re-engage APPR.In some NPAs, the final approach flies an "idle descent" segment from one altitude constraint toanother, followed by a level segment. This is materialized by a magenta level off symbol on NDfollowed by a blue start of descent.

Final approach trajectory with idle descent segment

SELECTED

For a selected approach, the Final Path Angle (FPA) should be preset on the FCU 1 nm prior to theFAF at the latest. A smooth interception of the final approach path can be achieved by pulling theFPA selector 0.2 nm prior to the FAF. If GPS is PRIMARY, the crew will monitor VDEV, XTK and F-PLN. Additionally, for VOR or ADF approaches, the crew will monitor raw data.

REACHING THE MINIMAIdent.: NO-120-00005548.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

When approaching MDA, the pilot flying should expand the instrument scan to include outside visualcues.Reaching MDA, "MINIMUM" is either monitored or called by the crew. The current altitude valuebecomes amber.If the required conditions are not met by MDA, a missed approach must be initiated.




When the required visual conditions are met to continue the approach, the AP must be disconnected,the FDs selected off, Bird ON and continue for visual approach.

LOC ONLY APPROACHIdent.: NO-120-00005550.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

LOC ONLY approaches may be flown using the LOC signal for lateral navigation and FPA for verticalguidance. General recommendations mentioned above still apply i.e. stabilized approach technique,use of the bird. Some additional recommendations need to be highlighted.

INITIAL APPROACH

The crew will select LS p/b on the EIS control panel.


The crew will press LOC p/b on the FCU when cleared to intercept. He will monitor the LOC armedmode and then LOC capture.

FINAL APPROACH

Approaching FAF, the crew will select FPA. When established on the final path, the crew willmonitor:• Lateral displacement with LOC deviation• Vertical displacement with DME and ALT, "yoyo", chrono

LOC BACK COURSE APPROACHIdent.: NO-120-00005552.0001001 / 26 MAR 08Criteria: SA�

9 Applicable to: MSN 0002-2611, 2613-2632, 2634-2655, 2657-2682, 2684-2698, 2700-2718, 2720-2757, 2759, 2761-2788, 2790-2800,2802-2815, 2817-2825, 2827-2841, 2843-2880, 2882-2884, 2886-2925, 2927-2943, 2945-2955, 2957-2988, 2990-2999, 3001-3017, 3019-3030,3032-3042, 3044-3059, 3061-3063, 3065-3084, 3086-3093, 3095-3096, 3098-3116, 3118-3139, 3141-3153, 3155-3172, 3174-3181, 3183-3193,3195-3200, 3202-3222, 3224-3231, 3233-3260, 3262-3276, 3278-3290, 3292-3298, 3300-3326, 3328-3337, 3339-3352, 3354-3369, 3371-3393,3395-3403, 3405, 3407-3426, 3428-3435, 3437-3447, 3449-3451, 3453-3476, 3478-3485, 3487-3488, 3490-3504, 3506-3520, 3522-3535,3537-3548, 3550-3567, 3569-3575, 3577-3581, 3583-3609, 3611-3627, 3629-3647, 3649-3659, 3661-3678, 3680-3700, 3702-3714, 3716-3728,3730-3764, 3766-3775, 3777-3812, 3814-3874, 3876-3891, 3893-3996

LOC-BC approaches may be flown using the Bird with reference to the LOC-BC signal for lateralguidance and FPA for vertical guidance. General recommendations mentioned above still apply i.e.stabilized approach technique and use of the bird. Some additional recommendations need to behighlighted.




GENERAL

The LOC BC approach consists in using the LOC signal of the opposite runway for lateral approachmanagement.

The ILS will be manually entered in the MCDU RAD NAV page using:• Either the ident (ILS stored in the FMS database). RWY/ILS MISMATCH message may be

triggered and will be disregarded.• Or the frequency (ILS not stored in the FMS database).

In both cases, the front course will be entered in the CRS field.

INITIAL APPROACH

The crew will select ROSE ILS and TRK/FPA. The crew will not select ILS or L/S p/b on the EIScontrol panel and ISIS , as it would provide reverse deviation.


When clear for approach, the crew will intercept manually LOC/BC using the blue TRK index withreference with LOC/BC lateral deviation on ND. The crew will not arm LOC or APPR modes.

FINAL APPROACH

Approaching the FAF, the crew will select the FPA corresponding to the final approach path, LOCdeviation (proper directional guidance), DME/ALT, time, yoyo.


10 Applicable to: MSN 2612, 2633, 2656, 2683, 2699, 2719, 2758, 2760, 2789, 2816, 2826, 2842, 2881, 2885, 2926, 2944, 2956, 2989, 3000,3018, 3031, 3043, 3060, 3064, 3085, 3094, 3097, 3117, 3140, 3154, 3173, 3182, 3194, 3201, 3223, 3232, 3261, 3277, 3291, 3299, 3327, 3338,3353, 3370, 3394, 3404, 3406, 3427, 3436, 3448, 3452, 3477, 3486, 3489, 3505, 3521, 3536, 3549, 3568, 3576, 3582, 3610, 3628, 3648, 3660,3679, 3701, 3715, 3729, 3765, 3776, 3813, 3875, 3892, 2801

LOC-BC approaches may be flown using the Bird with reference to the LOC-BC signal for lateralguidance and FPA for vertical guidance. General recommendations mentioned above still apply i.e.stabilized approach technique and use of the bird. Some additional recommendations need to behighlighted.

GENERAL

The LOC BC approach consists in using the LOC signal of the opposite runway for lateral approachmanagement.If the LOC BC approach is stored in the FMS database, it will be inserted into the F-PLN. The ILSfrequency and associated back course are automatically tuned and displayed on the MCDU RADNAV page. The CRS digit will be preceded by a "B".If LOC BC is not stored in the FMS database, the crew will enter the ILS frequency and the finalapproach CRS the aircraft will actually fly preceded by a "B" in MCDU RAD NAV page. B/C in




magenta will be displayed both on PFD and ND. This provides a proper directional deviation on PFDand a proper directional guidance from the FG.

INITIAL APPROACH

The crew will select L/S p/b on the EIS control panel.


The crew will press LOC p/b on the FCU to arm LOC/BC and will monitor LOC/BC capture.

FINAL APPROACH

Approaching the FAF, the crew will select the FPA corresponding to the final approach path, LOCdeviation (proper directional guidance), DME/ALT, time, yoyo.


NORMAL OPERATIONSCIRCLING APPROACH


PREFACEIdent.: NO-130-00005554.0001001 / 26 MAY 08Criteria: SA�Applicable to: ALL

The circling approach is flown when the tower wind is such that the landing runway is different from therunway fitted with an instrument approach, which is used for the descent and approach in order to getvisual with the airfield.

APPROACH PREPARATIONIdent.: NO-130-00005556.0001001 / 26 MAY 08Criteria: SA�Applicable to: ALL

The approach preparation follows the same schema as described in APPROACH PREPARATIONsection in the CRUISE chapter. However, some characteristics need to be highlighted:

FPLN

Lateral: STAR, instrument approach procedure.Vertical: Insert F speed as constraint at FAF since the approach will be flown CONF 3, landinggear down and F speed (stabilized approach). Check altitude constraints.

RAD NAV

Manually tune the VOR/DME of destination airfield as required.

PROG

Insert VOR/DME of destination airfield in the BRG/DIST field as required. Check NAV ACCY ifrequired by comparing BRG/DIST data to raw data.

PERF

PERF APPR: Descent winds, destination airfield weather, minima and landing flap selection (windshear anticipated or in case of failure).PERF GO AROUND: Check thrust reduction and acceleration altitude.

FUEL PRED

Check estimated landing weight and extra fuel.

SEC F-PLN

When planning for a circling approach, the landing runway will be inserted into the SEC F-PLN. Thecrew will update the SEC F-PLN as follows:• SEC F-PLN then COPY ACTIVE• Lateral revision on destination and insert landing runway




• Keep the F-PLN discontinuity

FINAL INSTRUMENT APPROACHIdent.: NO-130-00005557.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The crew will fly a stabilized approach at F speed, configuration 3 and landing gear down.

CIRCLING APPROACHIdent.: NO-130-00005558.0001001 / 08 JAN 09Criteria: SA�Applicable to: ALL

When reaching circling minima and with appropriate visual reference for circling,• Level OFF• Select TRK/FPA• Select a TRK of 45 ° away from the final approach course (or as required by the published

procedure)• When wings level, start the chrono.• Once established downwind, activate the SEC F-PLN to take credit of the "GS mini" protection in

final approach when managed speed is used. Additionally, the landing runway will be shown on theND and the 10 nm range should be selected to assist in positioning onto final approach.

• By the end of the downwind leg, disconnect the AP, select both FDs off and keep the A/THR• When leaving the circling altitude, select the landing configuration• Once fully configured, complete the Landing Checklist.

Once the SEC F-PLN is activated, the go-around procedure in the MCDU will be that for the landingrunway rather than the one associated with the instrument approach just carried out. Therefore, ifvisual references were lost during the circling approach, the go-around would have to be flown usingselected guidance, following the pre-briefed missed approach procedure.For circling approach with one engine inoperative, Refer to AO-020 CIRCLING ONE ENGINEINOPERATIVE.




Low Visibility Circling Approach


NORMAL OPERATIONSVISUAL APPROACH


INITIAL APPROACHIdent.: NO-140-00005560.0001001 / 26 MAY 08Criteria: 22-1109, P7519, P7520, P7706, P7707, SA�


The crew must keep in mind that the pattern is flown visually. However, the XTK is a good cue of theaircraft lateral position versus the runway centreline. This is obtained when sequencing the F-PLN untilthe TO WPT (displayed on the ND top right hand corner) is on the final approach course.

The crew will aim to get the following configuration on commencement of the downwind leg:• Both AP and FDs will be selected off• BIRD ON• A/THR confirmed active in speed mode, i.e. SPEED on the FMA.• Managed speed will be used to enable the "GS mini” function• The downwind track will be selected on the FCU to assist in downwind tracking.• The downwind track altitude will be set on FCU






The crew must keep in mind that the pattern is flown visually. However, the XTK is a good cue ofthe aircraft lateral position versus the runway centreline. This is obtained when pressing DIR TO CIRADIAL IN.

The crew will aim to get the following configuration on commencement of the downwind leg:• Both AP and FDs will be selected off• BIRD ON• A/THR confirmed active in speed mode, i.e. SPEED on the FMA.• Managed speed will be used to enable the "GS mini" function• The downwind track will be selected on the FCU to assist in downwind tracking.• The downwind track altitude will be set on FCU

INTERMEDIATE/FINAL APPROACHIdent.: NO-140-00005562.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Assuming a 1 500 ft AAL circuit, the base turn should be commenced 45 s after passing abeam thedownwind threshold (± 1 s/kt of head/tailwind).The final turn onto the runway centreline will be commenced with 20 ° angle of bank. Initially the rate ofdescent should be 400 ft/min, increasing to 700 ft/min when established on the correct descent pathThe pilot will aim to be configured for landing at VAPP by 500 ft AAL, at the latest. If not stabilised, ago-around must be carried out.




visual approach


NORMAL OPERATIONSPRECISION APPROACH


GENERALIdent.: NO-150-00005563.0001001 / 23 MAY 08Criteria: SA�Applicable to: ALL

CAT II and CAT III approaches are flown to very low DH (or without DH) with very low RVR. Theguidance of the aircraft on the ILS beam and the guidance of the aircraft speed must be consistentlyof high performance and accurate so that an automatic landing and roll out can be performed in goodconditions and, the acquisition of visual cues is achieved and the aircraft properly stabilized. Hence,• The automatic landing is required in CAT III operations including roll out in CAT IIIB.• The automatic landing is the preferred landing technique in CAT II conditions• Any failures of the automated systems shall not significantly affect the aircraft automatic landing

system performance• The crew procedures and task sharing allow to rapidly detect any anomaly and thus lead to the right

decision

DEFINITIONIdent.: NO-150-00005564.0001001 / 25 JUN 08Criteria: SA�Applicable to: ALL

DECISION HEIGHT

The Decision Height (DH) is the wheel height above the runway elevation by which a go aroundmust be initiated unless appropriate visual reference has been established and the aircraft positionand the approach path have been assessed as satisfactory to continue the automatic approach andlanding safely. The DH is based on RA.

ALERT HEIGHT

The Alert Height (AH) is the height above the runway, based on the characteristics of the aeroplaneand its fail-operational automatic landing system, above which a CATIII approach would bediscontinued and a missed approach initiated if a failure occurred in one of the redundant parts ofthe automatic landing system, or in the relevant ground equipment.In others AH definition, it is generally stated that if a failure affecting the fail-operational criteriaoccurs below the AH, it would be ignored and the approach continued (except if AUTOLANDwarning is triggered). The AH concept is relevant when CAT 3 DUAL is displayed on FMA.On single aisle Airbus family, the AH =100 ft.

CAT 3 SINGLE

CAT 3 SINGLE is announced when the airborne systems are fail passive which means that a singlefailure will lead to the AP disconnection without any significant out of trim condition or deviation ofthe flight path or attitude. Manual flight is then required. This minimum DH is 50 ft.




CAT 3 DUAL

CAT 3 DUAL is announced when the airborne systems are fail-operational. In case of a singlefailure, the AP will continue to guide the aircraft on the flight path and the automatic landing systemwill operate as a fail-passive system. In the event of a failure below the AH, the approach, flare andlanding can be completed by the remaining part of the automatic system. In that case, no capabilitydegradation is indicated. Such a redundancy allows CAT III operations with or without DH.

CAT II OR CAT III APPROACHES

ICAO FAA JAADH 100 ft ≤ DH < 200 ft 100 ft ≤ DH < 200 ft 100 ft ≤ DH < 200 ftCAT II

RVR RVR ≥ 350 mRVR ≥ 1 200 ft

350 m ≤ RVR < 800 m1 200 ft ≤ RVR < 2 400 ft

RVR ≥ 300 mRVR ≥ 1 000 ft

DH No DH or DH < 100 ft No DH or DH < 100 ft DH < 100 ft (1)CAT IIIARVR RVR ≥ 200 m

RVR ≥ 700 ftRVR ≥ 200 mRVR ≥ 700 ft

RVR ≥ 200 mRVR ≥ 700 ft

DH No DH or DH < 50 ft No DH or DH < 50 ft No DH or DH < 50 ftCAT IIIBRVR 50 m ≤ RVR < 200 m

150 ft ≤ RVR < 700 ft50 m ≤ RVR < 200 m150 ft ≤ RVR < 700 ft

75 m ≤ RVR < 200 m250 ft ≤ RVR < 700 ft

(1) DH ≥ 50 ft if fail passive

FLIGHT PREPARATIONIdent.: NO-150-00005566.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

In addition to the normal flight preparation, the following preparation must be performed when CAT II orCAT III approach is planned:• Ensure that destination airport meets CAT II or CAT III requirements• Check aircraft required equipment for CAT II or CAT III in QRH• Check that crew qualification is current• Consider extra fuel for possible approach delay• Consider weather at alternate




APPROACH PREPARATIONIdent.: NO-150-00005567.0001001 / 23 MAY 08Criteria: SA�Applicable to: ALL

LIMITATIONS

• The crew will check that tower wind remains within the limit for CAT II or CAT III approaches(Refer to FCOM/LIM-22-20 MAXIMUM WIND CONDITIONS FOR CAT II OR CAT III AUTOMATICAPPROACH LANDING AND ROLL OUT)

• The autoland maximum altitude must be observed.

AIRCRAFT CAPABILITY

The failures that may affect the aircraft's CAT II or CAT III capability are listed in the QRH. Most ofthese failures are monitored by the FMGS and the landing capability will be displayed on the FMAonce the APPR pb is pressed, i.e. CAT II, CAT III SINGLE, CAT III DUAL. However, there are anumber of failures which affect the aircraft's landing capability which are not monitored by the FMGSand, consequently, not reflected on the FMA. It is very important, therefore, that the crew refer to theQRH to establish the actual landing capability if some equipment are listed inoperative.

AIRPORT FACILITIES

The airport authorities are responsible for establishing and maintaining the equipment required forCAT II/III approach and landing. The airport authorities will activate the LVP procedures as the needarises based on RVR. Prior to planning a CAT II/III approach, the crew must ensure that LVP are inforce.

CREW QUALIFICATION

The captain must ensure that both crew members are qualified and that their qualification is currentfor the planned approach.

SEATING POSITION

The crew must realise the importance of eye position during low visibility approaches and landing.A too low seat position may greatly reduce the visual segment. When the eye reference position islower than intended, the visual segment is further reduced by the cut-off angle of the glareshieldor nose. As a rule of thumb, an incorrect seating position which reduces the cut-off angle by 1 °reduces the visual segment by approximately 10 m (30 ft).

USE OF LANDING LIGHTS

The use of landing lights at night in low visibility can be detrimental to the acquisition of visualreference. Reflected lights from water droplets or snow may actually reduce visibility. The landinglights would, therefore, not normally be used in CAT II/III weather conditions.




APPROACH STRATEGY

Irrespective of the actual weather conditions, the crew should plan the approach using the bestapproach capability. This would normally be CAT III DUAL with autoland, depending upon aircraftstatus. The crew should then assess the weather with respect to possible downgrade capability.

CAT IIIConditions CAT I CAT IIWITH DH NO DH

Flying technique Manual flying orAP/FD, A/THR

AP/FD, A/THRdown to DH

AP/FD/ATHR and Autoland

Minima & weather DA (DH) Baro ref Visibility DH with RARVR

Autoland Possible with precautions Recommended Mandatory

GO AROUND STRATEGY

The crew must be ready mentally for go-around at any stage of the approach. Should a failure occurabove 1 000 ft RA, all ECAM actions (and DH amendment if required) should be completed beforereaching 1 000 ft RA, otherwise a go-around should be initiated. This ensures proper task sharingfor the remainder of the approach. Any alert generated below 1 000 ft should lead to a go-around.

APPROACH BRIEFING

Before commencing a CAT II/III approach a number of factors must be considered by the crew. Inaddition to the standard approach briefing, the following points should be emphasised during anapproach briefing for a low visibility approach:• Aircraft capability• Airport facilities• Crew qualification• Weather minima• Task sharing• Call-outs• Go-around strategy

APPROACH PROCEDUREIdent.: NO-150-00005568.0001001 / 25 JUN 08Criteria: SA�Applicable to: ALL

TASK SHARING

The workload is distributed in such a way that the PF primary tasks are supervising and decisionmaking and the PNF primary task is monitoring the operation of the automatic system.




The PF supervises the approach (trajectory, attitude, speed) and takes appropriate decision in caseof failure and at DH. Since the approach is flown with AP/FD/A-THR, the PF must be continuouslyready to take-over• If any AP hard over is experienced• If a major failure occurs• If any doubt arises

The PF announces "LAND", when displayed on FMA.

The PNF is head down throughout the approach and landing. The PNF monitors:• The FMA and calls mode change as required (except "LAND")• The Auto call out• The aircraft trajectory or attitude exceedance• Any failures

The PNF should be go-around minded.

SOME SYSTEM PARTICULARS

• Below 700 ft RA, data coming from the FMS is frozen e.g. ILS tune inhibit.• Below 400 ft RA, the FCU is frozen.• At 350 ft, LAND must be displayed on FMA. This ensures correct final approach guidance.• Below 200 ft, the AUTOLAND red light illuminates if

‐ Both APs trip off‐ Excessive beam deviation is sensed‐ Localizer or glide slope transmitter or receiver fails‐ A RA discrepancy of at least 15 ft is sensed.

• Flare comes at or below 40 ft• THR IDLE comes at or below 30 ft• RETARD auto call out comes at 10 ft for autoland as an order. (Instead of 20 ft for manual landing

as an indication)

VISUAL REFERENCE

Approaching the DH, the PF starts to look for visual references, progressively increasing externalscanning. It should be stressed that the DH is the lower limit of the decision zone. The captainshould come to this zone prepared for a go-around but with no pre-established judgement.

Required conditions to continue• With DH

In CAT II operations, the conditions required at DH to continue the approach are that the visualreferences should be appropriate to monitor the continued approach and landing and that theflight path should be acceptable. If both these conditions are not satisfied, it is mandatory to




initiate a go-around. A 3 lights segment and a lateral light element is the minimum visual cue forJAR OPS.In CAT III operations, the condition required at DH is that there should be visual referenceswhich confirm that the aircraft is over the touch down zone. Go-around is mandatory if the visualreferences do not confirm this. A 3 lights segment is required by JAR OPS for fail passive systemand 1 centerline light segment for fail operational system.

• Without DHThe decision to continue does not depend on visual references, even though a minimum RVRis specified. The decision depends only on the operational status of the aircraft and groundequipment. If a failure occurs prior to reaching the AH, a go-around will be initiated. A go-aroundmust nevertheless be performed if AUTOLAND warning is triggered below AH. However, it is goodairmanship for the PF to acquire visual cues during flare and to monitor the roll out.

Loss of visual reference• With DH before touch down

If decision to continue has been made by DH and the visual references subsequently becomeinappropriate a go-around must be initiated.A late go-around may result in ground contact. If touch down occurs after TOGA is engaged, theAP remains engaged in that mode and A/THR remains in TOGA. The ground spoilers and auto-brake are inhibited.

• With DH or without DH after touch downIf visual references are lost after touch down, a go-around should not be attempted. The roll-outshould be continued with AP in ROLL OUT mode down to taxi speed.

FLARE/LANDING/ROLL OUT

During the flare, decrab and roll-out, the PF will look outside to assess that the autoland is properlycarried out, considering the appropriate visual references.For CAT II approaches, autoland is recommended. If manual landing is preferred, the PF will take-over at 80 ft at the latest. This ensures a smooth transition for the manual landing.Select maximum reverse at main landing gear touch down.The use of auto-brake is recommended as it ensures a symmetrical brake pressure application.However, the crew should be aware of possible dissymmetry in case of crosswind and wet runways.The PNF will use standard call out. Additionally, he will advise ATC when aircraft is properlycontrolled (speed and lateral trajectory).




FAILURE AND ASSOCIATED ACTIONSIdent.: NO-150-00005570.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

As a general rule, if a failure occurs above 1 000 ft AGL, the approach may be continued, ECAMactions completed, approach briefing update performed and a higher DH set if required.Below 1 000 ft (and down to AH in CAT3 DUAL), the occurrence of any failure implies a go-around anda reassessment of the system capability. Another approach may be under taken according to the newsystem capability. It has been considered that below 1 000 ft, not enough time is available for the crewto perform the necessary switching, to check system configuration and limitation and brief for minima.In CAT3 DUAL and below AH, as a general rule, a single failure does not necessitate a go-around. Ago-around is required if the AUTOLAND warning is triggered.

AUTOLAND IN CAT 1 OR BETTER WEATHER CONDITIONSIdent.: NO-150-00005571.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The crew may wish to practice automatic landings in CAT I or better weather conditions for trainingpurposes. This type of approach should be carried out only with the airline authorization. The crewshould be aware that fluctuations of the LOC and/or GS might occur due to the fact that protection ofILS sensitive areas, which applies during LVP, will not necessarily be in force. It is essential, therefore,that the PF is prepared to take over manually at any time during a practice approach and rollout,should the performance of the AP become unsatisfactory.


NORMAL OPERATIONSLANDING



When Transitioning from IMC to VMC, the crew will watch the bird versus the aircraft attitude symbol inthe center of the PFD. This provides a good assessment of the drift, thus in which direction to look forthe runway.

But, then• Do not turn towards the runway• Do not duck under

MAIN GEAR CLEARANCEIdent.: NO-160-00005575.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The boxed images below are the one to retain to ensure about 20 ft wheel clearance at threshold.use of VASI/TVASI/PAPI




use of VASI/TVASI/PAPI

This technique will ensure that performance margins are not compromised and provide adequate maingear clearance.

FLAREIdent.: NO-160-00005576.0001001 / 19 DEC 08Criteria: SA�Applicable to: ALL

1 PITCH CONTROL

When reaching 50 ft, auto-trim ceases and the pitch law is modified to flare law. Indeed, the normalpitch law, which provides trajectory stability, is not the best adapted to the flare manoeuvre. Thesystem memorizes the attitude at 50 ft, and that attitude becomes the initial reference for pitchattitude control. As the aircraft descends through 30 ft, the system begins to reduce the pitch attitudeat a predetermined rate of 2 ° down in 8 s. Consequently, as the speed reduces, the pilot will have tomove the stick rearwards to maintain a constant path. The flare technique is thus very conventional.From stabilized conditions, the flare height is about 30 ft. This height varies with differentparameters, such as weight, rate of descent, wind variations...

Avoid under flaring.‐ The rate of descent must be controlled prior to the initiation of the flare (rate not increasing)‐ Start the flare with positive backpressure on the sidestick and holding as necessary‐ Avoid forward stick movement once Flare initiated (releasing back-pressure is acceptable)

At 20 ft, the "RETARD" auto call-out reminds the pilot to retard thrust levers. It is a reminder ratherthan an order. When best adapted, the pilot will rapidly retard all thrust levers: depending on theconditions, the pilot will retard earlier or later. However, the pilot must ensure that all thrust leversare at IDLE detent at the latest at touchdown, to ensure ground spoilers extension at touchdown. Inorder to assess the rate of descent in the flare, and the aircraft position relative to the ground, lookwell ahead of the aircraft. The typical pitch increment in the flare is approximately 4 °, which leadsto -1 ° flight path angle associated with a 10 kt speed decay in the manoeuvre. A prolonged float willincrease both the landing distance and the risk of tail strike.




LATERAL AND DIRECTIONAL CONTROL

FINAL APPROACH

In crosswind conditions, a crabbed-approach should be flown.

FLARE

The objectives of the lateral and directional control of the aircraft during the flare are:‐ To land on the centerline‐ And, to minimize the loads on the main landing gear.

During the flare, rudder should be applied as required to align the aircraft with the runwayheading. Any tendency to drift downwind should be counteracted by an appropriate lateral (roll)input on the sidestick.In the case of a very strong cross wind, the aircraft may be landed with a residual drift (up toabout 5 °) to prevent an excessive bank (up to about 5 °). Consequently, combination of the partialde-crab and wing down techniques may be required.

MAXIMUM DEMONSTRATED CROSSWIND FOR LANDINGIdent.: NO-160-00005578.0001001 / 16 JUN 08Criteria: SA�


With a good reported braking action, the maximum demonstrated crosswind at landing is 33 knots, withgusts up to 38 knots.

Ident.: NO-160-00005578.0002001 / 16 JUN 08Criteria: SA, A318�


With a good reported braking action, the maximum demonstrated crosswind at landing is 38.5 knots(gusts included).




CALL OUTIdent.: NO-160-00005579.0001001 / 26 MAR 08Criteria: SA�

4 Applicable to: MSN 0002-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487,0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534, 0537, 0539-0540,0542-0543, 0545-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569, 0571-0575, 0577-0580, 0582, 0584-0585,0587-0590, 0592, 0594, 0596, 0598, 0600-0603, 0605, 0607-0613, 0615-0619, 0621-0630, 0634-0641, 0643-0651, 0653-0662, 0665, 0667,0669-0673, 0676, 0678-0679, 0681-0683, 0685-0686, 0688-0691, 0693-0698, 0700-0714, 0716-0724, 0726-0730, 0732-0745, 0747-0760,0762-0764, 0766-0770, 0772-0774, 0776, 0778-0780, 0782-0786, 0788-0791, 0793-0795, 0797-0801, 0803-0805, 0807, 0809, 0812-0814,0816-0818, 0820-0822, 0824-0826, 0828-0834, 0836-0840, 0842-0847, 0849-0851, 0853-0854, 0856-0863, 0865-0877, 0879-0886, 0888-0890,0892-0900, 0902-0907, 0909-0914, 0916-0919, 0921-0925, 0927-0934, 0936-0939, 0942-0953, 0955, 0957-0958, 0960, 0962, 0964-0967,0969, 0971-0973, 0975-0982, 0984-0986, 0988-0990, 0992, 0994, 0996-1003, 1005, 1007, 1009-1011, 1013-1014, 1016, 1018-1020, 1022,1025-1026, 1028-1041, 1043-1044, 1046-1059, 1061-1079, 1081-1093, 1095-1132, 1134-1143, 1145-1152, 1154-1160, 1162-1173, 1175-1184,1187, 1189-1194, 1196-1198, 1200-1201, 1203, 1205-1206, 1208-1213, 1215-1217, 1221-1226, 1228-1232, 1234-1237, 1239-1240, 1242-1249,1251-1259, 1261-1272, 1274-1275, 1277-1292, 1294-1298, 1300-1306, 1308-1332, 1334-1355, 1357-1365, 1367-1398, 1400-1402, 1404-1407,1409-1411, 1413-1416, 1418-1420, 1422-1424, 1426-1427, 1429-1430, 1432, 1434-1435, 1437, 1439-1441, 1443-1446, 1448-1450, 1452-1454,1456-1457, 1459-1461, 1463-1464, 1466-1471, 1473-1475, 1477-1480, 1482-1486, 1488-1491, 1493-1495, 1497-1498, 1500-1502, 1504-1510,1512-1516, 1518, 1520, 1522-1524, 1526-1530, 1532-1535, 1537-1538, 1540-1553, 1555-1571, 1573-1586, 1588-1595, 1597-1601, 1603-1606,1608-1610, 1612-1613, 1615-1618, 1620-1622, 1624-1628, 1630-1631, 1633-1635, 1637, 1639-1641, 1643-1650, 1652-1657, 1659-1665,1667-1669, 1671-1674, 1676-1680, 1682-1689, 1692-1694, 1696-1700, 1702-1703, 1705-1706, 1708-1710, 1712, 1714-1715, 1717-1719,1721-1723, 1725, 1727-1733, 1735-1747, 1749-1762, 1764-1771, 1773-1775, 1777-1782, 1784-1787, 1789-1793, 1795-1797, 1799-1806,1808-1810, 1812-1816, 1818-1835, 1837-1842, 1844-1847, 1849, 1851-1858, 1860-1868, 1870-1877, 1879-1880, 1882-1886, 1888-1904,1906-1920, 1922-1925, 1927, 1929-1931, 1933-1940, 1942-1945, 1947-1949, 1951-1952, 1954-1955, 1957-1959, 1961-1965, 1968-1969, 1971,1973, 1975-1976, 1979-1983, 1986-1987, 1989-1993, 1996-2004, 2006-2020, 2022-2040, 2042-2044, 2046-2054, 2056-2059, 2061-2063,2065-2066, 2068-2075, 2077-2079, 2081-2104, 2106, 2108-2109, 2112-2114, 2116, 2118-2189, 2191-2207, 2209-2210, 2212-2215, 2217-2219,2221-2225, 2227-2233, 2235-2246, 2248-2254, 2256-2260, 2262-2266, 2268-2269, 2271-2289, 2291-2302, 2304, 2306-2308, 2310-2314,2316-2319, 2321-2322, 2325-2329, 2331-2336, 2338-2341, 2343-2350, 2352-2356, 2358-2362, 2364-2380, 2382-2409, 2411-2461, 2463-2471,2473-2475, 2477-2479, 2481-2487, 2489-2520, 2522-2529, 2531-2535, 2537-2542, 2544-2548, 2550-2552, 2554-2562, 2564-2589, 2591-2598,2600-2609, 2611-2652, 2654-2681, 2683-2686, 2688-2706, 2708-2712, 2714-2725, 2727-2729, 2731-2735, 2737-2740, 2742-2755, 2757-2758,2760-2766, 2768-2792, 2794-2798, 2800-2808, 2810-2822, 2824-2861, 2863-2867, 2869-2881, 2883-2894, 2896-2902, 2904-2911, 2913-2915,2917-2918, 2920-2926, 2928-2932, 2934-2935, 2937-2956, 2958-2964, 2966-2970, 2972-2973, 2975-2995, 2997-2998, 3000-3004, 3006-3012,3014, 3016-3021, 3023-3033, 3035-3050, 3052-3066, 3068-3069, 3071-3074, 3076-3080, 3082-3097, 3099-3105, 3107-3111, 3113-3119,3121-3125, 3127-3129, 3131-3145, 3147-3190, 3192-3197, 3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228, 3230-3232, 3234,3236-3240, 3242-3246, 3248, 3250, 3252-3253, 3255-3261, 3263-3264, 3266, 3268-3273, 3275-3282, 3284-3289, 3291-3293, 3295-3296,3298-3301, 3303-3306, 3308-3314, 3316-3321, 3323-3325, 3327-3328, 3330-3333, 3335-3338, 3341-3349, 3351-3354, 3356-3359, 3361-3366,3368, 3370-3371, 3373-3381, 3383-3386, 3388-3396, 3398, 3400, 3402-3404, 3406-3418, 3420-3428, 3430-3433, 3435-3440, 3442-3457,3460-3461, 3463-3470, 3472-3492, 3494-3497, 3499-3503, 3505-3506, 3508-3511, 3513-3521, 3524, 3526, 3528-3538, 3540-3545, 3547-3551,3553-3556, 3558-3565, 3567-3572, 3574, 3576-3582, 3585-3586, 3588-3591, 3594-3599, 3601-3611, 3613-3618, 3620-3622, 3624, 3626-3628,3630-3632, 3634-3635, 3640-3644, 3646-3652, 3654, 3656-3664, 3666-3668, 3670-3672, 3674-3677, 3679-3680, 3683-3687, 3689-3707,3709-3711, 3713-3716, 3718-3721, 3723-3724, 3726-3729, 3731-3736, 3739, 3741-3748, 3750-3751, 3753-3760, 3762-3763, 3765, 3767-3783,3785-3791, 3793-3795, 3807-3813, 3815, 3817-3819, 3863, 3871-3877, 3937, 3638, 3797-3805, 3821-3829, 3831-3846, 3848-3857, 3859-3861,3865-3866, 3868, 3880, 3882-3883, 3885-3892, 3894-3898, 3900-3915, 3917-3919, 3921-3923, 3925, 3927, 3931-3933, 3935, 3939,3941-3943, 3945-3947, 3949-3950, 3952-3954, 3956-3959, 3962, 3965, 3967-3968, 3970-3972, 3983-3984, 3995

If pitch attitude exceeds 10 °, the PNF will announce "PITCH".




Ident.: NO-160-00005579.0002001 / 26 MAR 08Criteria: SA, 321-100, 321-200�


If pitch attitude exceeds 7.5 °, the PNF will announce "PITCH".

DEROTATIONIdent.: NO-160-00005581.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

When the aircraft is on the ground, pitch and roll control operates in Direct Law. Consequently, whenthe aircraft touches down, the pilot flies the nose down conventionally, varying sidestick input asrequired, to control the derotation rate.After touch down, when reverse thrust is selected (on at least one engine) and one main landing gearstrut is compressed, the ground spoilers partially extend to establish ground contact. The groundspoilers fully extend when both main landing gears are compressed. A small nose down term on theelevators is introduced by the control law, which compensates the pitch up tendency with groundspoiler extension.It is not recommended to keep the nose high in order to increase aircraft drag during the initial partof the roll-out, as this technique is inefficient and increases the risk of tail strike. Furthermore, if autobrake MED is used, it may lead to a hard nose gear touch down.




ROLL OUTIdent.: NO-160-00005583.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

NORMAL CONDITIONS

During the roll out, the rudder pedals will be used to steer the aircraft on the runway centreline.At high speed, directional control is achieved with rudder. As the speed reduces, the Nose WheelSteering (NWS) becomes active. However, the NWS tiller will not be used until taxi speed isreached.

CROSSWIND CONDITIONS

The above-mentioned technique applies. Additionally, the pilot will avoid setting stick into the wind asit increases the weathercock effect. Indeed, it creates a differential down force on the wheels into thewind side and differential drag due to spoiler retraction.The reversers have a destabilizing effect on the airflow around the rudder and thus decrease theefficiency of the rudder. Furthermore they create a side force, in case of a remaining crab angle,which increases the lateral skidding tendency of the aircraft. This adverse effect is quite noticeableon contaminated runways with crosswind. In case a lateral control problem occurs in high crosswindlanding, the pilot will consider to set reversers back to Idle.At lower speeds, the directional control of the aircraft is more problematic, more specificallyon wet and contaminated runways. Differential braking is to be used if necessary. On wet andcontaminated runways, the same braking effect may be reached with full or half deflection of thepedals; additionally the anti skid system releases the brake pressure on both sides very early whenthe pilot presses on the pedals. Thus if differential braking is to be used, the crew will totally releasethe pedal on the opposite side to the expected turn direction.

BRAKINGIdent.: NO-160-00005584.0001001 / 30 JUN 08Criteria: SA�Applicable to: ALL

Once on the ground, the importance of the timely use of all means of stopping the aircraft cannot beoveremphasised. Three systems are involved in braking once the aircraft is on the ground:• The ground spoilers• The thrust reversers• The wheel brakes

THE GROUND SPOILERS

When the aircraft touches down with at least one main landing gear and when at least one thrustlever is in the reverse sector, the ground spoilers partially automatically deploy to ensure that the




aircraft is properly sit down on ground. Then, the ground spoilers automatically fully deploy. This isthe partial lift dumping function.The ground spoilers contribute to aircraft deceleration by increasing aerodynamic drag at highspeed. Wheel braking efficiency is improved due to the increased load on the wheels. Additionally,the ground spoiler extension signal is used for auto-brake activation.

THRUST REVERSERS

Thrust reverser efficiency is proportional to the square of the speed. So, it is recommended to usereverse thrust at high speeds.Select maximum reverse at main landing gear touch down.The maximum reverse thrust is obtained at N1 between 70 % and 85 % and is controlled by theFADEC.A slight pitch-up, easily controlled by the crew, may appear when the thrust reversers are deployedbefore the nose landing gear touches down.Below 70 kt, reversers efficiency decreases rapidly. Additionally, the use of high levels of reversethrust at low speed can cause engine stalls.Therefore, it is recommended to smoothly reduce the reverse thrust to idle at 70 kt. However, theuse of maximum reverse is allowed down to aircraft stop in case of emergency.If airport regulations restrict the use of reverse, select and maintain reverse idle until taxi speed isreached.Stow the reversers before leaving the runway to avoid foreign object ingestion.

WHEEL BRAKES

Wheel brakes contribute the most to aircraft deceleration on the ground. Many factors may affectefficient braking such as load on the wheels, tire pressure, runway pavement characteristics andrunway contamination and braking technique. The only factor over which the pilot has any control isthe use of the correct braking technique, as discussed below.

ANTI-SKID

The anti-skid system adapts pilot applied brake pressure to runway conditions by sensing animpending skid condition and adjusting the brake pressure to each individual wheel as required.The anti-skid system maintains the skidding factor (slip ratio) close to the maximum friction forcepoint. This will provide the optimum deceleration with respect to the pilot input. Full pedal brakingwith anti-skid provides a deceleration rate of 10 kt/sec.

BRAKES

The use of auto brake versus pedal braking should observe the following guidelines:• The use of A/BRAKE is usually preferable because it minimizes the number of brake

applications and thus reduces brake wear. Additionally, the A/BRAKE provides a symmetricalbrake pressure application which ensures an equal braking effect on both main landing




gear wheels on wet or evenly contaminated runway. More particularly, the A/BRAKE isrecommended on short, wet, contaminated runway, in poor visibility conditions and in Auto land.

• The use of LO auto brake should be preferred on long and dry runways whereas the use ofMED auto brake should be preferred for short or contaminated runways. The use of MAX autobrake is not recommended.

• On very short runways, the use of pedal braking is to be envisaged since the pilot may applyfull pedal braking with no delay after touch down.

• On very long runways, the use of pedal braking may be envisaged if the pilot anticipates thatbraking will not be needed. To reduce brake wear, the number of brake application should belimited.

• In case of pedal braking, do not ride the brakes but apply pedal braking when required andmodulate the pressure without releasing. This minimizes brake wear.

The green DECEL light comes on when the actual deceleration is 80 % of the selected rate. Forexample the DECEL light might not appear when the autobrake is selected on a contaminatedrunway, because the deceleration rate is not reached with the autobrake properly functioning.Whereas the DECEL light might appear with LO selected on a dry runway while only the reversersachieve the selected deceleration rate without autobrake being actually activated. In other words,the DECEL light is not an indicator of the autobrake operation as such, but that the decelerationrate is reached.Since the auto brake system senses deceleration and modulates brake pressure accordingly, thetimely application of MAX reverse thrust will reduce the actual operation of the brakes themselves,thus the brake wear and temperature.Auto-brake does not relieve the pilot of the responsibility of achieving a safe stop within theavailable runway length.

CROSS WIND CONDITIONS

The reverse thrust side force and crosswind component can combine to cause the aircraft to driftto the downwind side of the runway if the aircraft is allowed to weathercock into wind after landing.Additionally, as the anti-skid system will be operating at maximum braking effectiveness, the maingear tire cornering forces available to counteract this drift will be reduced.

braking force and cornering force vs antiskid




To correct back to the centreline, the pilot must reduce reverse thrust to reverse idle and release thebrakes. This will minimise the reverse thrust side force component, without the requirement to gothrough a full reverser actuating cycle, and provide the total tire cornering forces for realignment withthe runway centreline. Rudder and differential braking should be used, as required, to correct backto the runway centreline. When re-established on the runway centreline, the pilot should re-applybraking and reverse thrust as required.

Directional Control during Crosswind Landing

FACTORS AFFECTING LANDING DISTANCEIdent.: NO-160-00005586.0001001 / 16 MAY 08Criteria: SA�Applicable to: ALL

The field length requirements are contained in the FCOM PER, LND LANDING. The landing distancemargin will be reduced if the landing technique is not correct. Factors that affect stopping distanceinclude:• Height and speed over the threshold• Glide slope angle• Landing flare technique• Delay in lowering the nose on to the runway• Improper use of braking system• Runway conditions (discussed in adverse weather).

Height of the aircraft over the runway threshold has a significant effect on total landing distance. Forexample, on a 3 ° glide path, passing over the runway threshold at 100 ft altitude rather than 50 ft couldincrease the total landing distance by approximately 300 m/950 ft. This is due to the length of runwayused before the aircraft touches down.




A 5 kt speed increment on VAPP produces a 5 % increase in landing distance with auto brakeselected.For a 50 ft Threshold Crossing Height, a shallower glide path angle increases the landing distance, asthe projected touchdown point will be further down the runway.Floating above the runway before touchdown must be avoided because it uses a large portion of theavailable runway. The aircraft should be landed as near the normal touchdown point as possible.Deceleration rate on the runway is approximately three times greater than in the air.Reverse thrust and speedbrake drag are most effective during the high-speed portion of the landing.Therefore, reverse thrust should be selected without delay.Speed brakes fully deployed, in conjunction with maximum reverse thrust and maximum manual anti-skid braking provides the minimum stopping distance.

Operational factors affecting actual landing distance

(1) Those coefficients are given as indications.




CLEARANCE AT TOUCH DOWNIdent.: NO-160-00005587.0001001 / 26 MAR 08Criteria: 318-100�


Geometry limit at touch down Pitch attitude atVAPP(Vref +5 kt) (1)

Pitch attitude at touch down Clearance (2)

17.3 ° tbd tbd tbd°(1) Flight path in approach: -3 °(2) Clearance = geometry limit - pitch attitude at touch down




Continued from previous page15.5 ° 3.4 ° 7.7 ° 7.8 °

(1) Flight path in approach: -3 °(2) Clearance = geometry limit - pitch attitude at touch down




Continued from previous page13.5 ° 3.3 ° 7.6 ° 5.9 °

(1) Flight path in approach: -3 °(2) Clearance = geometry limit - pitch attitude at touch down

Ident.: NO-160-00005587.0005001 / 26 MAR 08Criteria: 321-100�Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522,0524, 0526, 0529, 0532, 0535, 0538, 0541, 0544, 0550, 0552, 0555, 0557, 0560, 0563-0564, 0567, 0570, 0576, 0581, 0583, 0586, 0591, 0593,0595, 0597, 0599, 0604, 0606, 0614, 0620, 0631, 0642, 0652, 0664, 0692, 0699, 0731, 0746, 0765, 0819, 0848, 0887, 0901, 0940, 0959, 0987,1144, 1220, 1356, 1511



11.2 ° 2.4 ° 6.6 ° 4.6 °(1) Flight path in approach: -3 °(2) Clearance = geometry limit - pitch attitude at touch down


9 Applicable to: MSN 0633, 0663, 0666, 0668, 0674-0675, 0677, 0680, 0684, 0687, 0715, 0725, 0761, 0771, 0775, 0777, 0781, 0787, 0792,0796, 0802, 0806, 0808, 0810-0811, 0815, 0823, 0827, 0835, 0841, 0852, 0855, 0864, 0878, 0891, 0908, 0915, 0920, 0926, 0935, 0941,0954, 0956, 0961, 0963, 0968, 0970, 0974, 0983, 0991, 0993, 0995, 1004, 1006, 1008, 1012, 1015, 1017, 1021, 1023-1024, 1027, 1042, 1045,1060, 1080, 1094, 1133, 1153, 1161, 1174, 1185, 1188, 1195, 1199, 1202, 1204, 1207, 1214, 1218-1219, 1227, 1233, 1238, 1241, 1250, 1260,1273, 1276, 1293, 1299, 1307, 1333, 1366, 1399, 1403, 1408, 1412, 1417, 1421, 1425, 1428, 1431, 1433, 1436, 1438, 1442, 1447, 1451, 1455,1458, 1462, 1465, 1472, 1476, 1481, 1487, 1492, 1496, 1499, 1503, 1517, 1519, 1521, 1525, 1531, 1536, 1539, 1554, 1572, 1587, 1596, 1602,1607, 1611, 1614, 1619, 1623, 1629, 1632, 1636, 1638, 1642, 1651, 1658, 1666, 1670, 1675, 1681, 1690-1691, 1695, 1701, 1704, 1707, 1711,1713, 1716, 1720, 1724, 1726, 1734, 1748, 1763, 1772, 1776, 1783, 1788, 1794, 1798, 1807, 1811, 1817, 1836, 1843, 1848, 1850, 1859, 1869,1878, 1881, 1887, 1905, 1921, 1926, 1928, 1932, 1941, 1946, 1950, 1953, 1956, 1960, 1966-1967, 1970, 1972, 1974, 1977-1978, 1984, 1988,1994-1995, 2005, 2021, 2041, 2045, 2055, 2060, 2064, 2067, 2076, 2080, 2105, 2107, 2110, 2115, 2117, 2190, 2208, 2211, 2216, 2220, 2226,2234, 2247, 2255, 2261, 2267, 2270, 2290, 2303, 2305, 2309, 2315, 2320, 2323-2324, 2330, 2337, 2342, 2351, 2357, 2363, 2381, 2410, 2462,2472, 2476, 2480, 2488, 2521, 2530, 2536, 2543, 2549, 2553, 2563, 2590, 2599, 2610, 2653, 2682, 2687, 2707, 2713, 2726, 2730, 2736, 2741,2756, 2759, 2767, 2793, 2799, 2809, 2823, 2862, 2868, 2882, 2895, 2903, 2912, 2916, 2919, 2927, 2933, 2936, 2957, 2965, 2971, 2974, 2996,2999, 3005, 3013, 3015, 3022, 3034, 3051, 3067, 3070, 3075, 3081, 3098, 3106, 3112, 3120, 3126, 3130, 3146, 3191, 3198, 3207, 3212, 3217,3222, 3229, 3233, 3235, 3241, 3247, 3249, 3251, 3254, 3262, 3265, 3267, 3274, 3283, 3290, 3294, 3297, 3302, 3307, 3315, 3322, 3326, 3329,3334, 3339-3340, 3350, 3355, 3360, 3367, 3369, 3372, 3382, 3387, 3397, 3399, 3401, 3405, 3419, 3429, 3434, 3441, 3458-3459, 3462, 3471,3493, 3498, 3504, 3507, 3512, 3522-3523, 3525, 3527, 3539, 3546, 3552, 3557, 3566, 3573, 3575, 3583-3584, 3587, 3592-3593, 3600, 3612,3619, 3623, 3625, 3629, 3633, 3636-3637, 3639, 3645, 3653, 3655, 3665, 3669, 3673, 3678, 3681-3682, 3688, 3708, 3712, 3717, 3722, 3725,3730, 3737-3738, 3740, 3749, 3752, 3761, 3764, 3766, 3784, 3792, 3796, 3806, 3814, 3816, 3820, 3847, 3858, 3862, 3867, 3878-3879, 3920,3830, 3864, 3869, 3881, 3884, 3893, 3899, 3916, 3924, 3926, 3928-3930, 3934, 3936, 3938, 3940, 3944, 3948, 3951, 3955, 3960, 3964, 3966,3969, 3977-3981, 3989-3993, 3996



10.8 ° 2.4 ° 6.6 ° 4.2 °(1) Flight path in approach:-3 °(2) Clearance = geometry limit - pitch attitude at touch down




TAIL STRIKE AVOIDANCEIdent.: NO-160-00005589.0001001 / 23 MAY 08Criteria: SA�Applicable to: ALL

Although most of tail strikes are due to deviations from normal landing techniques, some areassociated with external conditions such as turbulence and wind gradient.

DEVIATION FROM NORMAL TECHNIQUES

Deviations from normal landing techniques are the most common causes of tail strikes. The mainreasons for this are due to:• Allowing the speed to decrease well below VAPP before flare

Flying at too low speed means high angle of attack and high pitch attitude, thus reducing groundclearance. When reaching the flare height, the pilot will have to significantly increase the pitchattitude to reduce the sink rate. This may cause the pitch to go beyond the critical angle.

• Prolonged hold off for a smooth touch downAs the pitch increases, the pilot needs to focus further ahead to assess the aircraft's position inrelation to the ground. The attitude and distance relationship can lead to a pitch attitude increasebeyond the critical angle.

• Too high flareA high flare can result in a combined decrease in airspeed and a long float. Since both lead to anincrease in pitch attitude, the result is reduced tail clearance.

• Too high sink rate, just prior reaching the flare heightIn case of too high sink rate close to the ground, the pilot may attempt to avoid a firm touch downby commanding a high pitch rate. This action will significantly increase the pitch attitude and, asthe resulting lift increase may be insufficient to significantly reduce the sink rate, the high pitchrate may be difficult to control after touch down, particularly in case of bounce.

• Bouncing at touch downIn case of bouncing at touch down, the pilot may be tempted to increase the pitch attitude toensure a smooth second touch down. If the bounce results from a firm touch down, associatedwith high pitch rate, it is important to control the pitch so that it does not further increase beyondthe critical angle.

APPROACH AND LANDING TECHNIQUES

A stabilized approach is essential for achieving successful landings. It is imperative that the flareheight be reached at the appropriate airspeed and flight path angle. The A/THR and FPV areeffective aids to the pilot.VAPP should be determined with the wind corrections (provided in FCOM/QRH) by using theFMGS functions. As a reminder, when the aircraft is close to the ground, the wind intensity tends todecrease and the wind direction to turn (direction in degrees decreasing in the northern latitudes).




Both effects may reduce the head wind component close to the ground and the wind correction toVAPP is there to compensate for this effect.When the aircraft is close to the ground, high sink rate should be avoided, even in an attempt tomaintain a close tracking of the glideslope. Priority should be given to the attitude and sink rate. If anormal touchdown distance is not possible, a go-around should be performed.If the aircraft has reached the flare height at VAPP, with a stabilized flight path angle, the normalSOP landing technique will lead to the right touchdown attitude and airspeed.During the flare, the pilot should not concentrate on the airspeed, but only on the attitude withexternal cues.Specific PNF call outs have been reinforced for excessive pitch attitude at landing.After touch down, the pilot must "fly" the nosewheel smoothly, but without delay, on to the runway,and must be ready to counteract any residual pitch up effect of the ground spoilers. However, themain part of the spoiler pitch up effect is compensated by the flight control law itself.

BOUNCING AT TOUCH DOWN

In case of light bounce, maintain the pitch attitude and complete the landing, while keeping thethrust at idle. Do not allow the pitch attitude to increase, particularly following a firm touch down witha high pitch rate.In case of high bounce, maintain the pitch attitude and initiate a go-around. Do not try to avoid asecond touch down during the go-around. Should it happen, it would be soft enough to preventdamage to the aircraft, if pitch attitude is maintained.Only when safely established in the go-around, retract flaps one step and the landing gear. A landingshould not be attempted immediately after high bounce, as thrust may be required to soften thesecond touch down and the remaining runway length may be insufficient to stop the aircraft.

CUMULATIVE EFFECTS

No single factor should result in a tail strike, but accumulation of several can significantly reduce themargin.


NORMAL OPERATIONSGO AROUND



Failure to recognize the need for and to execute a go-around, when required, is a major cause ofapproach and landing accidents. Because a go-around is an infrequent occurrence, it is important tobe "go-around minded". The decision to go-around should not be delayed, as an early go-around issafer than a last minute one at lower altitude.

CONSIDERATIONS ABOUT GO-AROUNDIdent.: NO-170-00005593.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

A go-around must be considered if:• There is a loss or a doubt about situation awareness• If there is a malfunction which jeopardizes the safe completion of the approach e.g. major navigation

problem• ATC changes the final approach clearance resulting in rushed action from the crew or potentially

unstable approach• The approach is unstable in speed, altitude, and flight path in such a way that stability will not be

obtained by 1 000 ft IMC or 500 ft VMC.• Any GPWS, TCAS or windshears alert occur• Adequate visual cues are not obtained reaching the minima.




AP/FD GO-AROUND PHASE ACTIVATIONIdent.: NO-170-00005594.0001001 / 26 MAR 08Criteria: P4319, P6197, SA�

1 Applicable to: MSN 0029-0031, 0034-0038, 0040-0041, 0043, 0045-0051, 0056-0058, 0069-0072, 0074-0075, 0078-0080, 0083, 0085-0086,0089-0090, 0093-0097, 0104, 0110-0111, 0113-0114, 0116-0119, 0121, 0123-0125, 0132, 0135, 0137, 0140, 0142, 0147, 0152-0153, 0157,0160-0164, 0167-0172, 0179-0180, 0189-0190, 0192, 0196-0197, 0200-0202, 0205-0206, 0208-0209, 0212-0213, 0216-0219, 0221-0222, 0225,0229-0230, 0245, 0247, 0252, 0256-0263, 0267-0269, 0272-0273, 0275-0276, 0280-0282, 0288, 0291-0301, 0304, 0306-0308, 0313-0314,0316, 0318-0322, 0326-0329, 0331-0332, 0336, 0338-0340, 0343-0349, 0353-0355, 0357-0358, 0360-0365, 0367-0373, 0376, 0379-0383,0385-0394, 0396-0402, 0405-0406, 0408, 0410-0418, 0420, 0422-0423, 0425, 0428, 0430-0432, 0435-0437, 0439, 0441-0444, 0446-0447,0449-0452, 0454, 0456-0458, 0460-0465, 0467-0470, 0472-0476, 0478-0479, 0482-0487, 0489-0490, 0492-0493, 0496, 0499-0508,0510-0512, 0518, 0523, 0525, 0528, 0530-0531, 0534, 0539, 0542, 0549, 0554, 0558, 0560-0561, 0563-0564, 0567-0569, 0571, 0575,0579-0580, 0587, 0589-0590, 0592, 0594-0595, 0597, 0601, 0604-0605, 0607, 0609-0611, 0613-0617, 0619, 0622-0624, 0626-0628, 0630,0634, 0636, 0638-0639, 0641, 0645, 0648-0652, 0655, 0658-0659, 0662, 0665-0667, 0669, 0671, 0677-0679, 0683, 0685-0686, 0689-0690,0692, 0694, 0699-0700, 0702, 0706, 0717, 0723-0724, 0726, 0729, 0737-0739, 0743-0745, 0748-0749, 0751, 0754, 0759, 0766-0767, 0772,0775, 0778, 0780, 0783, 0786-0788, 0792, 0798-0799, 0801, 0804, 0807, 0814, 0818, 0820, 0824-0826, 0828, 0830, 0832-0834, 0836, 0838,0842-0843, 0846-0847, 0850-0854, 0857-0858, 0860, 0862, 0865, 0867, 0869, 0871, 0873, 0875-0876, 0880, 0882-0883, 0886-0888, 0893,0897-0898, 0901, 0903, 0907, 0909, 0911, 0913-0914, 0916, 0918, 0921, 0923, 0925, 0939, 0944, 0948, 0952, 0954-0955, 0958, 0962-0965,0967, 0975, 0980-0981, 0984, 0986, 0988-0990, 0996, 1001, 1004-1006, 1008-1009, 1011, 1017, 1022, 1029, 1031-1032, 1037, 1041-1042,1058, 1062, 1071-1072, 1076, 1078, 1085, 1090-1091, 1093, 1108, 1117, 1126, 1129, 1131, 1149, 1164-1165, 1167, 1187, 1191, 1194-1196, 1199,1204, 1218, 1227, 1230, 1249, 1316, 1324-1325, 1345-1346, 1392, 1408, 1414, 1421, 1434, 1438, 1453, 1456, 1459, 1479, 1483, 1487, 1498,1501, 1520, 1535, 1543, 1549, 1567, 1570, 1582, 1633, 1641, 1646, 1659, 1662, 1683, 1685, 1693, 1700, 1709, 1714, 1738, 1746, 1752, 1766,1774, 1789, 1796, 1800, 1810, 1812, 1815, 1819-1820, 1824, 1828, 1833, 1839, 1870, 1875, 1897, 1923, 1959, 1976, 1982, 1990, 2002, 2013,2026, 2028, 2039, 2047, 2082, 2087, 2092, 2095, 2369, 2373, 2464, 2474, 2618, 2641

The go-around phase is activated when the thrust levers are set to TOGA, provided the flap lever isselected to Flap 1 or greater. The missed approach becomes the active F-PLN and the previouslyflown approach is strung back into the F-PLN.For the go-around, the appropriate flying reference is the attitude, since it is dynamic manoeuvre. So,if the "bird" is ON, the PF will ask the PNF to select HDG/VS, in order to remove the "bird". This alsopermits to replace the FPD by the FD bars, if the flight director is in use.If the autopilot or the flight director is in use, SRS and GA TRK modes engage.If the autopilot and both flight directors are off, the PF will maintain 15 ° of pitch.If TOGA thrust is not required during a go-around for any reason, e.g. an early go-around orderedby ATC, it is essential that thrust levers are set to TOGA momentarily to sequence the F-PLN. If thisis not done, the destination airfield will be sequenced and the primary F-PLN will become PPOS -DISCONT- .





2 Applicable to: MSN 0002-0021, 0033, 0039, 0042, 0044, 0052-0055, 0059-0068, 0073, 0076-0077, 0081-0082, 0084, 0087-0088, 0091,0098-0103, 0108-0109, 0112, 0115, 0120, 0122, 0126-0131, 0133-0134, 0136, 0138-0139, 0141, 0143-0146, 0148-0151, 0154-0156, 0158-0159,0165-0166, 0173-0178, 0181-0188, 0191, 0193-0195, 0198-0199, 0203-0204, 0207, 0210-0211, 0214-0215, 0220, 0223-0224, 0226-0228,0231-0244, 0246, 0248-0251, 0253-0255, 0264-0266, 0270, 0274, 0277-0279, 0283-0287, 0289-0290, 0302-0303, 0305, 0309-0312, 0315,0317, 0323-0325, 0330, 0333-0335, 0337, 0341-0342, 0350-0352, 0356, 0359, 0366, 0375, 0377-0378, 0384, 0395, 0403-0404, 0407, 0409,0419, 0421, 0424, 0426-0427, 0429, 0434, 0438, 0440, 0445, 0448, 0453, 0455, 0459, 0466, 0471, 0477, 0480, 0488, 0491, 0494-0495,0497-0498, 0509, 0513-0517, 0519-0522, 0524, 0526-0527, 0529, 0532-0533, 0535-0538, 0540-0541, 0543-0548, 0550-0553, 0555-0557, 0559,0562, 0565-0566, 0570, 0572-0574, 0576-0578, 0581-0586, 0588, 0591, 0593, 0596, 0598-0600, 0603, 0606, 0608, 0612, 0618, 0620-0621,0625, 0629, 0631-0633, 0635, 0637, 0640, 0642-0644, 0646-0647, 0653-0654, 0656-0657, 0660-0661, 0663-0664, 0668, 0670, 0672-0676,0680-0682, 0684, 0687-0688, 0691, 0693, 0695-0698, 0701, 0703-0705, 0707-0716, 0718-0722, 0725, 0727-0728, 0730-0736, 0740-0742,0746-0747, 0750, 0752, 0755-0758, 0760-0765, 0768-0771, 0773-0774, 0776-0777, 0779, 0781-0782, 0784-0785, 0790-0791, 0793-0797,0800, 0802-0803, 0805-0806, 0808-0813, 0815-0817, 0819, 0821-0823, 0827, 0829, 0831, 0835, 0837, 0839-0841, 0844-0845, 0848-0849,0855-0856, 0859, 0861, 0863-0864, 0866, 0868, 0870, 0872, 0874, 0877-0879, 0881, 0884-0885, 0889-0892, 0894-0896, 0899-0900,0902, 0904-0906, 0908, 0910, 0912, 0915, 0917, 0919-0920, 0922, 0924, 0926-0938, 0940-0943, 0945-0947, 0949-0951, 0953, 0956-0957,0959-0961, 0966, 0968-0974, 0976-0979, 0982-0983, 0985, 0987, 0991-0995, 0997-1000, 1002-1003, 1007, 1010, 1012-1016, 1018-1021,1023-1028, 1030, 1033-1036, 1038-1040, 1043-1057, 1059-1061, 1063-1070, 1073-1075, 1077, 1079-1084, 1086-1089, 1092, 1094-1107,1109-1116, 1118-1125, 1127-1128, 1130, 1132-1148, 1150-1163, 1166, 1168-1185, 1188-1190, 1192-1193, 1197-1198, 1200-1203, 1205-1217,1219-1226, 1228-1229, 1231-1248, 1250-1315, 1317-1323, 1326-1344, 1347-1391, 1393-1407, 1409-1413, 1415-1420, 1422-1433, 1435-1437,1439-1452, 1454-1455, 1457-1458, 1460-1478, 1480-1482, 1484-1486, 1488-1497, 1499-1500, 1502-1519, 1521-1534, 1536-1542, 1544-1548,1550-1566, 1568-1569, 1571-1581, 1583-1632, 1634-1640, 1642-1645, 1647-1658, 1660-1661, 1663-1682, 1684, 1686-1692, 1694-1699,1701-1708, 1710-1713, 1715-1737, 1739-1745, 1747-1751, 1753-1765, 1767-1773, 1775-1788, 1790-1795, 1797-1799, 1801-1809, 1811, 1814,1816-1818, 1821-1823, 1825-1827, 1829-1832, 1834-1838, 1840-1869, 1871-1874, 1876-1896, 1898-1922, 1924-1958, 1960-1975, 1977-1981,1983-1989, 1991-2001, 2003-2012, 2014-2024, 2027, 2029-2038, 2040-2046, 2048-2081, 2083-2086, 2088-2091, 2093-2094, 2096-2368,2370-2372, 2374-2463, 2465-2473, 2475-2617, 2619-2640, 2642-3996

The go-around phase is activated when the thrust levers are set to TOGA, provided the flap lever isselected to Flap 1 or greater. The FDs bars are displayed automatically and SRS and GA TRK modesengage. The missed approach becomes the active F-PLN and the previously flown approach is strungback into the F-PLN.For the go-around, the appropriate flying reference is the attitude, since it is dynamic manoeuvre. Thisis why, if the "bird" is ON, it is automatically removed, and the FD bars automatically replace the FPD.If TOGA thrust is not required during a go-around for any reason, e.g. an early go-around ordered byATC, it is essential that thrust levers are set to TOGA momentarily to sequence the F-PLN. If this is notdone, the destination airfield will be sequenced and the primary F-PLN will become PPOS - DISCONT-




GO-AROUND PHASEIdent.: NO-170-00005595.0001001 / 02 JUL 08Criteria: P4319, P6197, SA�


GO AROUND WITH FD ON

The SRS mode guides the aircraft with a maximum speed of VAPP or IAS at time of TOGA selection(limited to maximum of VLS +25 with all engines operative or VLS +15 with one engine inoperativewith FMS 2) until the acceleration altitude where the target speed increases to green dot.Some FMS misbehaviour may prevent this automatic target speed increase. Should this occur,pulling the FCU ALT knob for OP CLB manually disengages SRS mode and allows the target speedto increase to green dot. It should be noted however, that the target speed increases to green dotspeed as soon as ALT* mode engages when approaching the FCU clearance altitude.The GA TRK mode guides the aircraft on the track memorised at the time of TOGA selection. Themissed approach route becomes the ACTIVE F-PLN provided the waypoints have been correctlysequenced on the approach. Pushing for NAV enables the missed approach F-PLN to be followed.Above the go-around acceleration altitude, or when the flight crew engages another vertical mode(CLB, OP CLB), the target speed is green dot.

GO AROUND WITH FD OFF

The PF maintains 15 ° of pitch.The crew will not select the FD ON before the acceleration altitude, since this would not activate theSRS mode. (V/S mode would be activated, maintaining the V/S at mode engagement).At the thrust reduction/acceleration altitude, the crew will set the selected speed to green dot beforesetting CLB thrust, since the autothrust will activate in selected speed mode.The crew will then set the FD ON , and select the appropriate modes.




Ident.: NO-170-00005595.0002001 / 02 JUL 08Criteria: 22-1058, P4319, SA�


The SRS mode guides the aircraft with a maximum speed of VAPP or IAS at time of TOGA selection(limited to maximum of VLS +25 with all engines operative or VLS +15 with one engine inoperative withFMS 2) until the acceleration altitude where the target speed increases to green dot.Some FMS misbehaviour may prevent this automatic target speed increase. Should this occur, pullingthe FCU ALT knob for OP CLB manually disengages SRS mode and allows the target speed toincrease to green dot. It should be noted however, that the target speed increases to green dot speedas soon as ALT* mode engages when approaching the FCU clearance altitude.The GA TRK mode guides the aircraft on the track memorised at the time of TOGA selection. Themissed approach route becomes the ACTIVE F-PLN provided the waypoints have been correctlysequenced on the approach. Pushing for NAV enables the missed approach F-PLN to be followed.Above the go-around acceleration altitude, or when the flight crew engages another vertical mode(CLB, OP CLB), the target speed is green dot.

ENGINES ACCELERATIONIdent.: NO-170-00005596.0001001 / 23 MAY 08Criteria: SA�Applicable to: ALL

When the pilot sets TOGA thrust for go-around, it takes some time for the engines to spool up due tothe acceleration capability of the high by pass ratio engines. Therefore, the pilot must be aware that the




aircraft will initially loose some altitude. This altitude loss will be greater if initial thrust is close to idleand/or the aircraft speed is lower than VAPP.

altitude loss following a go-around

LEAVING THE GO-AROUND PHASEIdent.: NO-170-00005597.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The purpose of leaving the go-around phase is to obtain the proper target speed and properpredictions depending upon the strategy chosen by the crew. During the missed approach, the crewwill elect either of the following strategies:• Fly a second approach• Carry out a diversion

SECOND APPROACH

If a second approach is to be flown, the crew will activate the approach phase in the MCDU PERFGO-AROUND page. The FMS switches to Approach phase and the target speed moves accordingto the flaps lever setting, e.g. green dot for Flaps 0.The crew will ensure proper waypoint sequencing during the second approach in order to have themissed approach route available, should a further go-around be required.

DIVERSION

Once the aircraft path is established and clearance has been obtained, the crew will modify theFMGS to allow the FMGS switching from go-around phase to climb phase:• If the crew has prepared the ALTN FPLN in the active F-PLN, a lateral revision at the TO WPT is

required to access the ENABLE ALTN prompt. On selecting the ENABLE ALTN prompt, the lateralmode reverts to HDG if previously in NAV. The aircraft will be flown towards the next waypointusing HDG or NAV via a DIR TO entry.

• If the crew has prepared the ALTN FPLN in the SEC F-PLN, the SEC F-PLN will be activated, anda DIR TO performed as required. AP/FD must be in HDG mode for the ACTIVATE SEC F-PLNprompt to be displayed.




• If the crew has not prepared the ALTN FPLN, a selected climb will be initiated. Once establishedin climb and clear of terrain, the crew will make a lateral revision at any waypoint to insert a NEWDEST. The route and a CRZ FL (on PROG page) can be updated as required.

REJECTED LANDINGIdent.: NO-170-00005598.0001001 / 24 APR 08Criteria: SA�Applicable to: ALL

A rejected landing is defined as a go-around manoeuvre initiated below the minima.Once the decision is made to reject the landing, the flight crew must be committed to proceed with thego-around manoeuvre and not be tempted to retard the thrust levers in a late decision to complete thelanding.TOGA thrust must be applied but a delayed flap retraction should be considered. If the aircraft is onthe runway when thrust is applied, a CONFIG warning will be generated if the flaps are in conf full.The landing gear should be retracted when a positive climb is established with no risk of further touchdown. Climb out as for a standard go-around.In any case, if reverse thrust has been applied, a full stop landing must be completed.


NORMAL OPERATIONSTAXI IN


BRAKE FANS Ident.: NO-180-00005601.0001001 / 21 APR 08Criteria: SA�Applicable to: ALL

The use of brake fans could increase oxidation of the brake surface hot spots if brakes are notthermally equalized, leading to the rapid degradation of the brakes. For this reason, selection of brakefans should be delayed until approximately 5 min after touchdown or just prior to stopping at the gate(whichever occurs first). Selecting brake fans before reaching the gate allows avoiding blowing carbonbrake dust on ground personal.




BRAKE TEMPERATUREIdent.: NO-180-00005602.0001001 / 23 MAY 08Criteria: 32-1174, 32-1242, 32-1276, P4507, SA�

1 Applicable to: MSN 0002-0042, 0044-0112, 0115-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476,0478-0483, 0485-0487, 0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534,0537, 0539-0540, 0542-0543, 0545-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569, 0571-0574, 0577-0580,0582, 0584-0585, 0587-0590, 0592, 0594, 0596, 0598, 0600-0603, 0605, 0607-0613, 0615-0619, 0621-0630, 0634-0641, 0643-0651,0653-0658, 0660-0662, 0665, 0667, 0669-0673, 0676, 0678-0679, 0681-0683, 0685-0686, 0688-0691, 0693-0698, 0700-0714, 0716-0724,0726-0730, 0732-0745, 0747-0760, 0762-0764, 0766-0770, 0772-0774, 0776, 0778-0780, 0782-0786, 0788-0791, 0793-0795, 0797-0801,0803-0805, 0807, 0809, 0812-0814, 0816-0818, 0820-0822, 0824-0826, 0828-0834, 0836-0840, 0842-0847, 0849-0851, 0853-0854, 0856-0863,0865-0877, 0879-0886, 0888-0890, 0892-0900, 0902-0907, 0909-0914, 0916-0919, 0921-0925, 0927-0934, 0936-0939, 0942-0953, 0955,0957-0958, 0960, 0962, 0964-0967, 0969, 0971-0973, 0975-0982, 0984-0986, 0988-0990, 0992, 0994, 0996-1003, 1005, 1007, 1009-1011,1013-1014, 1016, 1018-1020, 1022, 1025-1026, 1028-1041, 1043-1044, 1046-1059, 1061-1079, 1081-1093, 1095-1132, 1134-1143, 1145-1152,1154-1160, 1162-1173, 1175-1184, 1187, 1189-1194, 1196-1198, 1200-1201, 1203, 1205-1206, 1208-1213, 1215-1217, 1221-1226, 1228-1232,1234-1237, 1239-1240, 1242-1249, 1251-1259, 1261-1272, 1274-1275, 1277-1292, 1294-1298, 1300-1306, 1308-1332, 1334-1355, 1357-1365,1367-1398, 1400-1402, 1404-1406, 1409-1411, 1413-1416, 1419-1420, 1422-1423, 1426-1427, 1429-1430, 1432, 1434-1435, 1437, 1439-1441,1443-1446, 1448-1450, 1452-1454, 1456-1457, 1459-1461, 1463-1464, 1466-1471, 1473-1475, 1477-1480, 1482-1486, 1488-1491, 1493-1495,1497-1498, 1500-1502, 1504-1510, 1512-1516, 1518, 1520, 1522-1524, 1526-1530, 1532-1535, 1537-1538, 1540-1553, 1555-1571, 1573-1586,1588-1595, 1597-1601, 1603-1606, 1608-1610, 1612-1613, 1615-1618, 1620-1622, 1624-1628, 1630-1631, 1633-1635, 1637, 1639-1641,1643-1650, 1652-1657, 1659-1665, 1667-1669, 1671-1674, 1676-1680, 1682-1689, 1692-1694, 1696-1700, 1702-1703, 1705-1706, 1708-1710,1712, 1714-1715, 1717-1719, 1721-1723, 1725, 1727-1733, 1735-1747, 1749-1762, 1764-1771, 1773-1775, 1777-1782, 1784-1787, 1789-1793,1795-1797, 1799-1806, 1808-1810, 1812-1816, 1818-1835, 1837-1842, 1844-1847, 1849, 1851-1858, 1860-1868, 1870-1877, 1879-1880,1882-1886, 1888-1904, 1906-1920, 1922-1925, 1927, 1929-1931, 1933-1940, 1942-1945, 1947-1949, 1951-1952, 1954-1955, 1957-1959,1961-1965, 1968-1969, 1971, 1973, 1975-1976, 1979-1983, 1986-1987, 1989-1993, 1996-2004, 2006-2020, 2022-2040, 2042-2044, 2046-2054,2056-2059, 2061-2063, 2065-2066, 2068-2075, 2077-2079, 2081-2104, 2106, 2108-2109, 2112-2114, 2116, 2118-2189, 2191-2207, 2209-2210,2212-2215, 2217-2219, 2221-2225, 2227-2233, 2235-2246, 2248-2254, 2256-2260, 2262-2266, 2268-2269, 2271-2289, 2291-2302, 2304,2306-2308, 2310-2314, 2316-2319, 2321-2322, 2325-2329, 2331-2336, 2338-2341, 2343-2350, 2352-2356, 2358-2362, 2364-2380, 2382-2409,2411-2461, 2463-2471, 2473-2475, 2477-2479, 2481-2487, 2489-2520, 2522-2529, 2531-2535, 2537-2542, 2544-2548, 2550-2552, 2554-2562,2564-2589, 2591-2598, 2600-2609, 2611-2652, 2654-2681, 2683-2686, 2688-2706, 2708-2712, 2714-2725, 2727-2729, 2731-2735, 2737-2740,2742-2755, 2757-2758, 2760-2766, 2768-2792, 2794-2798, 2800-2808, 2810-2822, 2824-2861, 2863-2867, 2869-2881, 2883-2894, 2896-2902,2904-2911, 2913-2915, 2917-2918, 2920-2926, 2928-2932, 2934-2935, 2937-2956, 2958-2964, 2966-2970, 2972-2973, 2975-2995, 2997-2998,3000-3004, 3006-3012, 3014, 3016-3021, 3023-3033, 3035-3050, 3052-3066, 3068-3069, 3071-3074, 3076-3080, 3082-3097, 3099-3105,3107-3111, 3113-3119, 3121-3125, 3127-3129, 3131-3145, 3147-3190, 3192-3197, 3199-3206, 3208-3211, 3213-3216, 3218-3221, 3223-3228,3230-3232, 3234, 3236-3240, 3242-3246, 3248, 3250, 3252-3253, 3255-3261, 3263-3264, 3266, 3268-3273, 3275-3282, 3284-3289,3291-3293, 3295-3296, 3298-3301, 3303-3306, 3308-3314, 3316-3321, 3323-3325, 3327-3328, 3330-3333, 3335-3338, 3341-3349, 3351-3354,3356-3359, 3361-3366, 3368, 3370-3371, 3373-3381, 3383-3386, 3388-3396, 3398, 3400, 3402-3404, 3406-3418, 3420-3428, 3430-3433,3435-3440, 3442-3457, 3460-3461, 3463-3470, 3472-3492, 3494-3497, 3499-3503, 3505-3506, 3508-3511, 3513-3521, 3524, 3526, 3528-3538,3540-3545, 3547-3551, 3553-3556, 3558-3565, 3567-3572, 3574, 3576-3582, 3585-3586, 3588-3591, 3594-3599, 3601-3611, 3613-3618,3620-3622, 3624, 3626-3628, 3630-3632, 3634-3635, 3640-3644, 3646-3652, 3654, 3656-3664, 3666-3668, 3670-3672, 3674-3677,3679-3680, 3683-3687, 3689-3707, 3709-3711, 3713-3716, 3718-3721, 3723-3724, 3726-3729, 3731-3736, 3739, 3741-3748, 3750-3751,3753-3760, 3762-3763, 3765, 3767-3783, 3785-3791, 3793-3795, 3807-3813, 3815, 3817-3819, 3863, 3871-3877, 3937, 3638, 3797-3805,3821-3829, 3831-3846, 3848-3857, 3859-3861, 3865-3866, 3868, 3880, 3882-3883, 3885-3892, 3894-3898, 3900-3915, 3917-3919, 3921-3923,3925, 3927, 3931-3933, 3935, 3939, 3941-3943, 3945-3947, 3949-3950, 3952-3954, 3956-3959, 3962, 3965, 3967-3968, 3970-3972,3983-3984, 3995

If there is a significant difference in brake temperature between the wheels of the same gear, whenreaching the gate, this materializes a potential problem with brake and a maintenance action is duee.g. if one wheel reaches the limit temperature of 600 °C while all others wheels brakes indicate lessthan 450 °C, this indicates that there is a potential problem of brake binding or permanent brakeapplication on that wheel. Conversely, if one wheel brake is at or below 60 °C whereas the others are




beyond 210 °C, this indicates that there is a potential loss of braking on that wheel. Selecting brakefans before reaching the gate allows avoiding blowing carbon brake dust on ground personal.If brake temperature is above 500 °C with fans OFF (350 °C fans ON ), use of the parkingbrake, unless operationally necessary, should be avoided to prevent brake damage.If one brake temperature exceeds 900 °C, a maintenance action is due.The MEL provides information regarding brake ground cooling time, both with and without brake fans

.

Ident.: NO-180-00005602.0002001 / 23 MAY 08Criteria: 32-1174, K2113, P4507, SA�

2 Applicable to: MSN 0043, 0113-0114, 0434, 0477, 0488, 0494-0495, 0513-0517, 0524, 0526, 0532, 0535, 0552, 0570, 0575-0576, 0581, 0583,0586, 0593, 0599, 0642, 0659, 0765, 0806, 0810, 0819, 0827, 0835, 0848, 0891, 0920, 0935, 0940-0941, 0959, 0961, 0968, 0974, 1174, 1185,1220, 1241, 1356, 1407, 1418, 1424, 1458, 1511, 1636, 1670, 1734, 1850, 1926, 1978, 2041, 2045, 2110, 2115, 2208, 2226, 2247, 2290, 2472,2488, 2563, 3297

If there is a significant difference in brake temperature between the wheels of the same gear, whenreaching the gate, this materializes a potential problem with brake and a maintenance action is duee.g. if one wheel reaches the limit temperature of 425 °C while all others wheels brakes indicate lessthan 325 °C, this indicates that there is a potential problem of brake binding or permanent brakeapplication on that wheel. Conversely, if one wheel brake is at or below 60 °C whereas the others arebeyond 160 °C, this indicates that there is a potential loss of braking on that wheel. Selecting brakefans before reaching the gate allows avoiding blowing carbon brake dust on ground personal.If brake temperature is above 500 °C with fans OFF (350 °C fans ON ), use of the parkingbrake, unless operationally necessary, should be avoided to prevent brake damage.If one brake temperature exceeds 500 °C, a maintenance action is due.The MEL provides information regarding brake ground cooling time, both with and without brake fans

.




Ident.: NO-180-00005602.0003001 / 23 MAY 08Criteria: 32-1136, 32-1263, K2113, P3341, SA�

3 Applicable to: MSN 0364, 0385, 0412, 0458, 0468, 0473-0474, 0484, 0493, 0498, 0502, 0505, 0509, 0518-0522, 0529, 0538, 0541, 0544,0550, 0555, 0557, 0560, 0563-0564, 0567, 0591, 0595, 0597, 0604, 0606, 0614, 0620, 0631-0633, 0652, 0663-0664, 0666, 0668, 0674-0675,0677, 0680, 0684, 0687, 0692, 0699, 0715, 0725, 0731, 0746, 0761, 0771, 0775, 0777, 0781, 0787, 0792, 0796, 0802, 0808, 0811, 0815, 0823,0841, 0852, 0855, 0864, 0878, 0887, 0901, 0908, 0915, 0926, 0954, 0956, 0963, 0970, 0983, 0987, 0991, 0993, 0995, 1004, 1006, 1008,1012, 1015, 1017, 1021, 1023-1024, 1027, 1042, 1045, 1060, 1080, 1094, 1133, 1144, 1153, 1161, 1188, 1195, 1199, 1202, 1204, 1207, 1214,1218-1219, 1227, 1233, 1238, 1250, 1260, 1273, 1276, 1293, 1299, 1307, 1333, 1366, 1399, 1403, 1408, 1412, 1417, 1421, 1425, 1428, 1431,1433, 1436, 1438, 1442, 1447, 1451, 1455, 1462, 1465, 1472, 1476, 1481, 1487, 1492, 1496, 1499, 1503, 1517, 1519, 1521, 1525, 1531, 1536,1539, 1554, 1572, 1587, 1596, 1602, 1607, 1611, 1614, 1619, 1623, 1629, 1632, 1638, 1642, 1651, 1658, 1666, 1675, 1681, 1690-1691, 1695,1701, 1704, 1707, 1711, 1713, 1716, 1720, 1724, 1726, 1748, 1763, 1772, 1776, 1783, 1788, 1794, 1798, 1807, 1811, 1817, 1836, 1843, 1848,1859, 1869, 1878, 1881, 1887, 1905, 1921, 1928, 1932, 1941, 1946, 1950, 1953, 1956, 1960, 1966-1967, 1970, 1972, 1974, 1977, 1984, 1988,1994-1995, 2005, 2021, 2055, 2060, 2064, 2067, 2076, 2080, 2105, 2107, 2117, 2190, 2211, 2216, 2220, 2234, 2255, 2261, 2267, 2270, 2303,2305, 2309, 2315, 2320, 2323-2324, 2330, 2337, 2342, 2351, 2357, 2363, 2381, 2410, 2462, 2476, 2480, 2521, 2530, 2536, 2543, 2549, 2553,2590, 2599, 2610, 2653, 2682, 2687, 2707, 2713, 2726, 2730, 2736, 2741, 2756, 2759, 2767, 2793, 2799, 2809, 2823, 2862, 2868, 2882, 2895,2903, 2912, 2916, 2919, 2927, 2933, 2936, 2957, 2965, 2971, 2974, 2996, 2999, 3005, 3013, 3015, 3022, 3034, 3051, 3067, 3070, 3075, 3081,3098, 3106, 3112, 3120, 3126, 3130, 3146, 3191, 3198, 3207, 3212, 3217, 3222, 3229, 3233, 3235, 3241, 3247, 3249, 3251, 3254, 3262, 3265,3267, 3274, 3283, 3290, 3294, 3302, 3307, 3315, 3322, 3326, 3329, 3334, 3339-3340, 3350, 3355, 3360, 3367, 3369, 3372, 3382, 3387, 3397,3399, 3401, 3405, 3419, 3429, 3434, 3441, 3458-3459, 3462, 3471, 3493, 3498, 3504, 3507, 3512, 3522-3523, 3525, 3527, 3539, 3546, 3552,3557, 3566, 3573, 3575, 3583-3584, 3587, 3592-3593, 3600, 3612, 3619, 3623, 3625, 3629, 3633, 3636-3637, 3639, 3645, 3653, 3655, 3665,3669, 3673, 3678, 3681-3682, 3688, 3708, 3712, 3717, 3722, 3725, 3730, 3737-3738, 3740, 3749, 3752, 3761, 3764, 3766, 3784, 3792, 3796,3806, 3814, 3816, 3820, 3847, 3858, 3862, 3867, 3878-3879, 3920, 3830, 3864, 3869, 3881, 3884, 3893, 3899, 3916, 3924, 3926, 3928-3930,3934, 3936, 3938, 3940, 3944, 3948, 3951, 3955, 3960, 3964, 3966, 3969, 3977-3981, 3989-3993, 3996

If there is a significant difference in brake temperature between the wheels of the same gear, whenreaching the gate, this materializes a potential problem with brake and a maintenance action is due.e.g. if one wheel reaches the limit temperature of 600 °C while all others wheels brakes indicate lessthan 450 °C, this indicates that there is a potential problem of brake binding or permanent brakeapplication on that wheel. Conversely, if one wheel brake is at or below 60 °C whereas the others arebeyond 210 °C, this indicates that there is a potential loss of braking on that wheel. Selecting brakefans before reaching the gate allows avoiding blowing carbon brake dust on ground personal.If brake temperature is above 500 °C with fans OFF (350 °C fans ON ), use of the parkingbrake, unless operationally necessary, should be avoided to prevent brake damage.If one brake temperature exceeds 800 °C, a maintenance action is due.The MEL provides information regarding brake ground cooling time, both with and without brake fans

.

ENGINES COOLING PERIODIdent.: NO-180-00005604.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

To avoid engine thermal stress, it is required that the engine be operated at, or near, idle for a coolingperiod as described in FCOM (Refer to FCOM/PRO-NOR-SOP-25-A PARKING - ENG MASTER 1AND 2)




TAXI WITH ONE ENGINE SHUTDOWNIdent.: NO-180-00005605.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Refer to NO-040 TAXI WITH ONE ENGINE SHUTDOWN

AFTER LANDING FLOW PATTERNIdent.: NO-180-00005606.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

AFTER LANDING FLOW PATTERN

ABNORMAL OPERATIONS


ABNORMAL OPERATIONSPRELIMINARY PAGES

TABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET AO-PLP-TOC. P 1/2FCTM 09 JAN 09

AO-PLP. PRELIMINARY PAGESTABLE OF CONTENTS........................................................................................................................................... 1/2SUMMARY OF HIGHLIGHTS.................................................................................................................................. 1/2

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AO-010. GENERALPREFACE................................................................................................................................................................. 1/6LANDING DISTANCE PROCEDURE...................................................................................................................... 1/6Vapp DETERMINATION...........................................................................................................................................1/6IN FLIGHT LANDING DISTANCE CALCULATION FOLLOWING FAILURES..........................................................4/6

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AO-020. OPERATING TECHNIQUESLOW SPEED ENGINE FAILURE........................................................................................................................... 1/20REJECTED TAKEOFF........................................................................................................................................... 1/20INTRODUCTION TO EMERGENCY EVACUATION.............................................................................................. 4/20The Emergency Evacuation Procedure................................................................................................................. 6/20TASKSHARING IN CASE OF EMERGENCY EVACUATION ............................................................................... 7/20ENGINE FAILURE AFTER V1............................................................................................................................... 8/20ENGINE FAILURE DURING INITIAL CLIMB-OUT...............................................................................................11/20ENGINE FAILURE DURING CRUISE.................................................................................................................. 11/20ENGINE-OUT LANDING...................................................................................................................................... 14/20CIRCLING ONE ENGINE INOPERATIVE............................................................................................................14/20ONE ENGINE INOPERATIVE GO-AROUND ..................................................................................................... 15/20Thrust Levers Management in case of Inoperative Reverser(s).......................................................................... 16/20

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AO-022. AUTOFLIGHTFMGC FAILURE....................................................................................................................................................... 1/2

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AO-024. ELECTRICALINTRODUCTION TO EMERGENCY ELECTRICAL CONFIGURATION..................................................................1/6TECHNICAL BACKGROUND...................................................................................................................................1/6GENERAL GUIDELINES..........................................................................................................................................3/6REMAINING SYSTEMS........................................................................................................................................... 5/6

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AO-026. FIRE PROTECTIONPREFACE................................................................................................................................................................. 1/8SMOKE DETECTION AND PROCEDURE APPLICATION..................................................................................... 1/8



TABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET AO-PLP-TOC. P 2/2FCTM 09 JAN 09

COORDINATION WITH CABIN CREW .................................................................................................................. 3/8SMOKE/FUMES/AVNCS SMOKE PAPER PROCEDURE.......................................................................................4/8CARGO SMOKE...................................................................................................................................................... 7/8

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AO-027. FLIGHT CONTROLSABNORMAL FLAPS/SLATS CONFIGURATION......................................................................................................1/2

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AO-028. FUELFUEL LEAK.............................................................................................................................................................. 1/2

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AO-029. HYDRAULICHYDRAULIC GENERATION PARTICULARITIES....................................................................................................1/6DUAL HYDRAULIC FAILURES................................................................................................................................1/6REMAINING SYSTEMS........................................................................................................................................... 3/6REMAINING SYSTEMS ..........................................................................................................................................4/6

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AO-032. LANDING GEARLDG WITH ABNORMAL L/G................................................................................................................................... 1/2Nose Wheel Steering Fault...................................................................................................................................... 2/2

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AO-034. NAVIGATIONADR/IRS FAULT..................................................................................................................................................... 1/14UNRELIABLE AIRSPEED INDICATIONS.............................................................................................................. 2/14ADR CHECK PROC / UNRELIABLE SPEED INDICATION QRH PROCEDURE..................................................4/14DUAL RADIO ALTIMETER FAILURE...................................................................................................................13/14

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AO-070. POWER PLANTALL ENGINE FLAMEOUT....................................................................................................................................... 1/2

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AO-090. MISCELLANEOUSEMERGENCY DESCENT...................................................................................................................................... 1/10OVERWEIGHT LANDING...................................................................................................................................... 3/10CREW INCAPACITATION.......................................................................................................................................9/10

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ENV A318/A319/A320/A321 FLEET AO-PLP-SOH. P 1/2FCTM 09 JAN 09

LocalizationTitle

Page ID Reason

AO-020INTRODUCTION TO EMERGENCYEVACUATION

4/20 1 Solution actual effectivity changed:0005,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3752,3753,3754,3756,3757,3758,3759,3760,3761,3762,3763,3764,3765,3766,3767,3768,3769,3770,3771,3772,3773,3774,3775,3776,3777,3778,3779,3780,3781,3782,3783,3784,3785,3786,3787,3788,3789,3790,3791,3792,3793,3794,3795,3796,3797,3798,3799,3800,3801,3802,3803,3804,3805,3806,3807,3808,3809,3810,3811,3812,3813,3814,3816,3817,3818,3819,3820,3821,3822,3823,3824,3825,3826,3827,3828,3829,3830,3832,3833,3834,3835,3836,3837,3838,3839,3840,3841,3843,3844,3845,3847,3848,3849,3850,3851,3852,3853,3854,3855,3856,3857,3858,3859,3860,3861,3862,3863,3864,3865,3866,3867,3868,3869,3871,3872,3873,3874,3875,3876,3877,3878,3879,3880,3881,3882,3883,3884,3887,3888,3889,3890,3891,3892,3893,3894,3895,3896,3898,3899,3900,3901,3902,3903,3904,3905,3907,3908,3909,3910,3911,3912,3913,3915,3916,3917,3918,3919,3920,3922,3923,3924,3925,3926,3927,3928,3930,3931,3933,3934,3935,3936,3937,3938,3939,3940,3941,3943,3944,3945,3946,3947,3948,3949,3950,3951,3952,3953,3954,3955,3959,3960,3962,3964,3965,3966,3967,3968,3969,3970,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added, 0004,0006,0017,0036,1374,2500 removed

AO-020INTRODUCTION TO EMERGENCYEVACUATION

5/20 2 Solution actual effectivity changed:3815,3831,3846,3885,3886,3897,3906,3921,3932,3956 added

AO-020Thrust Levers Management in caseof Inoperative Reverser(s)


AO-020Thrust Levers Management in caseof Inoperative Reverser(s)


AO-024TECHNICAL BACKGROUND


AO-024TECHNICAL BACKGROUND


AO-024GENERAL GUIDELINES


AO-024GENERAL GUIDELINES


AO-026SMOKE DETECTION ANDPROCEDURE APPLICATION


AO-026SMOKE DETECTION ANDPROCEDURE APPLICATION


AO-026SMOKE/FUMES/AVNCS SMOKEPAPER PROCEDURE

4/8 3 Additional information: when the flight crew sets the electricalemergency configuration following a smoke detection in theavionic compartment, the ECAM displays a specific ELECEMER CONFIG procedure that takes into account the smokedetection.

AO-029REMAINING SYSTEMS


AO-029REMAINING SYSTEMS


AO-034ADR/IRS FAULT


AO-034ADR/IRS FAULT





ENV A318/A319/A320/A321 FLEET AO-PLP-SOH. P 2/2FCTM 09 JAN 09

LocalizationTitle

Page ID Reason

AO-034ADR CHECK PROC / UNRELIABLESPEED INDICATION QRHPROCEDURE


AO-034ADR CHECK PROC / UNRELIABLESPEED INDICATION QRHPROCEDURE


AO-090OVERWEIGHT LANDING



4/10 2 Solution actual effectivity changed:0639,0649,0697,0742,0885,0890,1038,1046,1069,1089,1095,1254,1269,1328,1331,1348,1358,1369,1515,3754,3757,3759,3763,3768,3770,3772,3774,3779,3788,3790,3794,3799,3801,3803,3808,3810,3818,3822,3824,3826,3828,3832,3834,3836,3838,3839,3841,3844,3845,3849,3851,3853,3854,3856,3860,3865,3872,3874,3876,3888,3890,3892,3895,3897,3901,3903,3905,3911,3918,3950,3962,3970,3983added, 1155,1170,1209,1325,1392 removed


5/10 3 Solution actual effectivity changed:0002,0003,0007,0010,0012,0013,0014,0016,0019,0020,0021,0043,0113,0114,0185added, 0288,0331 removed




8/10 5 Solution actual effectivity changed:0005,0288,0331,1155,1170,1209,1325,1392,3591,3698,3716,3723,3734,3736,3739,3741,3743,3745,3747,3748,3750,3753,3756,3758,3760,3762,3765,3767,3769,3771,3773,3775,3776,3777,3778,3780,3781,3782,3783,3785,3786,3787,3789,3791,3793,3795,3797,3798,3800,3802,3804,3805,3807,3809,3811,3812,3813,3815,3817,3819,3821,3823,3825,3827,3829,3831,3833,3835,3837,3840,3843,3846,3848,3850,3852,3855,3857,3859,3861,3863,3866,3868,3871,3873,3875,3877,3880,3882,3883,3885,3887,3889,3891,3894,3896,3898,3900,3902,3904,3906,3907,3908,3909,3910,3912,3913,3915,3917,3919,3921,3922,3923,3925,3927,3931,3933,3935,3937,3939,3941,3943,3945,3946,3947,3949,3952,3953,3954,3956,3959,3965,3967,3968,3971,3972,3984,3995added,0002,0003,0004,0006,0007,0010,0012,0013,0014,0016,0017,0019,0020,0021,0036,0043,0113,0114,0185,0639,0649,0697,0742,0885,0890,1038,1046,1069,1089,1095,1254,1269,1328,1331,1348,1358,1369,1374,1515,2500removed


ABNORMAL OPERATIONSGENERAL

ENV A318/A319/A320/A321 FLEET AO-010. P 1/6FCTM 09 JAN 09

PREFACEIdent.: AO-010-00005607.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The ABNORMAL OPERATIONS chapter highlights techniques that will be used in some abnormaland emergency operations. Some of the procedures discussed in this chapter are the result of doubleor triple failures. Whilst it is very unlikely that any of these failures will be encountered, it is useful tohave a background understanding of the effect that they have on the handling and management of theaircraft. In all cases, the ECAM should be handled as described in FCTM (Refer to OP-040 PURPOSEOF THE ECAM).

LANDING DISTANCE PROCEDUREIdent.: AO-010-00005608.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Should a failure occur with "LANDING DISTANCE PROC....APPLY" message displayed on theECAM STATUS page, the crew will enter the LDG CONF/APP SPD/LDG DIST/ CORRECTIONSFOLLOWING FAILURES table in QRH abnormal procedures and read:• The flap lever position for landing• Delta VREF if required for VAPP determination• The landing distance factor for landing distance calculation

VAPP DETERMINATIONIdent.: AO-010-00005609.0001001 / 08 JAN 09Criteria: SA�Applicable to: ALL

BACKGROUND

Some failures affect the approach speed.• Some failures (typically slat or flap failure) increase the VLS. In this case, the VLS displayed on

the PFD (if available) takes into account the actual configuration.• In some others failures, it is required to fly at speed higher than VLS to improve the handling

characteristics of the aircraft. This speed increment is to be added to the VLS displayed on thePFD when the landing configuration is reached.

In order to prepare the approach and landing, the crew needs to calculate the VAPP in advance.The appropriate VLS is not necessarily available at that time on the PFD, because the landingconfiguration is not yet established. Hence, VAPP is determined using VREF, which is the VLS of




CONF FULL, and is available both in the MCDU PERF APPR page and the QRH part 2. ΔVREF,extracted from the QRH part 2, is then added.VAPP = VREF + ΔVREF + APPRoach CORrection

The APPRoach CORrection (APPR COR) takes into account:‐ The use of A/THR‐ Ice accretion if applicable and‐ Wind correction when required.




METHOD

If QRH shows a ΔVREFVAPP computation principle with ΔVREF

(1) For ΔVREF ≤ 10 kt: apply speed increment to the VAPP and/or additional factor to thelanding distance if applicable (See (2) and See (3) )

(2) Multiply the landing distance by an additional factor of 1.1

(3) In CONF 3, add another 5 kt speed increment and multiply the landing distance by anadditional factor of 1.2 (instead of 1.1)




Then, if landing in CONF 3 is required, select CONF 3 on the MCDU (this ensures properoperation of the GPWS).When fully configured in final approach, the crew will check the reasonableness of the finalapproach speed computed by the crew with regard to VLS on the PFD speed scale.If the QRH shows no ΔVREF:The flight crew can use the MCDU VAPP, as computed by the FMS (the FMS takessystematically into account the use of A/THR).

IN FLIGHT LANDING DISTANCE CALCULATION FOLLOWING FAILURESIdent.: AO-010-00005610.0001001 / 01 JUL 08Criteria: SA�Applicable to: ALL

GENERAL

The actual landing distance (from 50 ft above the runway surface until the aircraft comes to thecomplete stop) is measured during specific flight tests for the certification of the aircraft. Thisdistance represents the absolute performance capability of the aircraft. It is published without safetymargin under the name "LANDING DISTANCE WITHOUT AUTOBRAKE" in the QRH.To compute the actual landing distance following any failure affecting the landing performance, thecrew multiplies the "LANDING DISTANCE WITHOUT AUTOBRAKE" CONFIGURATION FULL bythe associated landing distance factor found in the QRH. This actual landing distance following afailure is computed with no safety margin.The flight crew checks this actual landing distance against the Landing Distance Available (LDA) ofthe runway used for landing applying the relevant safety margins.

The safety margins to be applied depend of the circumstances according to:• the Captain judgement• the Airline policy• the applicable regulations

Note: For example:

The US-FAA recommends to apply a minimum safety margin of 15 % between the actuallanding distance and the Landing Distance Available (LDA) in case of• in-flight determination of the landing distance• normal and abnormal conditions (except in an emergency)

Ref: US-FAA SAFO 06012 dated 31 Aug 2006.

DRY RUNWAY

The landing distance calculation does NOT include the effect of thrust reversers.




Landing distance with failure = Landing distance See (1) x Failure factor "dry" See (2) xAdditional factor (if applicable)See (3)(1): LANDING DISTANCE WITHOUT AUTOBRAKE – CONFIGURATION FULL (QRH part 4 – INFLIGHT PERFORMANCE Refer to FCOM/99 Duref cible)(2): Failure factor "dry" from the “LDG CONF/APPR SPD/ LDG DIST FOLLOWING FAILURES” table(QRH part 2 - ABNORMAL PROCEDURES). Refer to FCOM/99 Duref cible(3):Due to the use of A/THR or in case of ice accretion, if the ΔVREF ≤ 10 kt (Refer to AO-010 VappDETERMINATION).Reverse thrust credit:For the failure cases for which ALL thrust reversers remain available it is possible to include theeffect of reverse thrust in the calculation.Landing distance with failure = Landing distance See (1) x Reverse thrust credit See (4) xFailure factor "dry" See (2) x Additional factor (if applicable)See (3)(4): LANDING DISTANCE WITHOUT AUTOBRAKE – CONFIGURATION FULL - CORRECTIONStable all Reversers operative (QRH part 4 – IN FLIGHT PERFORMANCE Refer to FCOM/99 Durefcible)

WET OR CONTAMINATED RUNWAY

The landing distance calculation includes the effect of all available thrust reversers.Whatever is the failure, the actual landing distance found in the table "LANDING DISTANCEWITHOUT AUTOBRAKE" CONFIGURATION FULL must be corrected by the reversers credit.When applicable, the failure factors take into account the loss of one or more thrust reversers due tothe related failure.

Note: This method does not permit to compute the landing distance with NO REVERSE thrustcredit

Landing distance with failure = Landing distance See (1) x Reverse thrust credit See (4) xFailure factor "wet or contaminated" See (2) x Additional factor (if applicable)See (3)


ABNORMAL OPERATIONSOPERATING TECHNIQUES


LOW SPEED ENGINE FAILUREIdent.: AO-020-00005612.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

If an engine failure occurs at low speed, the resultant yaw may be significant, leading to rapiddisplacement from the runway centreline. For this reason, it is essential that the Captain keepshis hand on the thrust levers once take-off thrust has been set. Directional control is achieved byimmediately closing the thrust levers and using maximum rudder and braking. If necessary, thenosewheel tiller should be used to avoid runway departure.

REJECTED TAKEOFFIdent.: AO-020-00005614.0001001 / 03 JUL 08Criteria: SA�Applicable to: ALL

FACTORS AFFECTING RTO

Experience has shown that a rejected takeoff can be hazardous, even if correct procedures arefollowed. Some factors that can detract from a successful rejected takeoff are as follows:• Tire damage• Brakes worn or not working correctly• Error in gross weight determination• Incorrect performance calculations• Incorrect runway line-up technique• Initial brake temperature• Delay in initiating the stopping procedure• Runway friction coefficient lower than expected

Thorough pre-flight preparation and a conscientious exterior inspection can eliminate the effect ofsome of these factors.During the taxi-out, a review of the takeoff briefing is required. During this briefing, the crew shouldconfirm that the computed takeoff data reflects the actual takeoff conditions e.g. wind and runwaycondition. Any changes to the planned conditions require the crew to re-calculate the takeoff data.In this case, the crew should not be pressurised into accepting a takeoff clearance before being fullyready. Similarly, the crew should not accept an intersection takeoff until the takeoff performance hasbeen checked.The line-up technique is very important. The pilot should use the over steer technique to minimizefield length loss and consequently, to maximize the acceleration-stop distance available.




DECISION MAKING

A rejected takeoff is a potentially hazardous manoeuvre and the time for decision-making is limited.To minimize the risk of inappropriate decisions to reject a takeoff, many warnings and cautions areinhibited between 80 kt and 1 500 ft. Therefore, any warnings received during this period must beconsidered as significant.

To assist in the decision making process, the takeoff is divided into low and high speeds regimes,with 100 kt being chosen as the dividing line. The speed of 100 kt is not critical but was chosen inorder to help the Captain make the decision and to avoid unnecessary stops from high speed:• Below 100 kt, the Captain will seriously consider discontinuing the takeoff if any ECAM warning/

caution is activated.• Above 100 kt, and approaching V1, the Captain should be "go-minded" and only reject the takeoff

in the event of a major failure, sudden loss of thrust, any indication that the aircraft will not flysafely, any red ECAM warning, or any amber ECAM caution listed below:• F/CTL SIDESTICK FAULT• ENG FAIL• ENG REVERSER FAULT• ENG REVERSE UNLOCKIf a tire fails within 20 kt of V1, unless debris from the tire has caused noticeable engineparameter fluctuations, it is better to get airborne, reduce the fuel load and land with a full runwaylength available.

The decision to reject the takeoff is the responsibility of the Captain and must be made prior to V1speed:• If a malfunction occurs before V1, for which the Captain does not intend to reject the takeoff, he

will announce his intention by calling "GO".• If a decision is made to reject the takeoff, the Captain calls "STOP". This call both confirms the

decision to reject the takeoff and also states that the Captain now has control. It is the only timethat hand-over of control is not accompanied by the phrase "I have control".

RTO PROCEDURE

Should a RTO procedure is initiated, the following task sharing will be applied.




(1): Announcing the deceleration means that the deceleration is felt by the crew, and confirmedby the Vc trend on the PFD. The deceleration may also be confirmed by the DECEL light (if theautobrake is on). However, this light only comes on when the actual deceleration is 80 % of theselected rate, it is not an indicator of the proper autobrake operation. For instance, the DECEL lightmight not appear on a contaminated runway, with the autobrake working properly, due to the effectof the antiskid.If the takeoff is rejected prior to 72 kt, the spoilers will not deploy and the auto-brake will not function.If a rejected takeoff is initiated and MAX auto brake decelerates the aircraft, the captain will avoidpressing the pedals (which might be a reflex action). Conversely, if deceleration is not felt, thecaptain will press the brake pedals fully down.If takeoff has been rejected due to an engine fire, the ECAM actions will be completed until shuttingdown the remaining engines.




Rejected takeoff flow pattern

INTRODUCTION TO EMERGENCY EVACUATIONIdent.: AO-020-00005615.0001001 / 22 MAY 08Criteria: SA�

1 Applicable to: MSN 0002-3000, 3002-3029, 3031-3061, 3063-3099, 3101-3212, 3215, 3217-3237, 3239-3242, 3244-3294, 3296-3308,3310-3327, 3329-3330, 3332, 3334-3342, 3344-3361, 3364-3370, 3372-3384, 3386-3387, 3389, 3391-3411, 3413-3437, 3439-3463, 3465-3468,3470-3481, 3483-3501, 3503-3508, 3510-3514, 3516-3529, 3531, 3533-3562, 3565-3584, 3586-3597, 3599-3601, 3603-3605, 3607-3608,3610-3616, 3618-3634, 3636-3641, 3644-3665, 3667-3694, 3696-3731, 3733-3750, 3752-3814, 3816-3830, 3832-3845, 3847-3884, 3887-3896,3898-3905, 3907-3920, 3922-3931, 3933-3955, 3959-3996

GENERAL

The typical case, which may require an emergency evacuation, is an uncontrollable on groundengine fire. This situation, which may occur following a rejected takeoff or after landing, requiresgood crew coordination to cope with a high workload situation:‐ In the rejected takeoff case, the Captain calls "STOP". This confirms that the Captain has controls‐ In all other cases, the Captain calls "I HAVE CONTROLS" if required, to state the control hand

over.




DECISION MAKING

As soon as aircraft is stopped, and the parking brake is set, the captain notifies the cabin crew andcalls for ECAM ACTIONS. At this stage, the task sharing is defined as follow:‐ The first officer carries out the ECAM actions until shutting down the remaining engine‐ The captain builds up his decision to evacuate depending on the circumstances. Considerations

should be given to:• Fire remaining out of control after having discharged the agents• Possible passenger evacuation of the aircraft on the runway• Positioning the aircraft to keep the fire away from the fuselage, taking into account the wind

direction• Communicating intentions or requests to ATC.

If fire remains out of control after having discharged the fire agents, the captain calls for theEMERGENCY EVACUATION procedure located in the inside back cover of the QRH.

Ident.: AO-020-00005615.0002001 / 22 MAY 08Criteria: P9907, SA�

2 Applicable to: MSN 3001, 3030, 3062, 3100, 3213-3214, 3216, 3238, 3243, 3295, 3309, 3328, 3331, 3333, 3343, 3362-3363, 3371, 3385,3388, 3390, 3412, 3438, 3464, 3469, 3482, 3502, 3509, 3515, 3530, 3532, 3563-3564, 3585, 3598, 3602, 3606, 3609, 3617, 3635, 3642-3643,3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886, 3897, 3906, 3921, 3932, 3956

GENERAL

The typical case, which may require an emergency evacuation, is an uncontrollable on groundengine fire. This situation, which may occur following a rejected takeoff or after landing, requiresgood crew coordination to cope with a high workload situation:‐ In the rejected takeoff case, the Captain calls "STOP". This confirms that the Captain has controls‐ In all other cases, the Captain calls "I HAVE CONTROLS" if required, to state the control hand

over.

DECISION MAKING

As soon as aircraft is stopped, and the parking brake is set, the captain notifies the cabin crew andcalls for ECAM ACTIONS. At this stage, the task sharing is defined as follow:‐ The first officer carries out the ECAM actions‐ The captain builds up his decision to evacuate depending on the circumstances. Considerations

should be given to:• Fire remaining out of control after having discharged the agents• Possible passenger evacuation of the aircraft on the runway• Positioning the aircraft to keep the fire away from the fuselage, taking into account the wind

direction• Communicating intentions or requests to ATC.




If fire remains out of control after having discharged the fire agents, the captain calls for theEMERGENCY EVACUATION procedure located in the inside back cover of the QRH.

THE EMERGENCY EVACUATION PROCEDUREIdent.: AO-020-00005626.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

Some items need to be highlighted:‐ It is essential that the differential pressure be zeroed.

In automatic pressurization mode, the crew can rely on the CPC, and the Delta P check is thereforenot applicable.If MAN CAB PRESS is used in flight, the CAB PR SYS (1+2) FAULT procedure requires selectingMAN V/S CTL to FULL UP position during final approach to cancel any residual cabin pressure.However, since the residual pressure sensor indicator, installed in the cabin door, is inhibitedwith slides armed, an additional Delta P check is required by the EMERGENCY EVACUATIONprocedure.Since MAN CAB PRESS is never used for takeoff as at least one automatic cabin pressure controlmust be operative for departure, the Delta P check does not apply to the case of emergencyevacuation following a rejected takeoff.

‐ CABIN CREW (PA)…ALERT reminds the captain for the "CABIN CREW AT STATION" call out. (Incase of RTO, this is done during the RTO flow pattern). Cabin crew must be aware that the flightcrew is still in control of the situation. In certain circumstances, this will avoid any unwanted orunnecessary evacuation initiated by the cabin crew

‐ EVACUATION…INITIATE requires the captain confirmation that the emergency evacuation is stillrequired. If still required, the captain:• Notifies the cabin crew to start the evacuation• Activates the EVAC command• Advises ATC if required.This will be done preferably in this order for a clear understanding by cabin crew.

On ground with engines stopped, only the right dome light is operational and the three positions(BRT, DIM, OFF) of the DOME light sw remain available, allowing the EMERGENCY EVACUATIONprocedure completion.The crew will keep in mind that as long as the evacuation order is not triggered, the crew may differor cancel the passengers' evacuation. As soon as the evacuation order is triggered, this decision isirreversible.When aircraft is on batteries power, the crew seats can only be operated mechanically.




TASKSHARING IN CASE OF EMERGENCY EVACUATIONIdent.: AO-020-00005628.0001001 / 24 APR 08Criteria: SA�Applicable to: ALL

When applying the EMERGENCY EVACUATION procedure, the F/O can select the engine mastersOFF and push the FIRE pb, without any confirmation from the Captain.




ENGINE FAILURE AFTER V1Ident.: AO-020-00005617.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

AIRCRAFT HANDLING

If an engine fails after V1 the takeoff must be continued. The essential and primary tasks are linkedto aircraft handling. The aircraft must be stabilized at the correct pitch and airspeed, and establishedon the correct track prior to the initiation of the ECAM procedure.

ON THE GROUND:

Rudder is used conventionally to maintain the aircraft on the runway centreline.At VR, rotate the aircraft smoothly, at a slower rate than with all engines operation, usinga continuous pitch rate to an initial pitch attitude of 12.5 °. The combination of high FLEXtemperature and low V speeds requires precise handling during the rotation and lift off. The 12.5 °pitch target will ensure the aircraft becomes airborne.

WHEN SAFELY AIRBORNE:

The SRS orders should then be followed which may demand a lower pitch attitude to acquire ormaintain V2.With a positive rate of climb and when the Radio Altitude has increased, the PNF will call "positiveclimb". This will suggest to the PF for landing gear retraction.Shortly after lift off, the lateral normal law commands some rudder surface deflection to minimizethe sideslip (there is no feedback of this command to the pedals). Thus, the lateral behavior of theaircraft is safe and the pilot should not be in a hurry to react on the rudder pedals and to chasethe beta target.The blue beta target will replace the normal sideslip indication on the PFD. Since the lateralnormal law does not command the full needed rudder surface deflection, the pilot will have toadjust conventionally the rudder pedals to center the beta target.When the beta target is centred, total drag is minimized even though there is a small amountof sideslip. The calculation of the beta target is a compromise between drag produced bydeflection of control surfaces and airframe drag produced by a slight sideslip. Centering the betatarget produces less total drag than centering a conventional ball, as rudder deflection, ailerondeflection, spoiler deployment and aircraft body angle are all taken into account.The crew will keep in mind that the yaw damper reacts to a detected side slip. This means that,with hands off the stick and no rudder input, the aircraft will bank at about 5 ° maximum and then,will remain stabilized. Thus, laterally, the aircraft is a stable platform and no rush is required tolaterally trim the aircraft. Control heading conventionally with bank, keeping the beta target atzero with rudder. Accelerate if the beta target cannot be zeroed with full rudder. Trim the rudderconventionally.




The use of the autopilot is STRONGLY recommended. Following an engine failure, the ruddershould be trimmed out prior to autopilot engagement.Once AP is engaged, the rudder trim is managed through the AP and, hence, manual rudder trimcommand, including reset, is inhibited.

THRUST CONSIDERATIONS

Consider the use of TOGA thrust, keeping in mind the following:• For a FLEX takeoff, selecting the operating engine to TOGA provides additional performance

margin but is not a requirement of the reduced thrust takeoff certification. The application ofTOGA will very quickly supply a large thrust increase but this comes with a significant increase inyawing moment and an increased pitch rate. The selection of TOGA restores thrust margins but itmay be at the expense of increased workload in aircraft handling.

• TOGA thrust is limited to 10 min.

PROCEDURE

INITIATION OF THE PROCEDURE

The PNF will closely monitor the aircraft's flight path. He will cancel any Master Warning/Cautionand read the ECAM title displayed on the top line of the E/WD.

Procedures are initiated on PF command. No action is taken (apart from cancelling audiowarnings through the MASTER WARNING light) until:• The appropriate flight path is established and,• The aircraft is at least 400 ft above the runway, if a failure occurs during takeoff, approach or

go-around.A height of 400 ft is recommended because it is a good compromise between the necessarytime for stabilization and the excessive delay in procedure initiation. In some emergency casesand provided the flight path is established, the PF may initiate the ECAM actions before 400 ft.

Once the PF has stabilised the flight path, the PNF confirms the failure. If it is necessary to delaythe ECAM procedure, the PF should order "Standby", otherwise he should announce "ECAMactions".Priority must be given to the control of aircraft trajectory, and acceleration phase should not bedelayed for the purpose of applying the ENG FAIL ECAM procedure. Should the PF require anaction from the PNF during ECAM procedures, the order "STOP ECAM" should be used. Whenready to resume ECAM procedure, the order "CONTINUE ECAM" should be used.The procedure may be continued until "ENG MASTER OFF" (in case of engine failure withoutdamage) or until AGENT 1 DISCH (in case of engine failure with damage) before acceleration.

Note: In case of ENG FIRE, fire drill remains high priority.




ACCELERATION SEGMENT

At the engine-out acceleration altitude, push ALT to level off and allow the speed to increase. Ifthe aircraft is being flown manually, the PF should remember that, as airspeed increases, therudder input needed to keep the beta target centred will reduce. Retract the flaps as normal.When the flap lever is at zero, the beta target reverts to the normal sideslip indication.

FINAL TAKEOFF SEGMENT

As the speed trend arrow reaches Green Dot speed, pull for OPEN CLIMB, set THR MCT whenthe LVR MCT message flashes on the FMA (triggered as the speed index reaches green dot) andresume climb using MCT. If the thrust lever are already in the FLX/MCT detent, move lever to CLand then back to MCT.When an engine failure occurs after takeoff, noise abatement procedures are no longer arequirement. Additionally, the acceleration altitude provides a compromise between obstacleclearance and engine thrust limiting time. It allows the aircraft to be configured to Flap 0 andgreen dot speed, which provides the best climb gradient.Once established on the final takeoff flight path, continue the ECAM until the STATUS isdisplayed. At this point, the AFTER T/O checklist should be completed, computer resetconsidered and OEBs consulted (if applicable). STATUS should then be reviewed.

ONE ENGINE OUT FLIGHT PATH

The one engine out flight path will be flown according to the takeoff briefing made at the gate:• The EOSID (with attention to the decision point location)• The SID• Radar vectors...




Engine failure after V1

ENGINE FAILURE DURING INITIAL CLIMB-OUTIdent.: AO-020-00005619.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Proceed as above. If the failure occurs above V2 however, maintain the SRS commanded attitude. Inany event the minimum speed must be V2.When an engine failure is detected, the FMGS produces predictions based on the engine-outconfiguration and any pre-selected speeds entered in the MCDU are deleted.

ENGINE FAILURE DURING CRUISEIdent.: AO-020-00005620.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

GENERAL

There are three strategies available for dealing with an engine failure in the cruise:• The standard strategy




• The obstacle strategy• The fixed speed strategy

The fixed speed strategy refers to ETOPS. It is discussed in FCOM 2 "special operations" and isdiscussed in a separate course.Unless a specific procedure has been established before dispatch (considering ETOPS ormountainous areas), the standard strategy is used.

Note: Pressing the EO CLR key on the MCDU restores the all engine operative predictions andperformance. Reverting to one engine-out performance again is not possible.

PROCEDURE

As soon as the engine failure is recognized, the PF will simultaneously:• Set MCT on the remaining engine(s)• Disconnect A/THR

Then, PF will• Select the SPEED according to the strategy• If appropriate, select a HDG to keep clear of the airway, preferably heading towards an alternate.

Consideration should be given to aircraft position relative to any relevant critical point• Select the appropriate engine inoperative altitude in the FCU ALT window and pull for OPEN DES

Then, PF will• Require the ECAM actions

At high flight levels close to limiting weights, crew actions should not be delayed, as speed will decayquickly requiring prompt crew response. The crew will avoid decelerating below green dot.




The A/THR is disconnected to avoid any engine thrust reduction when selecting speed according tostrategy or when pulling for OPEN DES to initiate the descent. With the A/THR disconnected, thetarget speed is controlled by the elevator when in OPEN DES.Carrying out the ECAM actions should not be hurried, as it is important to complete the drillcorrectly. Generally, there will be sufficient time to cross check all actions.

STANDARD STRATEGY

Set speed target M 0.78/300 kt. The speed of 0.78/300 kt is chosen to ensure the aircraft is withinthe stabilised windmill engine relight in-flight envelope.The REC MAX EO Cruise altitude, which equates to LRC with anti-icing off, is displayed on theMCDU PROG page and should be set on the FCU. (One engine out gross ceiling at long-rangespeed is also available in the QRH in case of double FM failure).If V/S becomes less than 500 ft/min, select V/S - 500 ft/min and A/THR on. This is likely to occur aslevel off altitude is approached.Once established at level off altitude, long-range cruise performance with one engine out may beextracted from QRH or Refer to FCOM/PER-CRZ-OEI-GEN-10 PROCEDURE.




OBSTACLE STRATEGY

To maintain the highest possible level due to terrain, the drift down procedure must be adopted. Thespeed target in this case is green dot. The procedure is similar to the standard strategy, but as thespeed target is now green dot, the rate and angle of descent will be lower.The MCDU PERF CRZ page in EO condition will display the drift down ceiling, assuming green dotspeed and should be set on FCU. (One engine out gross ceiling at green dot speed is also availablein the QRH and FCOM).If, having reached the drift down ceiling altitude, obstacle problems remain, the drift down proceduremust be maintained so as to fly an ascending cruise profile.When clear of obstacles, set LRC ceiling on FCU, return to LRC speed and engage A/THR.

ENGINE-OUT LANDINGIdent.: AO-020-00005622.0001001 / 22 APR 08Criteria: SA�Applicable to: ALL

Autoland is available with one engine inoperative, and maximum use of the AP should be made tominimise crew workload. If required, a manual approach and landing with one engine inoperative isconventional. The pilot should trim to keep the slip indication centred. It remains yellow as long as thethrust on the remaining engine(s) is below a certain value.With flap selected and above this threshold value, the indicator becomes the blue beta target. This is avisual cue that the aircraft is approaching its maximum thrust capability.Do not select the gear down too early, as large amounts of power will be required to maintain levelflight at high weights and/or high altitude airports.To make the landing run easier, the rudder trim can be reset to zero in the later stages of theapproach. On pressing the rudder trim reset button, the trim is removed and the pilot should anticipatethe increased rudder force required. With rudder trim at zero, the neutral rudder pedal positioncorresponds to zero rudder and zero nose wheel deflection.

CIRCLING ONE ENGINE INOPERATIVEIdent.: AO-020-00005623.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

In normal conditions, circling with one engine inoperative requires the down wind leg to be flown inCONF 3, with landing gear extended.In hot and high conditions and at high landing weight, the aircraft may not be able to maintain levelflight in CONF 3 with landing gear down. The flight crew should check the maximum weight showed inthe QRH CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE procedure table. If the landingweight is above this maximum value, the landing gear extension should be delayed until established onfinal approach.




If the approach is flown at less than 750 ft RA, the warning "L/G NOT DOWN" will be triggered. "TOOLOW GEAR" warning is to be expected, if the landing gear is not downlocked at 500 ft RA. Therefore, ifweather conditions permit, it is recommended to fly a higher circling pattern.

ONE ENGINE INOPERATIVE GO-AROUNDIdent.: AO-020-00005624.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

A one engine inoperative go-around is similar to that flown with all engines. On the application ofTOGA, rudder must be applied promptly to compensate for the increase in thrust and consequently tokeep the beta target centred. Provided the flap lever is selected to Flap 1 or greater, SRS will engageand will be followed. If SRS is not available, the initial target pitch attitude is 12.5 °. The lateral FDmode will be GA TRK and this must be considered with respect to terrain clearance. ALT should beselected at the engine inoperative acceleration altitude, with the flap retraction and further climb carriedout using the same technique as described earlier in "ENGINE FAILURE AFTER V1" section.




THRUST LEVERS MANAGEMENT IN CASE OF INOPERATIVE REVERSER(S)Ident.: AO-020-00006319.0002001 / 08 JAN 09Criteria: CFMI, SA�

3 Applicable to: MSN 0002-0034, 0039-0042, 0044, 0059-0063, 0068-0073, 0078, 0083-0088, 0093-0094, 0100-0112, 0115-0162, 0167,0170-0177, 0181-0192, 0195-0197, 0199-0224, 0226-0229, 0231-0242, 0244-0246, 0248, 0253-0255, 0258, 0262-0274, 0277-0279, 0281-0290,0293-0294, 0297-0303, 0305-0307, 0309-0313, 0318-0319, 0323-0325, 0328-0331, 0333, 0337, 0339-0343, 0345-0346, 0348-0350, 0352,0355-0356, 0358-0360, 0365, 0367, 0370-0372, 0375, 0377-0384, 0387-0392, 0395, 0399-0404, 0407-0410, 0413, 0417-0422, 0426-0427,0434, 0436, 0438, 0445-0446, 0459, 0466, 0477, 0482, 0488, 0491, 0494-0495, 0497-0498, 0501, 0507, 0509, 0511, 0513-0517, 0519-0522,0524-0526, 0528-0529, 0531-0537, 0541, 0544-0549, 0552-0554, 0559, 0562, 0566, 0569-0570, 0572, 0574, 0576-0579, 0581, 0583,0585-0586, 0588, 0590, 0593-0594, 0596, 0598-0603, 0605, 0607-0612, 0615-0619, 0621-0630, 0634-0637, 0639, 0641-0651, 0653-0654,0656-0658, 0660, 0662, 0664-0666, 0669-0675, 0677, 0679, 0681-0682, 0684-0685, 0688-0689, 0691, 0693-0695, 0697, 0700-0701, 0703,0706-0707, 0711, 0713-0714, 0716-0717, 0719, 0721, 0723-0724, 0726-0730, 0732, 0734-0738, 0740, 0742, 0744-0745, 0749-0750, 0752-0755,0757, 0761, 0763-0769, 0772-0779, 0781-0782, 0785-0786, 0790, 0793-0797, 0799-0801, 0807-0809, 0813-0815, 0817-0819, 0821, 0823,0827-0833, 0837-0838, 0840-0841, 0844-0846, 0848, 0852-0854, 0860-0861, 0863, 0868-0870, 0875-0876, 0879-0880, 0883-0885, 0888,0890-0891, 0894, 0896-0897, 0903-0907, 0909, 0911, 0914, 0917, 0920-0923, 0925-0926, 0929, 0933, 0935-0942, 0945-0947, 0949, 0951,0956-0962, 0964, 0967, 0970-0973, 0975, 0978-0979, 0981-0982, 0984-0988, 0991-0992, 0994-1000, 1002, 1005-1006, 1009, 1011-1012,1016-1021, 1023, 1025-1030, 1033-1034, 1036-1038, 1040-1041, 1044, 1046-1048, 1051-1052, 1054-1055, 1058-1059, 1061-1063, 1065,1067-1073, 1077-1078, 1081, 1084, 1086-1087, 1089-1091, 1093-1095, 1097, 1099-1102, 1106-1109, 1112, 1114, 1119-1122, 1124-1127,1129-1138, 1141, 1144-1145, 1147-1152, 1154-1155, 1157, 1160, 1162, 1164-1165, 1167-1172, 1175-1176, 1179-1182, 1184-1187, 1189-1191,1198, 1200-1201, 1203, 1205-1206, 1208-1210, 1213, 1216-1217, 1219-1221, 1224, 1226, 1229-1231, 1233, 1237-1238, 1241-1242, 1244-1245,1247, 1249-1250, 1252, 1254-1255, 1259, 1262-1265, 1267-1269, 1271, 1275, 1277, 1283, 1285-1289, 1292, 1294, 1296-1299, 1301, 1303,1305-1320, 1322, 1324-1326, 1328, 1330-1331, 1336-1337, 1340, 1342, 1344-1348, 1352, 1354, 1357-1358, 1360-1362, 1364-1365, 1367,1369-1372, 1377-1379, 1381-1382, 1385-1394, 1396, 1399, 1402-1405, 1412-1417, 1425, 1429-1431, 1434, 1436-1437, 1439, 1441-1444,1447-1451, 1453-1458, 1461-1462, 1465, 1467, 1470-1473, 1476, 1478-1481, 1483-1485, 1488-1489, 1492-1494, 1496, 1498-1499, 1501-1505,1515-1517, 1519-1521, 1524-1525, 1530-1532, 1535-1536, 1539-1544, 1549-1551, 1553-1554, 1556, 1560, 1562, 1564, 1567, 1570-1572,1577-1579, 1582-1583, 1588, 1592, 1597-1599, 1601-1603, 1605, 1607, 1611-1612, 1615-1616, 1618, 1622-1623, 1625, 1629-1630, 1632-1634,1637-1641, 1645-1646, 1651, 1654-1655, 1657-1660, 1662, 1666-1668, 1673-1674, 1677-1679, 1681, 1683-1686, 1691-1694, 1699-1701,1704, 1706, 1709, 1712-1714, 1716-1720, 1722, 1724-1726, 1733, 1735-1736, 1738, 1740, 1742-1748, 1750-1753, 1756-1757, 1759, 1761-1762,1765-1767, 1769-1770, 1772, 1774-1775, 1777-1781, 1783, 1786-1787, 1789, 1791, 1793, 1795-1797, 1799-1800, 1803, 1805-1806, 1808-1812,1815-1816, 1819-1820, 1824, 1828, 1833, 1836, 1838-1839, 1841, 1846, 1851-1853, 1859-1860, 1863-1864, 1866-1867, 1870, 1872-1876, 1879,1881-1882, 1884-1887, 1889-1890, 1894, 1897, 1900-1901, 1905-1906, 1908, 1911, 1913, 1916, 1920-1921, 1923-1925, 1929-1932, 1936-1940,1942-1943, 1949, 1951, 1954, 1959-1961, 1963-1966, 1968, 1972-1973, 1975-1976, 1978, 1980-1983, 1988-1991, 1994, 1997, 1999, 2001-2003,2005, 2009-2013, 2017-2019, 2022, 2024-2026, 2028, 2030, 2033-2037, 2039, 2043, 2046-2054, 2056-2057, 2059-2062, 2064-2066,2068-2069, 2071-2072, 2074, 2076, 2078, 2081-2083, 2086-2087, 2091-2093, 2095, 2100-2101, 2103-2104, 2106, 2109, 2113-2117, 2119-2120,2122-2124, 2126-2127, 2129, 2131, 2133-2134, 2140, 2142-2146, 2151, 2154-2155, 2158, 2162-2163, 2165-2166, 2170-2171, 2174-2176,2178-2184, 2186-2187, 2189, 2191, 2196, 2198-2199, 2206-2209, 2212-2214, 2217-2222, 2224-2225, 2227-2228, 2230, 2233, 2235-2237,2239-2245, 2248-2251, 2253, 2256, 2258, 2260, 2262, 2264-2266, 2269-2272, 2274, 2276, 2278-2279, 2283, 2285, 2287, 2289, 2291,2293-2294, 2298, 2300, 2306, 2309, 2311, 2315, 2317-2319, 2325, 2327-2328, 2330, 2332-2333, 2337, 2342, 2344, 2346-2347, 2349-2350,2353-2354, 2357-2358, 2360-2361, 2364-2365, 2367, 2369-2370, 2373-2374, 2377-2378, 2380-2382, 2385, 2387-2388, 2390-2392, 2394,2398-2400, 2402, 2406-2407, 2409, 2411-2412, 2416, 2419-2420, 2425, 2427, 2432, 2436-2437, 2439-2440, 2442, 2446, 2448, 2450-2451,2456, 2460, 2463-2465, 2471-2472, 2474, 2477-2478, 2481, 2483-2484, 2486-2488, 2492-2495, 2497-2499, 2503, 2506-2508, 2511-2512,2514, 2516, 2518-2519, 2523, 2525, 2527-2529, 2532, 2538-2552, 2554-2558, 2561-2563, 2565, 2569, 2575, 2578, 2581-2584, 2586,2588, 2591-2593, 2596, 2599, 2601, 2605-2607, 2611-2612, 2616-2620, 2623-2625, 2627-2629, 2632-2633, 2635-2638, 2641, 2644, 2646,2652, 2654, 2656, 2658, 2662, 2665, 2668, 2672, 2674-2675, 2677-2678, 2681, 2683-2686, 2691, 2693, 2695-2696, 2699-2700, 2702,2705-2709, 2712, 2715-2716, 2719, 2721, 2726-2727, 2729, 2733, 2735-2736, 2740, 2742-2746, 2748-2751, 2754, 2756-2758, 2760-2765,2768-2770, 2773-2774, 2776-2779, 2782, 2785-2786, 2788-2790, 2792, 2794-2796, 2798, 2800-2801, 2803, 2805-2807, 2810-2812, 2816,2818-2822, 2824-2827, 2829-2831, 2834-2837, 2839, 2841-2843, 2846-2847, 2849, 2851-2855, 2857, 2860-2861, 2865-2867, 2869-2870,2873, 2875-2879, 2881-2882, 2884-2885, 2889-2891, 2895, 2897, 2899, 2902-2903, 2905, 2907, 2909-2910, 2912-2913, 2915, 2918,2920-2921, 2923-2926, 2930-2932, 2935, 2937-2939, 2944, 2946-2947, 2949-2951, 2954-2957, 2959-2962, 2964-2968, 2972-2973, 2975,2980, 2985-2986, 2988-2989, 2991, 2993-2996, 2998, 3000, 3002-3003, 3006, 3008-3009, 3014, 3016, 3018-3019, 3021, 3023-3025,3027-3028, 3031, 3035-3038, 3040-3041, 3043-3044, 3046-3048, 3051-3056, 3058-3061, 3063-3065, 3068, 3070, 3073, 3076, 3078-3080,3082-3085, 3087-3088, 3090, 3092-3102, 3107-3111, 3115, 3117-3118, 3121-3123, 3129-3140, 3145-3149, 3151-3155, 3157, 3160-3161,3163-3164, 3168-3171, 3173-3174, 3176, 3178-3182, 3184, 3186-3189, 3191, 3194, 3197, 3199, 3201-3206, 3209, 3211-3213, 3215, 3218,3220-3221, 3223-3226, 3230, 3232-3234, 3236-3238, 3240, 3242-3243, 3245-3247, 3249-3250, 3255-3256, 3260-3262, 3266-3268, 3271-3273,3277-3278, 3281-3282, 3284-3286, 3288-3289, 3291, 3293, 3295, 3298-3300, 3304-3307, 3309-3310, 3312-3313, 3318, 3320-3321,3323-3329, 3331, 3333-3334, 3336-3338, 3340, 3343-3347, 3349, 3353, 3356, 3359, 3361-3364, 3366-3368, 3370, 3372-3374, 3376-3377,3380, 3383, 3385, 3388-3389, 3391, 3394, 3396, 3398-3401, 3403-3404, 3406-3408, 3410-3413, 3415, 3417, 3419-3420, 3422, 3425-3427,3431-3433, 3435-3436, 3440-3448, 3452, 3455-3456, 3460-3461, 3464-3467, 3470-3473, 3475-3477, 3480, 3482, 3485-3487, 3489-3490,3492, 3494, 3498, 3501-3506, 3508, 3511, 3513-3516, 3518, 3521, 3523, 3528-3530, 3532-3533, 3536-3537, 3540, 3542, 3544-3545, 3549,3551, 3553, 3555, 3557, 3559-3560, 3563-3565, 3568-3569, 3571, 3573-3574, 3576, 3579, 3582, 3584, 3586, 3589, 3593-3594, 3596-3599,3601, 3604-3605, 3608-3612, 3615-3617, 3619-3620, 3623, 3626-3634, 3639-3640, 3643-3644, 3646-3648, 3651-3653, 3655-3658, 3660-3662,3664-3667, 3670, 3675, 3678-3679, 3682-3684, 3686-3687, 3689-3691, 3695-3696, 3704, 3706, 3708, 3711, 3715, 3720, 3722-3723, 3725,3727-3729, 3731-3733, 3735, 3739, 3742, 3744, 3746-3747, 3749-3752, 3754-3756, 3762-3763, 3765-3767, 3769, 3774, 3776-3778, 3780-3781,3786-3792, 3794-3795, 3798-3799, 3802, 3805-3806, 3808-3810, 3813-3815, 3817-3819, 3822-3828, 3838, 3843-3846, 3871-3872, 3874-3875,3891-3892, 3903, 3698-3702, 3758, 3830-3831, 3833-3835, 3840, 3848, 3852-3857, 3859, 3861, 3865-3866, 3868, 3879-3880, 3882-3889,3894-3896, 3898, 3900, 3905-3909, 3913-3915, 3918-3919, 3921-3923, 3925, 3928-3933, 3939-3940, 3945-3946, 3949-3950, 3952-3956,3967, 3970-3972, 3983-3984

PREFACE

This section provides recommendations on thrust levers management in case of inoperativereverser(s). These recommendations are applicable in case of in-flight failure (including enginefailure) and/or in case of MEL dispatch with reverser(s) deactivated.




AT LEAST ONE REVERSER OPERATIVE

If at least one reverser is operative, the general recommendation is to select the reverser thrust onboth engines during rejected takeoff (RTO) and at landing, as per normal procedures.

Note: The ENG 1(2) REVERSER FAULT ECAM caution may be triggered after the reverser thrustis selected. This is to remind the flight crew that one reverser is inoperative.

CAUTION In case of MEL dispatch with one reverser deactivated:If the ENG (affected side) REVERSE UNLOCKED ECAM caution is triggered duringflight, the PF must not select the thrust lever on the affected engine at landing.

NO REVERSERS OPERATIVE

If no reversers are operative, the general recommendation is to not select the reverser thrust duringRTO and at landing.However, the PF still sets both thrust levers to the IDLE detent, as per normal procedures.

BRIEFING

IMPORTANCE OF THE FLIGHT CREW BRIEFING

Among others, the aircraft status must be reviewed during the flight crew briefing. Anyparticularities (operational consequences, procedures, associated task sharing and callout) mustbe reviewed at that time. The flight crew must notably review:• The status of the thrust reversers and if reverser thrust can be used• Operational effect (aircraft handling during roll-out).




Ident.: AO-020-00006319.0001001 / 08 JAN 09Criteria: SA�

4 Applicable to: MSN 0035-0038, 0043, 0045-0058, 0064-0067, 0074-0077, 0080-0082, 0089-0091, 0095-0099, 0113-0114, 0163-0166,0168-0169, 0178-0180, 0193-0194, 0198, 0225, 0230, 0243, 0247, 0249-0252, 0256-0257, 0259-0261, 0275-0276, 0280, 0291-0292,0295-0296, 0304, 0308, 0314-0317, 0320-0322, 0326-0327, 0332, 0334-0336, 0338, 0344, 0347, 0351, 0353-0354, 0357, 0361-0364,0366, 0368-0369, 0373, 0376, 0385-0386, 0393-0394, 0396-0398, 0405-0406, 0411-0412, 0414-0416, 0423-0425, 0428-0432, 0435, 0437,0439-0444, 0447-0458, 0460-0465, 0467-0476, 0478-0480, 0483-0487, 0489-0490, 0492-0493, 0496, 0499-0500, 0502-0506, 0508, 0510,0512, 0518, 0523, 0527, 0530, 0538-0540, 0542-0543, 0550-0551, 0555-0558, 0560-0561, 0563-0565, 0567-0568, 0571, 0573, 0575, 0580,0582, 0584, 0587, 0589, 0591-0592, 0595, 0597, 0604, 0606, 0613-0614, 0620, 0631-0633, 0638, 0640, 0652, 0655, 0659, 0661, 0663,0667-0668, 0676, 0678, 0680, 0683, 0686-0687, 0690, 0692, 0696, 0698-0699, 0702, 0704-0705, 0709-0710, 0712, 0715, 0718, 0720,0722, 0725, 0731, 0733, 0739, 0741, 0743, 0746-0748, 0751, 0756, 0758-0760, 0762, 0770-0771, 0780, 0783-0784, 0787-0788, 0791-0792,0798, 0802-0806, 0810-0812, 0816, 0820, 0822, 0824-0826, 0834-0836, 0839, 0842-0843, 0847, 0849-0851, 0855-0859, 0862, 0864-0867,0871-0874, 0877-0878, 0881-0882, 0886-0887, 0889, 0892-0893, 0895, 0898-0902, 0908, 0910, 0912-0913, 0915-0916, 0918-0919, 0924,0927-0928, 0930-0932, 0934, 0943-0944, 0948, 0950, 0952-0955, 0963, 0965-0966, 0968-0969, 0974, 0976-0977, 0980, 0983, 0989-0990,0993, 1001, 1003-1004, 1007-1008, 1010, 1013-1015, 1022, 1024, 1031-1032, 1035, 1039, 1042-1043, 1045, 1049-1050, 1053, 1056-1057,1060, 1064, 1066, 1074-1076, 1079-1080, 1082-1083, 1085, 1088, 1092, 1096, 1098, 1103-1105, 1110-1111, 1113, 1115-1118, 1123, 1128,1139-1140, 1142-1143, 1146, 1153, 1156, 1158-1159, 1161, 1163, 1166, 1173-1174, 1177-1178, 1183, 1188, 1192-1197, 1199, 1202, 1204, 1207,1211-1212, 1214-1215, 1218, 1222-1223, 1225, 1227-1228, 1232, 1234-1236, 1239-1240, 1243, 1246, 1248, 1251, 1253, 1256-1258, 1260-1261,1266, 1270, 1272-1274, 1276, 1279-1282, 1284, 1290-1291, 1293, 1295, 1300, 1302, 1304, 1321, 1323, 1327, 1329, 1332-1335, 1338-1339,1341, 1343, 1349-1351, 1353, 1355-1356, 1359, 1363, 1366, 1368, 1373-1376, 1380, 1383-1384, 1395, 1397-1398, 1400-1401, 1406-1411,1418-1424, 1426-1428, 1432-1433, 1435, 1438, 1440, 1445-1446, 1452, 1459-1460, 1463-1464, 1466, 1468-1469, 1474-1475, 1477, 1482,1486-1487, 1490-1491, 1495, 1497, 1500, 1506-1514, 1518, 1522-1523, 1526-1529, 1533-1534, 1537-1538, 1545-1548, 1552, 1555, 1557-1559,1561, 1563, 1565-1566, 1568-1569, 1573-1576, 1580-1581, 1584-1587, 1589-1591, 1593-1596, 1600, 1604, 1606, 1608-1610, 1613-1614,1617, 1619-1621, 1624, 1626-1628, 1631, 1635-1636, 1642-1644, 1647-1650, 1652-1653, 1656, 1661, 1663-1665, 1669-1672, 1675-1676,1680, 1682, 1687-1690, 1695-1698, 1702-1703, 1705, 1707-1708, 1710-1711, 1715, 1721, 1723, 1727-1732, 1734, 1737, 1739, 1741, 1749,1754-1755, 1758, 1760, 1763-1764, 1768, 1771, 1773, 1776, 1782, 1784-1785, 1788, 1790, 1792, 1794, 1798, 1801-1802, 1804, 1807, 1814,1817-1818, 1821-1823, 1825-1827, 1829-1832, 1834-1835, 1837, 1840, 1842-1845, 1847-1850, 1854-1858, 1861-1862, 1865, 1868-1869, 1871,1877-1878, 1880, 1883, 1888, 1891-1893, 1895-1896, 1898-1899, 1902-1904, 1907, 1909-1910, 1912, 1914-1915, 1917-1918, 1922, 1926-1928,1933-1935, 1941, 1944-1948, 1950, 1952-1953, 1955-1958, 1962, 1967, 1969-1971, 1974, 1977, 1979, 1984-1987, 1993, 1995-1996, 1998,2000, 2004, 2006-2008, 2014-2016, 2020-2021, 2023, 2027, 2029, 2031-2032, 2038, 2040-2042, 2044-2045, 2055, 2058, 2063, 2067, 2070,2073, 2075, 2077, 2079-2080, 2084-2085, 2088-2090, 2094, 2096-2099, 2102, 2105, 2107-2108, 2110-2112, 2118, 2121, 2125, 2128, 2130,2132, 2135-2139, 2141, 2147-2150, 2152-2153, 2156-2157, 2159-2161, 2164, 2167-2169, 2172-2173, 2177, 2185, 2188, 2190, 2192-2195,2197, 2200-2205, 2210-2211, 2215-2216, 2223, 2226, 2229, 2231-2232, 2234, 2238, 2246-2247, 2252, 2254-2255, 2257, 2259, 2261, 2263,2267-2268, 2273, 2275, 2277, 2280-2282, 2284, 2286, 2288, 2290, 2292, 2295-2297, 2299, 2301-2305, 2307-2308, 2310, 2312-2314,2316, 2320-2324, 2326, 2329, 2331, 2334-2336, 2338-2341, 2343, 2345, 2348, 2351-2352, 2355-2356, 2359, 2362-2363, 2366, 2368,2371-2372, 2375-2376, 2379, 2383-2384, 2386, 2389, 2393, 2395-2397, 2401, 2403-2405, 2408, 2410, 2413-2415, 2417-2418, 2421-2424,2426, 2428-2431, 2433-2435, 2438, 2441, 2443-2445, 2447, 2449, 2452-2455, 2457-2459, 2461-2462, 2466-2470, 2473, 2475-2476,2479-2480, 2482, 2485, 2489-2491, 2496, 2501-2502, 2504-2505, 2509-2510, 2513, 2515, 2517, 2520-2522, 2524, 2526, 2530-2531,2533-2537, 2553, 2559-2560, 2564, 2566-2568, 2570-2574, 2576-2577, 2579-2580, 2585, 2587, 2589-2590, 2594-2595, 2597-2598, 2600,2602-2604, 2608-2610, 2613-2615, 2621-2622, 2626, 2630-2631, 2634, 2639-2640, 2642-2643, 2645, 2647-2651, 2653, 2655, 2657,2659-2661, 2663-2664, 2666-2667, 2669-2671, 2673, 2676, 2679-2680, 2682, 2687-2690, 2692, 2694, 2697-2698, 2701, 2703-2704,2710-2711, 2713-2714, 2717-2718, 2720, 2723-2725, 2728, 2730-2732, 2734, 2737-2739, 2741, 2747, 2752-2753, 2755, 2759, 2766-2767,2771-2772, 2775, 2780-2781, 2783-2784, 2787, 2791, 2793, 2797, 2799, 2802, 2804, 2808-2809, 2813-2815, 2817, 2823, 2828, 2832-2833,2838, 2840, 2844-2845, 2848, 2850, 2856, 2858-2859, 2862-2864, 2868, 2871-2872, 2874, 2880, 2883, 2886-2888, 2892-2894, 2896, 2898,2900-2901, 2904, 2906, 2908, 2911, 2914, 2916-2917, 2919, 2922, 2927-2929, 2933-2934, 2936, 2940-2943, 2945, 2948, 2952-2953, 2958,2963, 2969-2971, 2974, 2976-2979, 2981-2984, 2987, 2990, 2992, 2997, 2999, 3001, 3004-3005, 3007, 3010-3013, 3015, 3017, 3020, 3022,3026, 3029-3030, 3032-3034, 3039, 3042, 3045, 3049-3050, 3057, 3062, 3066-3067, 3069, 3071-3072, 3074-3075, 3077, 3081, 3086, 3089,3091, 3103-3106, 3112-3114, 3116, 3119-3120, 3124-3128, 3141-3144, 3150, 3156, 3158-3159, 3162, 3165-3167, 3172, 3175, 3177, 3183,3185, 3190, 3192-3193, 3195-3196, 3198, 3200, 3207-3208, 3210, 3214, 3216-3217, 3219, 3222, 3227-3229, 3231, 3235, 3239, 3241, 3244,3248, 3251-3254, 3257-3259, 3263-3265, 3269-3270, 3274-3276, 3279-3280, 3283, 3287, 3290, 3292, 3294, 3296-3297, 3301-3303, 3308,3311, 3314-3317, 3319, 3322, 3330, 3332, 3335, 3339, 3341-3342, 3348, 3350-3352, 3354-3355, 3357-3358, 3360, 3365, 3369, 3371, 3375,3378-3379, 3381-3382, 3384, 3386-3387, 3390, 3392-3393, 3395, 3397, 3402, 3405, 3409, 3414, 3416, 3418, 3421, 3423-3424, 3428-3430,3434, 3437-3439, 3449-3451, 3453-3454, 3457-3459, 3462-3463, 3468-3469, 3474, 3478-3479, 3481, 3483-3484, 3488, 3491, 3493,3495-3497, 3499-3500, 3507, 3509-3510, 3512, 3517, 3519-3520, 3522, 3524-3527, 3531, 3534-3535, 3538-3539, 3541, 3543, 3546-3548,3550, 3552, 3554, 3556, 3558, 3561-3562, 3566-3567, 3570, 3572, 3575, 3577-3578, 3580-3581, 3583, 3585, 3587-3588, 3590-3592,3595, 3600, 3602-3603, 3606-3607, 3613-3614, 3618, 3621-3622, 3624-3625, 3635-3638, 3641-3642, 3645, 3649-3650, 3654, 3659, 3663,3668-3669, 3671-3674, 3676-3677, 3680-3681, 3685, 3688, 3692-3694, 3697, 3703, 3705, 3707, 3709-3710, 3712-3714, 3716-3719, 3721,3724, 3726, 3730, 3734, 3736-3738, 3740-3741, 3743, 3745, 3748, 3753, 3757, 3759-3761, 3764, 3768, 3770-3773, 3779, 3782-3785, 3793,3796-3797, 3800-3801, 3803-3804, 3807, 3811-3812, 3816, 3820-3821, 3829, 3832, 3839, 3841, 3847, 3849-3851, 3858, 3860, 3862-3864,3867, 3890, 3904, 3920, 3775, 3836-3837, 3869, 3873, 3876-3878, 3881, 3893, 3897, 3899, 3901-3902, 3910-3912, 3916-3917, 3924,3926-3927, 3934-3938, 3941-3944, 3947-3948, 3951, 3959-3966, 3968-3969, 3977-3981, 3989-3996

PREFACE

This section provides recommendations on thrust levers management in case of inoperativereverser(s). These recommendations are applicable in case of in-flight failure (including enginefailure) and/or in case of MEL dispatch with reverser(s) deactivated.




AT LEAST ONE REVERSER OPERATIVE

If at least one reverser is operative, the general recommendation is to select the reverser thrust onboth engines during rejected takeoff (RTO) and at landing, as per normal procedures.

Note: The ENG 1(2) REVERSER FAULT ECAM caution may be triggered after the reverser thrustis selected. This is to remind the flight crew that one reverser is inoperative.

NO REVERSERS OPERATIVE

If no reversers are operative, the general recommendation is to not select the reverser thrust duringRTO and at landing.However, the PF still sets both thrust levers to the IDLE detent, as per normal procedures.

BRIEFING

IMPORTANCE OF THE FLIGHT CREW BRIEFING

Among others, the aircraft status must be reviewed during the flight crew briefing. Anyparticularities (operational consequences, procedures, associated task sharing and callout) mustbe reviewed at that time. The flight crew must notably review:• The status of the thrust reversers and if reverser thrust can be used• Operational effect (aircraft handling during roll-out).


ABNORMAL OPERATIONSAUTOFLIGHT

ENV A318/A319/A320/A321 FLEET AO-022. P 1/2FCTM 08 JUL 08

FMGC FAILUREIdent.: AO-022-00005631.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

SINGLE FMGC FAILURE

Should a single FMGC failure occur, the AP, if engaged on affected side, will disconnect. The APwill be restored using the other FMGC. The A/THR remains operative. Furthermore, flight planinformation on the affected ND may be recovered by using same range as the opposite ND. Thecrew should consider a FMGC reset as detailed in QRH.

DUAL FMGC FAILURE

Should a dual FMGC failure occur, the AP/FD and A/THR will disconnect. The crew will try torecover both AP and A/THR by selecting them back ON (The AP and A/THR can be recovered if theFG parts of the FMGS are still available).If both AP and A/THR cannot be recovered, the thrust levers will be moved to recover manual thrust.The pilot will switch off the FDs and select TRK / FPA to allow the blue track index and the bird to bedisplayed. The RMPs will be used to tune the NAVAIDs.The crew will refer to the QRH for computer reset considerations and then will Refer to FCOM/PRO-SUP-22-A AUTOMATIC FMGS RESET AND RESYNCHRONIZATION - FM RESET to reload bothFMGC as required.


ABNORMAL OPERATIONSAUTOFLIGHT




ABNORMAL OPERATIONSELECTRICAL


INTRODUCTION TO EMERGENCY ELECTRICAL CONFIGURATIONIdent.: AO-024-00005633.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The procedure discussed in this section is the EMERGENCY ELECTRICAL CONFIGURATION. Whilstit is very unlikely that this failure will be encountered, it is useful:• To refresh on the technical background• To recall the general guidelines that must be followed in such a case• To outline the main available systems according to the electrical power source.

TECHNICAL BACKGROUNDIdent.: AO-024-00005673.0001001 / 26 MAR 08Criteria: P5768, P6387, SA�

1 Applicable to: MSN 0002-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487,0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534, 0537, 0539-0540,0542-0543, 0545, 0548-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569, 0571, 0573-0575, 0577, 0579-0580,0582, 0584-0585, 0587, 0589-0590, 0592, 0594, 0596, 0601-0603, 0605, 0607, 0611, 0613, 0615, 0617, 0619, 0622, 0624, 0626, 0628, 0630,0635, 0638, 0640, 0643, 0645, 0648, 0650, 0653, 0655, 0657-0659, 0661-0662, 0665, 0667, 0669, 0671, 0673, 0676, 0678, 0681, 0683, 0685,0696, 0698, 0701-0710, 0712, 0714, 0716, 0718, 0720, 0722, 0724, 0726, 0730, 0733, 0735, 0737, 0739, 0741, 0743, 0745, 0747, 0749, 0751,0754, 0756, 0758, 0760, 0762, 0764, 0766, 0768, 0770, 0772, 0774, 0776, 0778, 0780, 0782, 0784, 0786, 0791, 0793, 0795, 0797, 0799,0801, 0803, 0805, 0807, 0809, 0812, 0814, 0816, 0818, 0820, 0822, 0824, 0826, 0828, 0830, 0832, 0834, 0836, 0838-0839, 0842, 0844, 0846,0849, 0851, 0854, 0856-0857, 0859, 0861, 0863, 0865-0866, 0868, 0870, 0872, 0874, 0876-0877, 0879, 0881, 0883-0884, 0886, 0888, 0892,0894-0895, 0897, 0899-0900, 0902-0903, 0905, 0907, 0909, 0911-0912, 0914, 0916, 0918-0919, 0921, 0923, 0925, 0927-0928, 0930, 0932,0934, 0936-0937, 0939, 0942-0943, 0945, 0947, 0950-0951, 0953, 0955, 0957-0958, 0960, 0962, 0964, 0966-0967, 0969, 0971, 0973, 0975,0977-0978, 0981-0982, 0984, 0986, 0988, 0990, 0992, 0994, 0996, 0999, 1001, 1003, 1005, 1007, 1009, 1011, 1013-1014, 1026, 1028, 1030,1032, 1035, 1037, 1039, 1041, 1044, 1047, 1050, 1052, 1054, 1057, 1059, 1061, 1063, 1065, 1067, 1070, 1072, 1075-1076, 1079, 1081, 1083,1085, 1087, 1093, 1099, 1101, 1104-1105, 1108, 1110, 1112, 1114, 1117, 1119, 1121, 1123, 1125, 1128, 1132, 1134, 1137, 1141, 1146, 1163, 1166,1187, 1200, 1208, 1221, 1229, 1234, 1237, 1255, 1262, 1274, 1288, 1292, 1296, 1316, 1318, 1337, 1345, 1347, 1365, 1367, 1379, 1396, 1430,1454, 1461, 1484, 1516, 1530, 1535, 1540, 1550, 1633, 1641, 1646, 1655, 1674, 1694, 1700, 1736, 1789, 1793, 1809, 1812, 2082, 2092, 2104,2143, 2225, 2242, 2248, 2347, 2391

The emergency electrical configuration is due to the loss of AC BUS 1 and 2. The RAT extendsautomatically. This powers the blue hydraulic circuit which drives the emergency generator. Theemergency generator supplies both AC and DC ESS BUS.When landing gear is down, the emergency generator is no longer powered. The emergencygeneration network is automatically transferred to the batteries and AC SHED ESS and DC SHED ESSBUS are shed.Below 100 kt, the DC BAT BUS is automatically connected and below 50 kt, the AC ESS BUS is shed.




Ident.: AO-024-00005673.0002001 / 26 MAR 08Criteria: 24-1096, K2113, K3154, P5768, SA�

2 Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522,0524, 0526, 0529, 0532, 0535, 0538, 0541, 0544, 0546, 0550, 0552, 0555, 0557, 0560, 0563-0564, 0567, 0570, 0572, 0576, 0578, 0581, 0583,0586, 0588, 0591, 0593, 0595, 0597-0600, 0604, 0606, 0608-0610, 0612, 0614, 0616, 0618, 0620-0621, 0623, 0625, 0627, 0629, 0631-0634,0636-0637, 0639, 0641-0642, 0644, 0646-0647, 0649, 0651-0652, 0654, 0656, 0660, 0663-0664, 0666, 0668, 0670, 0672, 0674-0675, 0677,0679-0680, 0682, 0684, 0686-0695, 0697, 0699-0700, 0711, 0713, 0715, 0717, 0719, 0721, 0723, 0725, 0727-0729, 0731-0732, 0734, 0736,0738, 0740, 0742, 0744, 0746, 0748, 0750, 0752, 0755, 0757, 0759, 0761, 0763, 0765, 0767, 0769, 0771, 0773, 0775, 0777, 0779, 0781, 0783,0785, 0787-0790, 0792, 0794, 0796, 0798, 0800, 0802, 0804, 0806, 0808, 0810-0811, 0813, 0815, 0817, 0819, 0821, 0823, 0825, 0827, 0829,0831, 0833, 0835, 0837, 0840-0841, 0843, 0845, 0847-0848, 0850, 0852-0853, 0855, 0858, 0860, 0862, 0864, 0867, 0869, 0871, 0873, 0875,0878, 0880, 0882, 0885, 0887, 0889-0891, 0893, 0896, 0898, 0901, 0904, 0906, 0908, 0910, 0913, 0915, 0917, 0920, 0922, 0924, 0926, 0929,0931, 0933, 0935, 0938, 0940-0941, 0944, 0946, 0948-0949, 0952, 0954, 0956, 0959, 0961, 0963, 0965, 0968, 0970, 0972, 0974, 0976,0979-0980, 0983, 0985, 0987, 0989, 0991, 0993, 0995, 0997-0998, 1000, 1002, 1004, 1006, 1008, 1010, 1012, 1015-1025, 1027, 1029, 1031,1033-1034, 1036, 1038, 1040, 1042-1043, 1045-1046, 1048-1049, 1051, 1053, 1055-1056, 1058, 1060, 1062, 1064, 1066, 1068-1069, 1071,1073-1074, 1077-1078, 1080, 1082, 1084, 1086, 1088-1092, 1094-1098, 1100, 1102-1103, 1106-1107, 1109, 1111, 1113, 1115-1116, 1118, 1120,1122, 1124, 1126-1127, 1129-1131, 1133, 1135-1136, 1138-1140, 1142-1145, 1147-1162, 1164-1165, 1167-1185, 1188-1199, 1201-1207, 1209-1220,1222-1228, 1230-1233, 1235-1236, 1238-1254, 1256-1261, 1263-1273, 1275-1287, 1289-1291, 1293-1295, 1297-1315, 1317, 1319-1336,1338-1344, 1346, 1348-1364, 1366, 1368-1378, 1380-1395, 1397-1429, 1431-1453, 1455-1460, 1462-1483, 1485-1515, 1517-1529, 1531-1534,1536-1539, 1541-1549, 1551-1632, 1634-1640, 1642-1645, 1647-1654, 1656-1673, 1675-1693, 1695-1699, 1701-1735, 1737-1788, 1790-1792,1794-1808, 1810-1811, 1814-2081, 2083-2091, 2093-2103, 2105-2142, 2144-2224, 2226-2241, 2243-2247, 2249-2346, 2348-2390, 2392-3996

The emergency electrical configuration is due to the loss of AC BUS 1 and 2. The RAT extendsautomatically. This powers the blue hydraulic circuit which drives the emergency generator. Theemergency generator supplies both AC and DC ESS BUS.Below 125 kt, the RAT stalls and the emergency generator is no longer powered. The emergencygeneration network is automatically transferred to the batteries and AC SHED ESS and DC SHED ESSBUS are shed.Below 100 kt, the DC BAT BUS is automatically connected and below 50 kt, the AC ESS BUS is shed.




GENERAL GUIDELINESIdent.: AO-024-00005674.0001001 / 26 MAR 08Criteria: P5768, P6387, SA�

3 Applicable to: MSN 0002-0363, 0365-0384, 0386-0411, 0413-0432, 0435-0457, 0459-0467, 0469-0472, 0475-0476, 0478-0483, 0485-0487,0489-0492, 0496-0497, 0499-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528, 0530-0531, 0533-0534, 0537, 0539-0540,0542-0543, 0545, 0548-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569, 0571, 0573-0575, 0577, 0579-0580,0582, 0584-0585, 0587, 0589-0590, 0592, 0594, 0596, 0601-0603, 0605, 0607, 0611, 0613, 0615, 0617, 0619, 0622, 0624, 0626, 0628, 0630,0635, 0638, 0640, 0643, 0645, 0648, 0650, 0653, 0655, 0657-0659, 0661-0662, 0665, 0667, 0669, 0671, 0673, 0676, 0678, 0681, 0683, 0685,0696, 0698, 0701-0710, 0712, 0714, 0716, 0718, 0720, 0722, 0724, 0726, 0730, 0733, 0735, 0737, 0739, 0741, 0743, 0745, 0747, 0749, 0751,0754, 0756, 0758, 0760, 0762, 0764, 0766, 0768, 0770, 0772, 0774, 0776, 0778, 0780, 0782, 0784, 0786, 0791, 0793, 0795, 0797, 0799,0801, 0803, 0805, 0807, 0809, 0812, 0814, 0816, 0818, 0820, 0822, 0824, 0826, 0828, 0830, 0832, 0834, 0836, 0838-0839, 0842, 0844, 0846,0849, 0851, 0854, 0856-0857, 0859, 0861, 0863, 0865-0866, 0868, 0870, 0872, 0874, 0876-0877, 0879, 0881, 0883-0884, 0886, 0888, 0892,0894-0895, 0897, 0899-0900, 0902-0903, 0905, 0907, 0909, 0911-0912, 0914, 0916, 0918-0919, 0921, 0923, 0925, 0927-0928, 0930, 0932,0934, 0936-0937, 0939, 0942-0943, 0945, 0947, 0950-0951, 0953, 0955, 0957-0958, 0960, 0962, 0964, 0966-0967, 0969, 0971, 0973, 0975,0977-0978, 0981-0982, 0984, 0986, 0988, 0990, 0992, 0994, 0996, 0999, 1001, 1003, 1005, 1007, 1009, 1011, 1013-1014, 1026, 1028, 1030,1032, 1035, 1037, 1039, 1041, 1044, 1047, 1050, 1052, 1054, 1057, 1059, 1061, 1063, 1065, 1067, 1070, 1072, 1075-1076, 1079, 1081, 1083,1085, 1087, 1093, 1099, 1101, 1104-1105, 1108, 1110, 1112, 1114, 1117, 1119, 1121, 1123, 1125, 1128, 1132, 1134, 1137, 1141, 1146, 1163, 1166,1187, 1200, 1208, 1221, 1229, 1234, 1237, 1255, 1262, 1274, 1288, 1292, 1296, 1316, 1318, 1337, 1345, 1347, 1365, 1367, 1379, 1396, 1430,1454, 1461, 1484, 1516, 1530, 1535, 1540, 1550, 1633, 1641, 1646, 1655, 1674, 1694, 1700, 1736, 1789, 1793, 1809, 1812, 2082, 2092, 2104,2143, 2225, 2242, 2248, 2347, 2391

As only PFD1 is available, the left hand seat pilot becomes PF. Once a safe flight path is established,and the aircraft is under control, ECAM actions will be carried out.This is a serious emergency and ATC should be notified using appropriate phraseology ("MAYDAY").Although the ECAM displays LAND ASAP in red, it would be unwise to attempt an approach at apoorly equipped airfield in marginal weather. However, prolonged flight in this configuration is notrecommended.AP/FD and ATHR are lost. The flight is to be completed manually in alternate and then, when geardown, in direct law. Crews should be aware that workload is immediately greatly increased.As only the EWD is available, disciplined use of the ECAM Control Panel (ECP) is essential, (Refer toOP-040 ECAM HANDLING).In case of simultaneous engine generator, the probability of a successful APU gen coupling is low.Therefore, APU start attempts should be avoided as this will significantly reduce the flight time onbatteries (about 3.5 min for one start attempt).A clear reading of STATUS is essential to assess the aircraft status and properly sequence actionsduring the approach.The handling of this failure is referred to as a "complex procedure". A summary for handling theprocedure is included in the QRH, which will be referred to upon completion of the ECAM procedure.The ELEC EMER CONFIG SYS REMAINING list is available in QRH.

When landing gear is down, flight time is limited to 22 min as batteries are the only remaining electricalsource and flight control law reverts to direct law. Additionally, some convenient loads are lost e.g. FACfor characteristic speed or FMGC1 for ILS tuning. It is the reason why:• Landing gear extension will be delayed until reaching 1 000 ft• Navaids tuning on RMP1 will be anticipated.




The BSCU are lost. Consequently, the NWS and anti skid are lost. Alternate braking with yellowhydraulic pressure modulation up to 1 000 PSI will be used. Additionally, reversers are not available.RA 1+2 are lost with their associated call out. Call out will be made by PNF.Approaching 50 kt during the landing roll, all CRTs will be lost.

Ident.: AO-024-00005674.0002001 / 26 MAR 08Criteria: 24-1096, K2113, K3154, P5768, SA�

4 Applicable to: MSN 0364, 0385, 0412, 0434, 0458, 0468, 0473-0474, 0477, 0484, 0488, 0493-0495, 0498, 0502, 0505, 0509, 0513-0522,0524, 0526, 0529, 0532, 0535, 0538, 0541, 0544, 0546, 0550, 0552, 0555, 0557, 0560, 0563-0564, 0567, 0570, 0572, 0576, 0578, 0581, 0583,0586, 0588, 0591, 0593, 0595, 0597-0600, 0604, 0606, 0608-0610, 0612, 0614, 0616, 0618, 0620-0621, 0623, 0625, 0627, 0629, 0631-0634,0636-0637, 0639, 0641-0642, 0644, 0646-0647, 0649, 0651-0652, 0654, 0656, 0660, 0663-0664, 0666, 0668, 0670, 0672, 0674-0675, 0677,0679-0680, 0682, 0684, 0686-0695, 0697, 0699-0700, 0711, 0713, 0715, 0717, 0719, 0721, 0723, 0725, 0727-0729, 0731-0732, 0734, 0736,0738, 0740, 0742, 0744, 0746, 0748, 0750, 0752, 0755, 0757, 0759, 0761, 0763, 0765, 0767, 0769, 0771, 0773, 0775, 0777, 0779, 0781, 0783,0785, 0787-0790, 0792, 0794, 0796, 0798, 0800, 0802, 0804, 0806, 0808, 0810-0811, 0813, 0815, 0817, 0819, 0821, 0823, 0825, 0827, 0829,0831, 0833, 0835, 0837, 0840-0841, 0843, 0845, 0847-0848, 0850, 0852-0853, 0855, 0858, 0860, 0862, 0864, 0867, 0869, 0871, 0873, 0875,0878, 0880, 0882, 0885, 0887, 0889-0891, 0893, 0896, 0898, 0901, 0904, 0906, 0908, 0910, 0913, 0915, 0917, 0920, 0922, 0924, 0926, 0929,0931, 0933, 0935, 0938, 0940-0941, 0944, 0946, 0948-0949, 0952, 0954, 0956, 0959, 0961, 0963, 0965, 0968, 0970, 0972, 0974, 0976,0979-0980, 0983, 0985, 0987, 0989, 0991, 0993, 0995, 0997-0998, 1000, 1002, 1004, 1006, 1008, 1010, 1012, 1015-1025, 1027, 1029, 1031,1033-1034, 1036, 1038, 1040, 1042-1043, 1045-1046, 1048-1049, 1051, 1053, 1055-1056, 1058, 1060, 1062, 1064, 1066, 1068-1069, 1071,1073-1074, 1077-1078, 1080, 1082, 1084, 1086, 1088-1092, 1094-1098, 1100, 1102-1103, 1106-1107, 1109, 1111, 1113, 1115-1116, 1118, 1120,1122, 1124, 1126-1127, 1129-1131, 1133, 1135-1136, 1138-1140, 1142-1145, 1147-1162, 1164-1165, 1167-1185, 1188-1199, 1201-1207, 1209-1220,1222-1228, 1230-1233, 1235-1236, 1238-1254, 1256-1261, 1263-1273, 1275-1287, 1289-1291, 1293-1295, 1297-1315, 1317, 1319-1336,1338-1344, 1346, 1348-1364, 1366, 1368-1378, 1380-1395, 1397-1429, 1431-1453, 1455-1460, 1462-1483, 1485-1515, 1517-1529, 1531-1534,1536-1539, 1541-1549, 1551-1632, 1634-1640, 1642-1645, 1647-1654, 1656-1673, 1675-1693, 1695-1699, 1701-1735, 1737-1788, 1790-1792,1794-1808, 1810-1811, 1814-2081, 2083-2091, 2093-2103, 2105-2142, 2144-2224, 2226-2241, 2243-2247, 2249-2346, 2348-2390, 2392-3996

As only PFD1 is available, the left hand seat pilot becomes PF. Once a safe flight path is established,and the aircraft is under control, ECAM actions will be carried out.This is a serious emergency and ATC should be notified using appropriate phraseology ("MAYDAY").Although the ECAM displays LAND ASAP in red, it would be unwise to attempt an approach at apoorly equipped airfield in marginal weather. However, prolonged flight in this configuration is notrecommended.AP/FD and ATHR are lost. The flight is to be completed manually in alternate and then, when geardown, in direct law. Crews should be aware that workload is immediately greatly increased.As only the EWD is available, disciplined use of the ECAM Control Panel (ECP) is essential, (Refer toOP-040 ECAM HANDLING).Consideration should be given to starting the APU as indicated by the ECAM and taking into accountthe probability to restore using APU generator.A clear reading of STATUS is essential to assess the aircraft status and properly sequence actionsduring the approach.The handling of this failure is referred to as a "complex procedure". A summary for handling theprocedure is included in the QRH, which will be referred to upon completion of the ECAM procedure.The ELEC EMER CONFIG SYS REMAINING list is available in QRH.When landing gear is down, flight control law reverts to direct law.The approach speed must be at least min RAT speed (140 kt) to keep the emergency generatorsupplying the electrical network.




The BSCU are lost. Consequently, the NWS and anti skid are lost. Alternate braking with yellowhydraulic pressure modulation up to 1 000 PSI will be used. Additionally, reversers are not available.RA 1+2 are lost with their associated call out. Call out will be made by PNF.Approaching 50 kt during the landing roll, all CRTs will be lost.

REMAINING SYSTEMSIdent.: AO-024-00005675.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The electrical distribution has been designed to fly, navigate, communicate and ensure passengerscomfort. The ELEC EMER CONFIG SYS REMAINING list is available in QRH. The significantremaining systems are:

Significant remaining systems in ELEC EMER CONFIGFLY PFD1, alternate law

NAVIGATE ND1, FMGC1,, RMP1, VOR1/ILS1COMMUNICATE VHF1, HF1, ATC1

On BAT, some additional loads are lost such as FAC1 and FMGC1.


ABNORMAL OPERATIONSFIRE PROTECTION


PREFACEIdent.: AO-026-00005676.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Fire and/or smoke in the fuselage present the crew with potentially difficult situations. Not only will theyhave to deal with the emergency itself but also the passengers are likely to panic should they becomeaware of the situation. It is essential therefore, that action to control the source of combustion is notdelayed.An immediate diversion should be considered as soon as the smoke is detected. If the source is notimmediately obvious, accessible and extinguishable, it should be initiated without delay.

SMOKE DETECTION AND PROCEDURE APPLICATIONIdent.: AO-026-00005677.0001001 / 08 JAN 09Criteria: SA�

1 Applicable to: MSN 0002-3000, 3002-3029, 3031-3061, 3063-3099, 3101-3212, 3215, 3217-3237, 3239-3242, 3244-3294, 3296-3308,3310-3327, 3329-3330, 3332, 3334-3342, 3344-3361, 3364-3370, 3372-3384, 3386-3387, 3389, 3391-3411, 3413-3437, 3439-3463, 3465-3468,3470-3481, 3483-3501, 3503-3508, 3510-3514, 3516-3529, 3531, 3533-3562, 3565-3584, 3586-3597, 3599-3601, 3603-3605, 3607-3608,3610-3616, 3618-3634, 3636-3641, 3644-3665, 3667-3694, 3696-3731, 3733-3750, 3752-3814, 3816-3830, 3832-3845, 3847-3884, 3887-3896,3898-3905, 3907-3920, 3922-3931, 3933-3955, 3959-3996

The smoke will be identified either by an ECAM warning, or by the crew without any ECAM warning.If the smoke is detected by the crew, without any ECAM warning, the flight crew will refer directly to theQRH SMOKE/FUMES/AVNCS SMOKE paper procedure.If the "AVIONICS SMOKE" ECAM caution is activated, the flight crew can refer directly to the QRHSMOKE/FUMES/AVNCS SMOKE paper procedure, or apply first the ECAM actions, before enteringthe QRH.After the immediate actions, the ECAM displays a countdown (5 min). The flight crew will take theopportunity of this countdown to switch to paper procedure. When the paper procedure is entered, theflight crew will continue with this procedure, rather than coming back to the ECAM.If another ECAM SMOKE warning (e.g. LAVATORY SMOKE) is triggered, the flight crew must applythe ECAM procedure. If any doubt exists about the smoke origin, the flight crew will than refer to theQRH SMOKE/FUMES/AVNCS SMOKE paper procedure




smoke/fumes procedure architecture

Ident.: AO-026-00005677.0002001 / 08 JAN 09Criteria: P9907, SA�

2 Applicable to: MSN 3001, 3030, 3062, 3100, 3213-3214, 3216, 3238, 3243, 3295, 3309, 3328, 3331, 3333, 3343, 3362-3363, 3371, 3385,3388, 3390, 3412, 3438, 3464, 3469, 3482, 3502, 3509, 3515, 3530, 3532, 3563-3564, 3585, 3598, 3602, 3606, 3609, 3617, 3635, 3642-3643,3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886, 3897, 3906, 3921, 3932, 3956

The smoke will be identified either by an ECAM warning, or by the crew without any ECAM warning.If the smoke is detected by the crew, without any ECAM warning, the flight crew will refer directly to theQRH SMOKE/FUMES/AVNCS SMOKE paper procedure.If the "AVIONICS SMOKE" ECAM caution is activated, the flight crew can refer directly to the QRHSMOKE/FUMES/AVNCS SMOKE paper procedure, or apply first the ECAM actions, before enteringthe QRH.




If another ECAM SMOKE warning (e.g. LAVATORY SMOKE) is triggered, the flight crew must applythe ECAM procedure. If any doubt exists about the smoke origin, the flight crew will than refer to theQRH SMOKE/FUMES/AVNCS SMOKE paper procedure.

smoke/fumes procedure architecture

COORDINATION WITH CABIN CREWIdent.: AO-026-00005680.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

Good coordination between cockpit and cabin crew is a key element .




In case of smoke in the cabin, it is essential that the cabin crew estimate and inform the cockpitconcerning the density of smoke and the severity of the situation.

SMOKE/FUMES/AVNCS SMOKE PAPER PROCEDUREIdent.: AO-026-00005679.0001001 / 09 DEC 08Criteria: SA�Applicable to: ALL

GENERAL

The SMOKE/FUMES/AVNCS SMOKE paper procedure implements a global philosophy that isapplicable to both cabin and cockpit smoke cases. This philosophy includes the following mainsteps:• Diversion to be anticipated• Immediate actions

▸ If smoke source not immediately isolated:• Diversion initiation• Smoke origin identification and fighting

Furthermore, at any time during the procedure application, if smoke/fumes becomes the greatestthreat, the boxed items will be completed.The main steps of this global philosophy may be visualized in the SMOKE/FUMES/AVNCS SMOKEQRH procedure.




SMOKE/FUMES/AVNCS SMOKE procedure presentation in QRH

CONSIDERATIONS ABOUT DIVERSION

Time is critical.This is why a diversion must be immediately anticipated (as indicated by LAND ASAP).Then, after the immediate actions, if the smoke source cannot be immediately identified andisolated, the diversion must be initiated before entering the SMOKE ORIGIN IDENTIFICATION ANDFIGHTING part of the procedure.

IMMEDIATE ACTIONS

These actions are common to all cases of smoke and fumes, whatever the source.

Their objectives are:• avoiding any further contamination of the cockpit/cabin,• communication with cabin crew• flight crew protection.

3 SMOKE ORIGIN IDENTIFICATION AND FIGHTING

The crew tries to identify the smoke source by isolating systems. Some guidelines may help thecrew to identify the origin of smoke:• If smoke initially comes out of the cockpit's ventilation outlets, or if smoke is detected in the cabin,

the crew may suspect an AIR COND SMOKE. In addition, very shortly thereafter, several SMOKE




warnings (cargo, lavatory, avionics) will be triggered. The displayed ECAM procedures musttherefore be applied.

• Following an identified ENG or APU failure, smoke may emanate from the faulty item through thebleed system and be perceptible in the cockpit or the cabin. In that case, it will be re-circulatedthroughout the aircraft, until it completely disappears from the air conditioning system.

• If only the AVIONICS SMOKE warning is triggered, the crew may suspect an AVIONICS SMOKE.• If smoke is detected, while an equipment is declared faulty, the crew may suspect that smoke is

coming from this equipment.

According to the source he suspects, the crew will enter one of the 3 paragraphs:1. IF AIR COND SMOKE SUSPECTED…2. IF CAB EQUIPMENT SMOKE SUSPECTED…3. IF AVNCS/COCKPIT SMOKE SUSPECTED…

Since electrical fire is the most critical case, he will also enter paragraph 3 if he doesn't know thesource of the smoke, or if the application of paragraph 1 and/or 2 has been unsuccessful.In this part of the procedure, the flight crew must consider setting the Emergency ElectricalConfiguration, to shed as much equipment as possible. This is in order to attempt to isolate thesmoke source.If at least one battery is charging when one side and then the other side of the electrical systemare shed, the DC1, DC2, and BAT bus bars become inoperative for the remainder of the flight.Therefore, the procedure for attempting to partially shed the electrical system was removed from thesmoke procedure. This change in the procedure is to enable the flight crew to recover the normalelectrical configuration for landing, particularly to recover normal braking.If the flight crew sets the electrical emergency configuration following a smoke detection in theavionic compartment ("AVIONICS SMOKE" ECAM caution triggered), the ECAM does not displaysthe same procedure as the one displayed following the loss of main generators. In fact in thiscase, the ECAM displays a specific procedure that takes into account the smoke detection: Asthe flight crew has voluntarily set the electrical emergency configuration, the purpose of the ELECEMER CONFIG ECAM procedure is not to try to restore the generators, but to remain in electricalemergency configuration, and restore generators before landing to perform the landing in normalelectrical configuration.

BOXED ITEMS

These items (applying SMOKE REMOVAL procedure, setting electrical emergency configuration,or considering immediate landing) may be applied at any time, in the procedure (but not before theimmediate actions).Once the first step of the smoke removal procedure have been applied, the flight crew will comeback to the SMOKE/FUMES/AVNCS SMOKE procedure, to apply the appropriate steps, dependingon the suspected smoke source while descending to FL 100. Reaching FL 100, the smoke removalprocedure will be completed.




CARGO SMOKEIdent.: AO-026-00005678.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The crew should be aware that, even after successful operation of the cargo fire bottle, the CARGOSMOKE warning might persist due to the smoke detectors being sensitive to the extinguishing agent.On the ground, the crew should instruct the ground crew not to open the cargo door until thepassengers have disembarked and fire services are present.If SMOKE warning is displayed on ground with the cargo compartment door open, do not initiate anAGENT DISCHARGE. Request the ground crew to investigate and eliminate the smoke source. Onground, the warning may be triggered due to a high level of humidity.


ABNORMAL OPERATIONSFLIGHT CONTROLS


ABNORMAL FLAPS/SLATS CONFIGURATIONIdent.: AO-027-00005681.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

CAUSES

Abnormal operation of the flaps and/or slats may be due to one of the following problems:• Double SFCC failure• Double hydraulic failure (B+G or Y+G)• Flaps/Slats jammed (operation of the WTB)

CONSEQUENCES

Abnormal operation of the flaps and slats has significant consequences since:• The control laws may change• The selected speed must be used• A stabilized approach should be preferred• The approach attitudes change• Approach speeds and landing distances increase• The go-around procedure may have to be modified.

Note: The FMS predictions do not take into account the slat or flap failures. Since fuelconsumption is increased, these predictions are not valid.

FAILURE AT TAKEOFF

Should a flap/slat retraction problem occur at takeoff, the crew will PULL the speed knob for selectedspeed to stop the acceleration and avoid exceeding VFE. The overspeed warning is computedaccording to the actual slats/flaps position.The landing distance available at the departure airport and the aircraft gross weight will determinethe crew's next course of action.

FAILURE DURING THE APPROACH

The detection of a slat or flap failure occurs with the selection of flap lever during the approach. WithA/THR operative, the managed speed target will become the next manoeuvring characteristic speede.g. S speed when selecting flap lever to 1. At this stage, if a slat or flap failure occurs, the crew will:• Pull the speed knob for selected speed to avoid further deceleration• Delay the approach to complete the ECAM procedure• Refer to LANDING WITH FLAPS OR SLATS JAMMED paper check list.• Update the approach briefing

In the QRH, the line, "SPEED SEL............VFE NEXT -5 kt" is designed to allow the crew toconfigure the aircraft for landing whilst controlling the speed in a safe manner. This procedure


ABNORMAL OPERATIONSFLIGHT CONTROLS


may involve reducing speed below the manoeuvring speed for the current configuration which isacceptable provided the speed is kept above VLS. The speed reduction and configuration changesshould preferably be carried out wings level.The landing distance factors and approach speed increments are available in the QRH. (Refer toAO-010 LANDING DISTANCE PROCEDURE)Assuming VLS is displayed on the PFD, VAPP should be close to VLS + wind correction, since thisspeed is computed on the actual slat/flap position.The AP may be used down to 500 ft AGL. As the AP is not tuned for the abnormal configurations, itsbehaviour can be less than optimum and must be monitored.

During the approach briefing, emphasis should be made of:• Tail strike awareness• The go-around configuration• Any deviation from standard call out• The speeds to be flown, following a missed approach• At the acceleration altitude, selected speed must be used to control the acceleration to the

required speed for the configuration.

Consider the fuel available and the increased consumption associated with a diversion when flyingwith flaps and/or slats jammed. Additionally, when diverting with flaps/slats extended, cruise altitudeis limited to 20 000 ft.


ABNORMAL OPERATIONSFUEL


FUEL LEAKIdent.: AO-028-00005682.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

Significant fuel leaks although rare, are sometimes difficult to detect. Fuel check will be carried out by• Checking that the remaining fuel added to the burnt fuel corresponds to the fuel on board at the

gate.• Maintaining the fuel log and comparing fuel on board to expected flight plan fuel would alert the crew

to any discrepancy.

Fuel checks should be carried out when sequencing a waypoint and at least every 30 min. Anydiscrepancy should alert the crew and investigation should be carried out without delay.Should an engine failure occur, the ECAM requires the opening of the fuel X feed to avoid fuelimbalance. In case of supposed or obvious engine damages, the opening of the fuel X feed will beperformed only after being certain that there is no fuel leak.Any time an unexpected fuel quantity indication, ECAM fuel message or imbalance is noted, a fuelleak should be considered as a possible cause. Initial indications should be carefully cross-checked byreference to other means, including if possible, a visual inspection.

If a leak is suspected, the crew should action the "FUEL LEAK" abnormal checklist available in QRH:• If the leak is positively identified as coming from the engine, the affected engine is shut down to

isolate the fuel leak and fuel cross-feed valve may be used as required.• If the leak is not from the engine or cannot be located, it is imperative that the cross-feed valve is not

opened.


ABNORMAL OPERATIONSFUEL




ABNORMAL OPERATIONSHYDRAULIC


HYDRAULIC GENERATION PARTICULARITIESIdent.: AO-029-00005683.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

PREFACE

The aircraft has three continuously operating hydraulic systems: green, blue and yellow. Abidirectional Power Transfer Unit (PTU) enables the yellow system to pressurize the green systemand vice versa. Hydraulic fluid cannot be transferred from one system to another.

PTU PRINCIPLE

In flight, the PTU operates automatically if differential pressure between green and yellow systemsexceeds 500 PSI. This allows to cover the loss of one engine or one engine driven pump cases.

USE OF PTU IN CASE OF FAILURE

In case of reservoir low level, reservoir overheat, reservoir low air pressure, the PTU must beswitched OFF as required by ECAM to avoid a PTU overheat which may occur two minutes later.Indeed, a PTU overheat may lead to the loss of the second hydraulic circuit.

RECOMMENDATIONS

When required by the ECAM, the PTU should switched off without significant delay in case of:• HYD G(Y) RSVR LO LVL• HYD G(Y) RSVR LO PR• HYD G(Y) RSVR OVHT

However, if PTU has been switched off because of HYD G(Y) RSVR OVHT and the alertdisappears, affected pump may be restored and PTU switched back to AUTO.

DUAL HYDRAULIC FAILURESIdent.: AO-029-00005684.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

PREFACE

Single hydraulic failures have very little effect on the handling of the aircraft but will cause adegradation of the landing capability to CAT 3 Single.

Dual hydraulic failures however, although unlikely, are significant due to the following consequences:• Loss of AP• Flight control law degradation (ALTN)• Landing in abnormal configuration




• Extensive ECAM procedures with associated workload and task-sharing considerations• Significant considerations for approach and landing.

GENERAL GUIDELINES

It is important to note that the AP will not be available to the crew but both FD and A/THR stillremain. Additionally, depending on the affected hydraulic circuits, aircraft handling characteristicsmay be different due to the loss of some control surfaces. The PF will maneuver with care to avoidhigh hydraulic demand on the remaining systems.The PF will be very busy flying the aircraft and handling the communications with the flight controlsin Alternate Law.A double hydraulic failure is an emergency situation, with red LAND ASAP displayed, and aMAYDAY should be declared to ATC. A landing must be carried out as soon as possible bearing inmind, however, that the ECAM actions should be completed prior the approach.PF will then require the ECAM actions. A clear reading of STATUS is essential to assess the aircraftstatus and properly sequence actions during the approach.This failure is called a "complex procedure" and the QRH summary should be referred to uponcompletion of the ECAM procedure. Refer to OP-040 USE OF SUMMARIESWhile there is no need to remember the following details, an understanding of the structure of thehydraulic and flight control systems would be an advantage. The F/CTL SD page and the OPSDATA section of the QRH provide an overview of the flight controls affected by the loss of hydraulicsystems.

The briefing will concentrate on safety issues since this will be a hand-flown approach with certainhandling restrictions:• Use of the selected speeds on the FCU.• Landing gear gravity extension• Approach configuration and flap lever position• Approach speed VAPP• Tail strike awareness• Braking and steering considerations• Go around call out, aircraft configuration and speed

The STATUS page requires, in each case, a landing gear gravity extension. The LANDING GEARGRAVITY EXTENSION procedure will be completed with reference to the QRH.A stabilized approach will be preferred.




REMAINING SYSTEMSIdent.: AO-029-00005685.0001001 / 26 MAR 08Criteria: SA�


Remaining systemsFlight phase Systems HYD G+B SYS LO PR HYD G+Y SYS LO PR HYD B+Y SYS LO PR

Auto pilot Inop Inop InopYaw damper YD2 only Inop YD1 onlyControl law ALTN LAW and DI-

RECT LAW when L/G DNALTN LAW and DI-

RECT LAW when L/G DNNORM LAW

Stabilizer Avail Inop See (1) AvailSpoilers 2 SPLRS/wing 1 SPLR/wing 2 SPLRS/wingElevator R ELEV only Avail L ELEV only

Cruise

Aileron Inop Avail AvailSlats/Flaps FLAPS slow only SLATS slow Only See (2) SLATS/FLAPS slow only

L/G extension Gravity Gravity GravityBraking ALTN BRK only Y ACCU PRESS only NORM BRK onlyAnti skid Avail Inop Avail

Nose wheel steering Inop Inop Inop

Landing

Reverse REV 2 only Inop REV 1 onlyGo/around L/G retraction Inop Inop Inop

SYSTEMS PARTICULARITIES1. The stabilizer is lost. In alternate law, the auto trim function is provided through the elevators. At

landing gear extension, switching to direct law, the auto trim function is lost. However, the meanelevator position at that time is memorized, and becomes the reference for centered sidestickposition. This is why, in order to ensure proper centered sidestick position for approach and landing,the procedure requires to wait for stabilization at VAPP, before landing gear extension.If this procedure is missed, the flare and pitch control in case of go-around may be difficult.The PFD message USE MAN PITCH TRIM after landing gear extension should thus be disregarded.




2. High pitch during approach should be expected. Approach briefing should outline it for tail strikeawareness and pitch attitude will be monitored during flare.

REMAINING SYSTEMSIdent.: AO-029-00005685.0002001 / 26 MAR 08Criteria: P4576, SA�


Remaining systemsFlight phase Systems HYD G+B SYS LO PR HYD G+Y SYS LO PR HYD B+Y SYS LO PR

Auto pilot Inop Inop InopYaw damper YD2 only Inop YD1 onlyControl law ALTN LAW and DI-

RECT LAW when L/G DNALTN LAW and DI-

RECT LAW when L/G DNNORM LAW

Stabilizer Avail Inop See (1) AvailSpoilers 2 SPLRS/wing 1 SPLR/wing 2 SPLRS/wingElevator R ELEV only Avail L ELEV only

Cruise

Aileron Inop Avail AvailSlats/Flaps FLAPS slow only SLATS slow Only See (2) SLATS/FLAPS slow onlyLanding

L/G extension Gravity Gravity GravityTo be continued on next page




Continued from previous pageBraking ALTN BRK only Y ACCU PRESS only NORM BRK onlyAnti skid Avail Inop Avail

Nose wheel steering Avail Inop InopReverse REV 2 only Inop REV 1 only

Go/around L/G retraction Inop Inop Inop

SYSTEMS PARTICULARITIES1. The stabilizer is lost. In alternate law, the auto trim function is provided through the elevators. At

landing gear extension, switching to direct law, the auto trim function is lost. However, the meanelevator position at that time is memorized, and becomes the reference for centered sidestickposition. This is why, in order to ensure proper centered sidestick position for approach and landing,the procedure requires to wait for stabilization at VAPP, before landing gear extension.If this procedure is missed, the flare and pitch control in case of go-around may be difficult.The PFD message USE MAN PITCH TRIM after landing gear extension should thus be disregarded.

2. High pitch during approach should be expected. Approach briefing should outline it for tail strikeawareness and pitch attitude will be monitored during flare.


ABNORMAL OPERATIONSLANDING GEAR


LDG WITH ABNORMAL L/GIdent.: AO-032-00005686.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

This situation might occur following completion of a L/G GEAR NOT DOWNLOCKED procedure. It isalways better to land with any available gear rather than carry out a landing without any gear.In all cases, weight should be reduced as much as possible to provide the slowest possible touchdownspeed. Although foaming of the runway is not a requirement, full advantage should be taken of anyATC offer to do so.The passengers and cabin crew should be informed of the situation in good time. This will allow thecabin crew to prepare the cabin and perform their emergency landing and evacuation procedures.If one or both main landing gears in abnormal position, the ground spoilers will not be armed to keepas much roll authority as possible for maintaining the wings level. Ground spoiler extension wouldprevent spoilers from acting as roll surfaces.The crew will not arm the autobrake as manual braking will enable better pitch and roll control.Furthermore, with at least one main landing gear in the abnormal position, the autobrake cannot beactivated (ground spoilers not armed).With one main landing gear not extended, the reference speed used by the anti-skid system is notcorrectly initialized. Consequently, the anti-skid must be switched off to prevent permanent brakerelease.

In all cases, a normal approach should be flown and control surfaces used as required to maintain theaircraft in a normal attitude for as long as possible after touchdown. The engines should be shut downearly enough to ensure that fuel is cut off prior to nacelle touchdown, but late enough to keep sufficientauthority on control surfaces in order to:• Maintain runway axis• Prevent nacelle contact on first touch down• Maintain wing level and pitch attitude as long as possible.

Considering a realistic hydraulic demand, the hydraulic power remains available up to approximately30 s after the shut down of the related engine. It is the reason why the recommendations to switch theENG masters OFF are as follow:• If NOSE L/G abnormal

Before nose impact• If one MAIN L/G abnormal

At touch down.• If both MAIN L/G abnormal

In the flare, before touch down

The reversers will not be used to prevent the ground spoilers extension and because the engine willtouch the ground during roll out.


ABNORMAL OPERATIONSLANDING GEAR


The engines and APU fire pbs are pushed when the use of flight controls is no longer required i.e.when aircraft has stopped.

NOSE WHEEL STEERING FAULTIdent.: AO-032-00006423.0001001 / 08 JAN 09Criteria: SA�Applicable to: ALL

If the Nose Wheel Steering (NWS) is lost for taxiing, the flight crew can steer the aircraft withdifferential braking technique. If the flight crew does not have experience with this technique, heshould preferably request a towing to return to the gate. The flight crew can request the towing early inapproach, if the failure has been triggered in flight.


ABNORMAL OPERATIONSNAVIGATION


ADR/IRS FAULTIdent.: AO-034-00005687.0002001 / 30 JUN 08Criteria: P9171, SA�

1 Applicable to: MSN 3606, 3609, 3617, 3635, 3642-3643, 3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886, 3897, 3906, 3921, 3932, 3956

Each ADIRS has two parts (ADR and IRS), that may fail independently of each other. Additionally theIRS part may fail totally or may be available in ATT mode.Single NAV ADR FAULT or NAV IRS FAULT are simple procedures, and only require action on theswitching panel as indicated by the ECAM.Dual NAV ADR or NAV IRS failures will cause the loss of AP and A/THR and the flight controls revertto ALTN LAW.In the case of a triple ADR failure, AP and A/THR are lost and the flight controls revert to ALTN LAW.The NAV ADR 1+2+3 FAULT warning is triggered and the ECAM procedure requires that the 3 ADRsbe switched OFF, to replace the PFD's normal speed scale and altitude indication by the Back-UpSpeed Scale (BUSS) and GPS altitude information.There is no procedure for IRS 1 + 2 + 3 failure but the ECAM status page will give approach procedureand inoperative systems. In this unlikely event, the standby instruments are the only attitude, altitude,speed and heading references

Note: To switch off an ADR, the flight crew must use the ADR pushbutton. Do not use the rotaryselector, because this would also cut off the electrical supply to the IR part.

Ident.: AO-034-00005687.0001001 / 26 MAR 08Criteria: SA�

2 Applicable to: MSN 0002-3605, 3607-3608, 3610-3616, 3618-3634, 3636-3641, 3644-3665, 3667-3694, 3696-3731, 3733-3750, 3752-3814,3816-3830, 3832-3845, 3847-3884, 3887-3896, 3898-3905, 3907-3920, 3922-3931, 3933-3955, 3959-3996

Each ADIRS has two parts (ADR and IRS), that may fail independently of each other. Additionally theIRS part may fail totally or may be available in ATT mode.Single NAV ADR FAULT or NAV IRS FAULT are simple procedures, and only require action on theswitching panel as indicated by the ECAM.Dual NAV ADR or NAV IRS failures will cause the loss of AP, A/THR and flight controls revert to ALTNLAW.Due to the low probability of a triple ADR failure, the associated procedure will not be displayed on theECAM. In this case, the crew will refer to QRH procedure for ADR 1 + 2 + 3 failure.There is no procedure for IRS 1 + 2 + 3 failure but the ECAM status page will give approach procedureand inoperative systems. In this unlikely event, the standby instruments are the only attitude, altitude,speed and heading references.

Note: To switch off an ADR, the flight crew must use the ADR pushbutton. Do not use the rotaryselector, because this would also cut off the electrical supply to the IR part.




UNRELIABLE AIRSPEED INDICATIONSIdent.: AO-034-00005688.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

PREFACE

Most failures modes of the airspeed/altitude system are detected by the ADIRS. These failuresmodes lead to the loss of corresponding cockpit indications and the triggering of associated ECAMdrills.However, there may be some cases where the airspeed or altitude output is erroneous without beingrecognized as such by the ADIRS. In these cases, the cockpit indications appear normal but areactually false and pilots must rely on their basic flying skills to identify the faulty source and takethe required corrective actions. When only one source provides erroneous data, a straightforwardcrosscheck of the parameters provided by the three ADRs allows the faulty ADR to be identified.This identification becomes more difficult in the extreme situation when two, or even all of three,sources provide erroneous information.

MAIN REASONS FOR ERRONEOUS AIRSPEED/ALTITUDE DATA

The most probable reason for erroneous airspeed and altitude information is obstructed pitot tubesor static sources. Depending on the level of obstruction, the symptoms visible to the flight crew willbe different. However, in all cases, the data provided by the obstructed probe will be false. Since it ishighly unlikely that the aircraft probes will be obstructed at the same time, to the same degree andin the same way, the first indication of erroneous airspeed/altitude data available to flight crews, willmost probably be a discrepancy between the various sources.

CONSEQUENCES OF OBSTRUCTED PITOT TUBES OR STATIC PORTS

All aircraft systems, using anemometric data, have been built-in fault accommodation logics. Thefault accommodation logics are not the same for various systems but, all rely on voting principlewhereby when one source diverges from the average value, it is automatically rejected and thesystem continues to operate normally with the remaining two sources. This principle applies to flightcontrols and flight guidance systems.

NORMAL SITUATION

Each ELAC receives speed information from all ADIRUs and compares the 3 values. Pressurealtitude information is not used by the ELAC.Each FAC (Flight Augmentation Computer) receives speed information from all ADIRUs andcompares the 3 values.




ONE ADR OUTPUT IS ERRONEOUS AND THE TWO REMAINING ARE CORRECT

The ELAC and the FAC and/or FMGC eliminate it without any cockpit effect (no caution, normaloperation is continued), except that one display is wrong and CAT III DUAL is displayed as INOPSYS on STATUS page.

TWO ADR OUTPUTS ARE ERRONEOUS, BUT DIFFERENT, AND THE REMAINING ADR ISCORRECT, OR IF ALL THREE ARE ERRONEOUS, BUT DIFFERENT :

The autopilot and the auto thrust are disconnected (whichever autopilot is engaged). The ELACtriggers the F/CTL ADR DISAGREE ECAM caution. Flight controls revert to Alternate law (withouthigh and low speed protection). On both PFDs, the "SPD LIM" flag is shown; no VLS, no VSW andno VMAX is displayed.This situation is latched, until an ELAC reset is performed on ground, without any hydraulicpressure.However, if the anomaly was only transient, the autopilot and the autothrust can be re-engagedwhen the disagree has disappeared.

ONE ADR IS CORRECT, BUT THE OTHER TWO ADRS PROVIDE THE SAME ERRONEOUSOUTPUT, OR IF ALL THREE ADRS PROVIDE CONSISTENT AND ERRONEOUS DATA :

The systems will reject the "good" ADR and will continue to operate normally using the two "bad"ADRs. This condition can be met when, for example, two or all three pitot tubes are obstructed at thesame time, to the same degree, and in the same way. (Flight through a cloud of volcanic ash, takeoffwith two pitots obstructed by foreign matter (mud, insects)).The following chart provides a non-exhaustive list of the consequences of various cases of partiallyor totally obstructed pitot tubes and static ports on airspeed and altitude indications. It shouldbe noted that the cases described below cover extreme situations (e.g. totally obstructed orunobstructed drain holes), and that there could be multiple intermediate configurations with similar,but not identical, consequences.

FAILURE CASE CONSEQUENCESWater accumulated due to heavyrain. Drain holes unobstructed.

Transient speed drop until water drains. IAS fluctu-ations. IAS step drop and gradual return to normal.

Water accumulated due to heavyrain. Drain holes obstructed.

Permanent speed drop.

Ice accretion due to pitot heat failure, or transient pitotblocked due to severe icing. Unobstructed drain holes.

Total pressure leaks towards static pres-sure. IAS drop until obstruction cleared/fluc-tuation, if transient erratic A/THR is transient.





Continued from previous pageIce accretion due to pitot heat failure, or pitot obstruc-

tion due to foreign objects. Obstructed drain holes.Total pressure blocked. Constant IAS inlevel flight, until obstruction is cleared.

In climb, IAS increases. In descent, IAS decreases.

Abnormal AP/FD/ATHR behavior :a. AP/FD pitch up in OPN CLB to hold target IAS.b. AP/FD pitch down in OPN DES to hold target IAS

Total obstruction of static ports on ground. Static pressure blocked at airfield level. Normal indica-tions during T/O roll. After lift-off altitude remains con-

stant. IAS decreases, after lift-off. IAS decreases, whenaircraft climbs. IAS increases, when aircraft descends.

The above table clearly illustrates that no single rule can be given to conclusively identify all possibleerroneous airspeed/altitude indications cases.

ADR CHECK PROC / UNRELIABLE SPEED INDICATION QRH PROCEDUREIdent.: AO-034-00005690.0002001 / 08 JAN 09Criteria: P9171, SA�

3 Applicable to: MSN 3606, 3609, 3617, 3635, 3642-3643, 3666, 3695, 3732, 3751, 3815, 3831, 3846, 3885-3886, 3897, 3906, 3921, 3932, 3956

INTRODUCTION

The UNRELIABLE SPEED INDICATIONS / ADR CHECK PROC procedure has two objectives: toidentify and isolate the affected ADR (s), and, if not successful, to fly the aircraft until landing usingthe Back-Up Speed Scale (BUSS) and the GPS altitude information.

It includes the following steps:1. Memory items2. Trouble shooting and isolation3. Flight using the BUSS.

WHEN TO APPLY THIS PROCEDURE?

The flight crew may enter this procedure, either upon ECAM request (ADR DISAGREE or ANTI-ICEPITOT caution), or because he suspects an erroneous indication, without any ECAM warning.

Erroneous speed/altitude indication can be suspected by:1. Speed discrepancy (between ADR1, 2, 3, and standby indication)2. Fluctuating or unexpected increase/decrease/permanent indicated speed, or pressure altitude.3. Abnormal correlation of basic flight parameters (IAS, pitch, attitude, thrust, climb rate) :

• IAS increasing, with large nose-up pitch attitude• IAS decreasing, with large nose down pitch attitude• IAS decreasing, with nose down pitch attitude and aircraft descending

4. Abnormal AP/FD/ATHR behavior




5. STALL warning, or OVERSPEED warnings, or a Flap RELIEF ECAM message, that contradictswith at least one of the indicated speeds.• Rely on the stall warning that could be triggered in alternate or direct law. It is not affected by

unreliable speeds, because it is based on angle of attack.• Depending on the failure, the OVERSPEED warning may be false or justified. Buffet,

associated with the OVERSPEED VFE warning, is a symptom of a real overspeed condition.6. Inconsistency between radio altitude and pressure altitude.7. Reduction in aerodynamic noise with increasing speed, or increase in aerodynamic noise with

decreasing speed.8. Impossibility of extending the landing gear by the normal landing gear system.




HOW TO APPLY THIS PROCEDURE?

Because the displayed information may be erroneous, the flying accuracy cannot be assumed.Incorrect transponder altitude reporting could cause confusion. Therefore, this is an emergencysituation which requires to land as soon as possible, and a MAYDAY should be declared to adviseATC and other aircraft of the situation.

PART 1: MEMORY ITEMS

If the safe conduct of the flight is affected, the flight crew applies the memory items. They allow″safe flight conditions″ to be rapidly established in all flight phases (takeoff, climb, cruise) and




aircraft configurations (weight and slats/flaps). The memory items apply more particularly when afailure appears just after takeoff.Once the target pitch attitude and thrust values have been stabilized, the flight crew will enter theQRH abnormal procedures, to perform trouble shooting. This should not be delayed, since using thememory item parameters for a prolonged period may lead to speed limit exceedance.

PART 2: TROUBLE SHOOTING AND ISOLATION

GENERAL

If the wrong speed or altitude information does not affect the safe conduct of the flight, the crewwill not apply the memory items, and will directly enter the QRH abnormal procedures.Depending of the cause of the failure, the altitude indication may also be unreliable. There arehowever, a number of correct indications available to the crew. GPS altitude and ground speedare available on MCDU GPS monitor page and RA may be used at low altitude.

TROUBLE SHOOTING AND FAULT ISOLATION

When one indication differs from the others, flight crews may be tempted to reject the outlierinformation. They should be aware, however, that in very extreme circumstances, it may happenthat two, or even all three ADRs may provide identical and erroneous data.

BEWARE OF INSTINCTIVELY REJECTING AN OUTLIER ADR

Once the affected ADR has (or have) been positively identified, it (they) should be switchedOFF. This will trigger the corresponding ECAM warnings and associated drills, which should befollowed to address all the consequences on the various aircraft systems.In the extreme case where the affected ADR(s) cannot be identified or all speed indicationsremain unreliable, all ADRs should be switched OFF, to replace the PFD's normal speed scaleand altitude indication by the Back-Up Speed Scale (BUSS) and the GPS altitude information.With the BUSS, when all ADRs are switched OFF, the STALL WARNING is not lost.If at least one ADR remains reliable, the flight crew will use it (after having confirmed its validity),and so, will stop the application of the ADR CHECK PROC / UNRELIABLE SPEED INDICATIONPROC.

PART 3: FLYING THE BACK-UP SPEED SCALE (BUSS)

GENERAL

When the trouble shooting procedure did not permit to identify at least one correct indication, orif the NAV ADR 1+2+3 FAULT ECAM warning is triggered, the flight crew switches OFF all ADRsand flies the aircraft using the BUSS.The BUSS, displayed on both PFDs, is based on the Angle Of Attack information, and enables tocontinue a safe flight and landing in this remote failure case.




BUSS DESIGN

The BUSS design enables to fly the aircraft in the entire flight domain i.e. from high altitude andhigh Mach number to low altitude and low speed while observing the flight domain limits.The BUSS has been divided into different color-coded zones:

• The green zone provides normal margin towards ultimate limits i.e. VMO/VFE for upper limitand stall for lower limit.

• The amber zone provides limited margin towards ultimate limits. Flying the amber zone isacceptable for a limited period of time but should be avoided.

• The red zone indicates the speed range that must be avoided.

The BUSS is tuned for the aerodynamic model with the speed brake retracted. Therefore, thespeed brake must not be used, as it would affect the relation between the speed and the AOA andthe BUSS would provide erroneous data.

FLYING TECHNIQUE

When the BUSS is used:

• The AP/FD and A/THR are lost• The flight control law is in alternate law. The alpha protection and VMO/MMO warning are lost

but the stall warning remains available.




PF will fly the aircraft using the bird. CM1 will crosscheck the BUSS indications with the standbyinstrument indications if reliable.The altimeters indications are based on GPS information. As the GPS altitude is less accuratethan barometric altitude, two amber dashes replace the last two digits. The crew will note that aGPS altitude is not a FL. The vertical speed indicator is not available anymore.For approach, a stabilized approach technique will be preferred. Flight crews should change theaircraft configuration with wings levelled.Prior to the retraction/extension of the next slat/flap configuration, it is preferable to fly the higher/lower part of the green band to limit the excursion in the amber band once slat/flap is configured

Ident.: AO-034-00005690.0001001 / 30 JUN 08Criteria: SA�

4 Applicable to: MSN 0002-3605, 3607-3608, 3610-3616, 3618-3634, 3636-3641, 3644-3665, 3667-3694, 3696-3731, 3733-3750, 3752-3814,3816-3830, 3832-3845, 3847-3884, 3887-3896, 3898-3905, 3907-3920, 3922-3931, 3933-3955, 3959-3996

INTRODUCTION

The UNRELIABLE SPEED INDICATIONS / ADR CHECK PROC procedure has two objectives: toidentify and isolate the affected ADR (s), and, if not successful, to fly the aircraft until landing withoutany speed reference.

It includes the following steps:1. Memory items2. Trouble shooting and isolation3. Flight using Pitch/thrust references.

WHEN TO APPLY THIS PROCEDURE?

The flight crew may enter this procedure, either upon ECAM request (ADR DISAGREE or ANTI-ICEPITOT caution), or because he suspects an erroneous indication, without any ECAM warning.

Erroneous speed/altitude indication can be suspected by:1. Speed discrepancy (between ADR1, 2, 3, and standby indication)2. Fluctuating or unexpected increase/decrease/permanent indicated speed, or pressure altitude.3. Abnormal correlation of basic flight parameters (IAS, pitch, attitude, thrust, climb rate) :

• IAS increasing, with large nose-up pitch attitude• IAS decreasing, with large nose down pitch attitude• IAS decreasing, with nose down pitch attitude and aircraft descending

4. Abnormal AP/FD/ATHR behavior5. STALL warning, or OVERSPEED warnings, or a Flap RELIEF ECAM message, that contradicts

with at least one of the indicated speeds.• Rely on the stall warning that could be triggered in alternate or direct law. It is not affected by

unreliable speeds, because it is based on angle of attack.




• Depending on the failure, the OVERSPEED warning may be false or justified. Buffet,associated with the OVERSPEED VFE warning, is a symptom of a real overspeed condition.

6. Inconsistency between radio altitude and pressure altitude.7. Reduction in aerodynamic noise with increasing speed, or increase in aerodynamic noise with

decreasing speed.8. Impossibility of extending the landing gear by the normal landing gear system.

HOW TO APPLY THIS PROCEDURE?

Because the displayed information may be erroneous, the flying accuracy cannot be assumed.Incorrect transponder altitude reporting could cause confusion. Therefore, this is an emergencysituation which requires to land as soon as possible, and a MAYDAY should be declared to adviseATC and other aircraft of the situation.




PART 1: MEMORY ITEMS

If the safe conduct of the flight is affected, the flight crew applies the memory items. They allow″safe flight conditions″ to be rapidly established in all flight phases (takeoff, climb, cruise) andaircraft configurations (weight and slats/flaps). The memory items apply more particularly when afailure appears just after takeoff.Once the target pitch attitude and thrust values have been stabilized, as soon as above safe altitude,the flight crew will enter the QRH abnormal procedures, to level off the aircraft and perform troubleshooting. This should not be delayed, since using the memory item parameters for a prolongedperiod may lead to speed limit exceedance.

PART 2: TROUBLE SHOOTING AND ISOLATION

GENERAL

If the wrong speed or altitude information does not affect the safe conduct of the flight, the crewwill not apply the memory items, and will directly enter the QRH abnormal procedures.Depending of the cause of the failure, the altitude indication may also be unreliable. There arehowever, a number of correct indications available to the crew. GPS altitude and ground speedare available on MCDU GPS monitor page and RA may be used at low altitude.For affected ADR (s) identification, the flight crew may, either level off and stabilize the flight usingthe dedicated table in PART 2, or, if for instance already stabilized in climb, use the CLIMB tablegiven in part 3. The trouble shooting will be more accurate, using the level off table.

LEVEL OFF AND STABILIZATION (IF REQUIRED)

The table gives the proper pitch and thrust values for stabilization in level off according to weight,configuration and altitude.It must be noticed that, if the altitude information is unreliable, FPV and V/S are also affected.In this case, the GPS altitude, if available, is the only means to confirm when the aircraft ismaintaining a level. When reliable, the FPV should be used.If the memory items have been maintained for a significant period of time, the current speed maybe quite above the target.

If FPV is reliable, or if GPS altitude information is available:

‐ Maintain level flight (FPV on the horizon or constant GPS altitude)‐ Adjust thrust according to the table‐ Observe the resulting pitch attitude, and compare it with the recommended table pitch

target.• If the aircraft pitch to maintain level flight is above the table pitch target, the aircraft is

slow, then increase thrust• If the aircraft pitch to maintain level flight is below the table pitch target, the aircraft is

fast, then decrease thrust




When the pitch required to maintain level off gets close to the table pitch target, re-adjustthrust according to table thrust target.This technique permits to stabilize the speed quickly, without inducing altitude changes.If FPV is not reliable and GPS altitude information is not available (no means to ensurelevel flight):Adjust pitch and thrust according to table, and wait for speed stabilization. Expect a significantstabilization time and important altitude variations.

TROUBLE SHOOTING AND FAULT ISOLATION

When one indication differs from the others, flight crews may be tempted to reject the outlierinformation. They should be aware, however, that in very extreme circumstances, it may happenthat two, or even all three ADRs may provide identical and erroneous data.

BEWARE OF INSTINCTIVELY REJECTING AN OUTLIER ADR

Once the affected ADR has (or have) been positively identified, it (they) should be switchedOFF. This will trigger the corresponding ECAM warnings and associated drills, which should befollowed to address all the consequences on the various aircraft systems.In the extreme case where the affected ADR(s) cannot be identified or all speed indicationsremain unreliable, 2 ADRs should be selected OFF to prevent the flight control laws from usingtwo coherent but unreliable ADR data. One must be kept ON to keep the stall warning protection.If at least one ADR remains reliable, the flight crew will use it (after having confirmed its validity),and so, will stop the application of the ADR CHECK PROC / UNRELIABLE SPEED INDICATIONPROC.

PART 3: FLYING WITHOUT ANY SPEED REFERENCE

When the trouble shooting procedure did not permit to identify at least one correct indication, thispart of the procedure gives pitch/thrust reference to fly the aircraft safely, in all flight phases, down tolanding.The flight crew may enter directly this part if he knows already that no speed information is reliable(for instance in case of dual pitot heating failure, plus an ADR failure), or if level off for troubleshooting is not convenient from an operational point of view, for instance in descent, close todestination.When flying the aircraft with unreliable speed and/or altitude indications, it is recommended tochange only one flying parameter at a time i.e. speed, altitude or configuration. For this reason, awide pattern and a stabilized approach are recommended.For final approach, if available, an ILS (with a -3 ° G/S) will ensure path guidance.If final descent is started with stabilized speed (VAPP), flying a -3 ° flight path with the recommendedtable thrust, the resulting pitch attitude should be close to the recommended table pitch value. If anadjustment is required, vary the thrust, as explain in the initial level off paragraph.




DUAL RADIO ALTIMETER FAILUREIdent.: AO-034-00005689.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The Radio Altimeters (RAs) provide inputs to a number of systems, including the GPWS and FWC forauto-callouts. They also supply information to the AP and A/THR modes, plus inputs to switch flightcontrol laws at various stages. Although the ECAM procedure for a RA 1 + 2 FAULT is straightforward,the consequences of the failure on the aircraft operation require consideration.

Instead of using RA information, the flight control system uses inputs from the LGCIU to determinemode switching. Consequently, mode switching is as follows:• On approach, flare law becomes active when the L/G is selected down and provided AP is

disconnected. At this point, "USE MAN PITCH TRIM" is displayed on the PFD.• After landing, ground law becomes active when the MLG is compressed and the pitch attitude

becomes less than 2.5 °

It is not possible to capture the ILS using the APPR pb and the approach must be flown to CAT 1 limitsonly. However, it is possible to capture the localiser using the LOC pb.Furthermore, the final stages of the approach should be flown using raw data in order to avoid possibleexcessive roll rates if LOC is still engaged. Indeed, as the autopilot gains are no longer updated withthe radio altitude signal, the AP/FD behaviour may be unsatisfactory when approaching the ground.There will be no auto-callouts on approach, and no "RETARD" call in the flareThe GPWS/EGPWS will be inoperative; therefore terrain awareness becomes very important. Similarly,the "SPEED, SPEED, SPEED" low energy warning is also inoperative, again requiring increasedawareness.


ABNORMAL OPERATIONSPOWER PLANT


ALL ENGINE FLAMEOUTIdent.: AO-070-00005691.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

Following an all engine flame out, the flight deck indications change dramatically as the generatorsdrop off line. The RAT is deployed to supply the emergency generator and pressurize the bluehydraulic circuit.Control of the aircraft must be taken immediately by the left hand seat pilot, and a safe flight pathestablished.When convenient, an emergency will be declared to ATC using VHF1. Depending on the exactsituation, assistance may be available from ATC regarding position of other aircraft, safe direction etc.

Significant remaining systems in ALL ENGINES FLAME OUTFLY PFD1, Alternate law

NAVIGATE RMP1, VOR1COMMUNICATE VHF1/HF1/ATC1

Note: The AP and pitch trim are not available. Rudder trim is recoverable.

If engine wind milling is sufficient, additional hydraulic power may be recovered.The ECAM actions are displayed and allow coping with this situation. However, as the ECAM cannotdistinguish whether fuel is available or not, they provide a dimensioning procedure which cover allcases. Furthermore, The ECAM procedure refers to paper QRH for OPERATING SPEEDS, L/GGRAVITY EXTENSION and DITCHING or FORCED LANDING.It is the reason why the ENG DUAL FAILURE– FUEL REMAINING or ENG DUAL FAILURE - NOFUEL REMAINING procedures are available in the QRH. As they distinguish whether fuel is availableor not, these single paper procedures are optimized for each case and include the required paperprocedure until landing, including FORCED LANDING and DITCHING. Consequently, the crew shouldapply the QRH procedure and then, if time permits, clear ECAM warning to read status.

In the fuel remaining case,• The actions should be commenced, with attention to the optimum relight speed without starter assist

(with wind milling). If there is no relight within 30 s, the ECAM will order engine masters off for 30 s.This is to permit ventilation of the combustion chamber. Then, the engine masters may be set ONagain. Without starter assist (wind milling), this can be done at the same time.

• If the crew wants to take credit of the APU bleed air, the APU should be started below FL 250. BelowFL 200, an engine relight should be attempted with starter assist (using the APU bleed).

• Green dot, which corresponds to the optimum relight speed with starter assist, is displayed on theleft PFD. With starter assist (APU bleed), only one engine must be started at a time.


ABNORMAL OPERATIONSPOWER PLANT


All engine flame out procedure


ABNORMAL OPERATIONSMISCELLANEOUS


EMERGENCY DESCENTIdent.: AO-090-00005694.0001001 / 21 APR 08Criteria: SA�Applicable to: ALL

The emergency descent should only be initiated upon positive confirmation that cabin altitude andrate of climb is excessive and uncontrollable. This procedure should be carried out by the crew frommemory. The use of AP and auto thrust is strongly recommended for an emergency descent. The FCUselections for an emergency descent progress from right to left, i.e. ALT, HDG, SPD.At high flight levels, the speed brake should be extended slowly while monitoring VLS to avoid theactivation of angle of attack protection This would cause the speed brakes to retract and may alsoresult in AP disconnection. If structural damage is suspected, caution must be used when using speedbrakes to avoid further airframe stress. When the aircraft is established in the descent, the PF shouldrequest the ECAM actions if any or QRH.The passenger oxygen MASK MAN ON pb should be pressed only when it is clear that cabin altitudewill exceed 14 000 ft.When in idle thrust, high speed and speed brake extended, the rate of descent is approximately7 000 ft/min. To descend from FL 390 to FL 100, it takes approximately 4 min and 40 nm. The crew willbe aware that MORA displayed on ND (if available) is the highest MORA within a 80 nm circle roundthe aircraft.After taking off the emergency mask following an emergency descent, the crew should close the maskbox and reset the control slide in order to deactivate the mask microphone.




OVERWEIGHT LANDINGIdent.: AO-090-00005692.0035001 / 24 JUN 08Criteria: 32-1291, J0071, P3924, P4808, P5518, P7721, P8440, 318-100�


Automatic landing is certified up to MLW, but has been demonstrated in flight up to MTOW. Indetermining the best course of action, the flight crew may consider the option to perform an automaticlanding, provided the runway is approved for automatic landing.Should an overweight landing be required, a long straight in approach, or a wide visual pattern, shouldbe flown in order to configure the aircraft for a stabilized approach.The stabilized approach technique should be used, and VAPP established at the FAF. The speed willbe reduced to reach VLS at runway threshold, to minimize the aircraft energy.

The crew will elect the landing configuration according to the "maximum weight for go-around in CONF3" table provided both in QRH and in FCOM:• If aircraft weight is below the maximum weight for go-around in CONF 3, landing will be performed

CONF full (and go-around CONF 3) as it is the preferred configuration for optimized landingperformance

• If aircraft weight is above the maximum weight for go-around in CONF 3, landing will be performedCONF 3 (and go-around CONF 1+F). The CONF 1+F meets the approach climb gradientrequirement in all cases except in high/hot conditions. In those cases, the hot/high procedure (alsoavailable in the QRH) is to be applied. This procedure enables to increase the go around speed, inorder to increase the climb gradient.

The crew may briefly recall the main point of the go-around procedure (Configuration, call-out and anyspeed increase) once established in final approach.If a go-around CONF 1+F is carried out following an approach CONF 3, VLS CONF 1+F may be higherthan VLS CONF 3 +5 kt. The recommendation in such a case is to follow FD bars orders which willaccelerate the aircraft up to the go-around speed. It should be noted, however, that VLS CONF 1+Fequates to 1.23 VS1G whereas the minimum go-around speed required by regulations is 1.13 VS1G.This requirement is always satisfied.The crew should be aware that the transition from -3 ° flight path angle to go around climb gradientrequires a lot of energy and therefore some altitude loss.Taking into account the runway landing distance available, the use of brakes should be modulated toavoid very hot brakes and the risk of tire deflation.When the aircraft weight exceeds the maximum landing weight, structural considerations impose theability to touch down at 360 ft/min without damage. This means that no maintenance inspection isrequired if vertical speed is below 360 ft/min. If vertical speed exceeds 360 ft/min at touch down, amaintenance inspection is required.




Ident.: AO-090-00005692.0036001 / 24 JUN 08Criteria: 32-1188, 32-1196, 32-1232, 32-1244, 32-1245, 32-1247, 32-1291, 32-1336, J0071, P3924, P4808, P5518, P7721, P8440, 319-100�

2 Applicable to: MSN 0578, 0588, 0598, 0600, 0608-0610, 0612, 0616, 0618, 0621, 0623, 0625, 0627, 0629, 0636-0637, 0639, 0641, 0644,0646-0647, 0649, 0651, 0654, 0656, 0660, 0672, 0679, 0682, 0689, 0691, 0694-0695, 0697, 0700, 0713, 0717, 0723, 0727, 0729, 0734, 0738,0740, 0742, 0744, 0750, 0755, 0763, 0767, 0769, 0773, 0785, 0790, 0794, 0821, 0833, 0837, 0853, 0860, 0869, 0875, 0880, 0885, 0889-0890,0906, 0910, 0913, 0917, 0924, 0931, 0933, 0938, 0946, 0949, 0976, 0979, 0985, 0998, 1000, 1002, 1010, 1016, 1018, 1020, 1025, 1029, 1034,1036, 1038, 1043, 1046, 1048-1049, 1053, 1056, 1058, 1062, 1064, 1068-1069, 1071, 1073-1074, 1078, 1082, 1086, 1088-1092, 1095-1096,1098, 1100, 1102-1103, 1106-1107, 1111, 1113, 1115-1116, 1118, 1120, 1124, 1126-1127, 1129, 1131, 1136, 1139-1140, 1142, 1145, 1147, 1151,1154, 1157, 1159-1160, 1164-1165, 1169, 1172, 1176, 1178, 1180, 1184, 1190-1191, 1193, 1197, 1201, 1212, 1216, 1222-1223, 1225, 1228,1230, 1232, 1236, 1239, 1247, 1249, 1252, 1254, 1256, 1258, 1261, 1263, 1267, 1269, 1271, 1279, 1281, 1283, 1285, 1295, 1303, 1305, 1309,1323-1324, 1328-1329, 1331, 1335-1336, 1338, 1344, 1346, 1348, 1350, 1352, 1358, 1362, 1364, 1369, 1373-1375, 1377, 1380, 1384, 1386,1388, 1395, 1397, 1404, 1406, 1410, 1414-1415, 1423, 1429, 1434, 1440, 1444-1445, 1449, 1453, 1456, 1463, 1466, 1468, 1471, 1479, 1483,1485, 1490, 1494, 1498, 1501, 1505, 1510, 1513, 1515, 1520, 1524, 1527, 1529, 1534, 1537, 1541, 1543, 1547, 1549, 1551-1552, 1556, 1558,1563, 1565, 1574-1576, 1589-1590, 1592, 1594, 1598, 1601, 1603-1604, 1606, 1608, 1612, 1616, 1618, 1622, 1625, 1634, 1640, 1643, 1645,1654, 1656, 1677, 1679, 1698-1699, 1703, 1706, 1722, 1727, 1729, 1733, 1740, 1745, 1750, 1752-1753, 1756, 1765-1766, 1768, 1770, 1774,1778-1779, 1786, 1791, 1795-1796, 1800-1801, 1808, 1810, 1815, 1819-1820, 1824, 1826, 1828, 1831, 1833, 1837, 1839, 1844, 1846, 1853,1855, 1866, 1870, 1872, 1875, 1880, 1882, 1884, 1897, 1901, 1908, 1916, 1923, 1925, 1934, 1936, 1938, 1947, 1952, 1955, 1959, 1963, 1976,1982, 1990, 1999-2000, 2002, 2007, 2013, 2015, 2023, 2026, 2028, 2032-2033, 2037, 2039, 2043, 2047, 2050, 2052-2053, 2057, 2062, 2066,2069, 2072, 2074, 2078, 2083, 2086-2087, 2089, 2091, 2093, 2095-2096, 2098, 2101, 2103, 2113, 2119-2120, 2122, 2124, 2126-2127, 2129,2131, 2170, 2172, 2174, 2176, 2179, 2181, 2184, 2186, 2188, 2192, 2194, 2196, 2198, 2200, 2202-2203, 2205, 2209, 2213-2214, 2222, 2224,2228, 2230, 2232, 2236-2237, 2240-2241, 2243, 2245, 2249, 2251, 2253, 2258, 2260, 2262-2266, 2268-2269, 2271, 2273, 2277, 2279, 2281,2283, 2285, 2287, 2289, 2293, 2295-2296, 2298, 2300, 2302, 2304, 2306, 2308, 2311, 2313, 2318-2319, 2321, 2326, 2332, 2335, 2339, 2341,2346, 2348, 2353, 2355, 2360, 2362, 2365, 2369-2371, 2373, 2375, 2378-2380, 2382-2383, 2385, 2387, 2389, 2392, 2396, 2398, 2400, 2402,2404, 2406, 2408, 2412, 2414, 2416, 2418, 2420-2421, 2424, 2426-2427, 2429, 2431, 2433, 2435-2436, 2438, 2440, 2442, 2444, 2446, 2448,2450, 2452, 2454, 2456, 2458, 2460, 2463-2471, 2473-2474, 2477, 2481, 2483, 2485, 2487, 2490, 2492, 2494-2495, 2497, 2499-2501, 2503,2505, 2507-2508, 2510, 2512, 2514, 2516, 2518-2519, 2525, 2527-2528, 2532, 2534, 2538, 2541, 2545-2548, 2550-2551, 2554-2561, 2565,2567-2568, 2570, 2572, 2574, 2578-2579, 2581, 2585-2586, 2588, 2592-2593, 2595, 2597, 2603, 2605, 2607, 2611, 2614-2615, 2617-2618,2621-2622, 2624-2625, 2628-2629, 2631-2632, 2634, 2636, 2638-2639, 2641, 2643-2644, 2646, 2648, 2650, 2652, 2655, 2657, 2659-2660,2662, 2664, 2666-2667, 2669, 2672-2673, 2675, 2677, 2679, 2681, 2684, 2690-2691, 2693-2694, 2697-2698, 2700, 2702, 2704, 2709, 2711,2715-2716, 2718, 2720, 2723, 2727, 2729, 2733, 2735, 2738-2739, 2742, 2744, 2746, 2748, 2751, 2754, 2757, 2762-2763, 2765, 2769, 2771,2773-2774, 2777, 2779-2780, 2782, 2784, 2786, 2788, 2790, 2795, 2797, 2803, 2805-2806, 2811-2813, 2815, 2818-2819, 2821, 2825, 2827,2829, 2831, 2833, 2836-2837, 2839, 2841, 2843, 2845, 2847, 2849-2850, 2852, 2854, 2857-2858, 2860, 2864, 2866, 2870, 2872-2873, 2876,2878-2879, 2884, 2886-2894, 2897-2898, 2901, 2905, 2907, 2913, 2921, 2923, 2925, 2929, 2935, 2938, 2940, 2942, 2946, 2948-2949, 2954,2959, 2961, 2963, 2969, 2976, 2978-2979, 2981, 2983, 2985, 2997, 3003, 3007, 3011, 3017, 3019-3020, 3024, 3026, 3028, 3032, 3036, 3041,3043, 3045-3046, 3049, 3053-3054, 3057, 3059, 3061, 3065, 3069, 3073, 3077-3078, 3082, 3084-3085, 3088, 3090, 3094, 3096, 3102, 3104,3108, 3114, 3116, 3118, 3122, 3124, 3128, 3133-3134, 3137, 3139, 3142, 3144, 3165, 3168-3169, 3171-3172, 3175-3176, 3179, 3181, 3184,3186, 3188, 3193, 3195, 3200, 3202, 3204, 3209, 3226, 3231, 3243, 3245, 3248, 3250, 3252-3253, 3255, 3258, 3260, 3269, 3271, 3276, 3279,3281, 3285, 3288, 3292, 3298, 3300, 3305, 3309, 3311, 3317, 3320, 3324, 3331, 3336, 3342, 3344, 3346-3347, 3352, 3356, 3358, 3364, 3375,3377, 3380, 3385, 3388, 3393, 3395, 3403, 3406-3407, 3411, 3413, 3415, 3417, 3421, 3424, 3426, 3428, 3432, 3436, 3442-3443, 3445, 3447,3450, 3452, 3454, 3463, 3466-3467, 3491, 3500, 3513, 3518, 3520, 3533-3534, 3537, 3542, 3544, 3548, 3551, 3555, 3560-3561, 3564, 3569,3571, 3578, 3580, 3586, 3588-3590, 3595, 3604, 3608, 3614-3615, 3620, 3632, 3634, 3647, 3651, 3657, 3660-3661, 3663, 3671, 3675, 3680,3683-3687, 3689, 3691, 3694, 3700, 3702, 3704-3705, 3710, 3720, 3727-3728, 3733, 3735, 3742, 3744, 3746, 3754, 3757, 3759, 3763, 3768,3770, 3772, 3774, 3779, 3788, 3790, 3794, 3799, 3801, 3803, 3808, 3810, 3822, 3824, 3828, 3832, 3838-3839, 3841, 3844-3845, 3849, 3851,3860, 3874, 3888, 3890, 3892, 3903, 2706, 2801, 3638, 3818, 3826, 3834, 3836, 3853-3854, 3856, 3865, 3872, 3876, 3895, 3897, 3901, 3905,3911, 3918, 3950, 3962, 3970, 3983

Automatic landing is certified up to MLW, but has been demonstrated in flight up to MTOW. Indetermining the best course of action, the flight crew may consider the option to perform an automaticlanding, provided the runway is approved for automatic landing.Should an overweight landing be required, a long straight in approach, or a wide visual pattern, shouldbe flown in order to configure the aircraft for a stabilized approach.




The stabilized approach technique should be used, and VAPP established at the FAF. The speed willbe reduced to reach VLS at runway threshold, to minimize the aircraft energy.



• If aircraft weight is above the maximum weight for go-around in CONF 3, landing will be performedCONF 3 (and go-around CONF 1+F). The CONF 1+F meets the approach climb gradientrequirement in all cases (high weights, high altitude and temperature).

If a go-around CONF 1+F is carried out following an approach CONF 3, VLS CONF 1+F may behigher than VLS CONF 3 +5 kt. The recommendation in such a case is to follow SRS orders whichwill accelerate the aircraft up to the displayed VLS. It should be noted, however, that VLS CONF 1+Fequates to 1.23 VS1G whereas the minimum go-around speed required by regulations is 1.13 VS1G.This requirement is always satisfied.The crew should be aware that the transition from -3 ° flight path angle to go around climb gradientrequires a lot of energy and therefore some altitude loss.Taking into account the runway landing distance available, the use of brakes should be modulated toavoid very hot brakes and the risk of tire deflation.When the aircraft weight exceeds the maximum landing weight, structural considerations impose theability to touch down at 360 ft/min without damage. This means that no maintenance inspection isrequired if vertical speed is below 360 ft/min. If vertical speed exceeds 360 ft/min at touch down, amaintenance inspection is required.

Ident.: AO-090-00005692.0001001 / 24 JUN 08Criteria: 32-1162, 32-1174, 32-1196, 32-1232, 32-1247, 32-1336, J0071, 320-100, 320-200�

3 Applicable to: MSN 0002-0003, 0007-0021, 0043, 0045-0051, 0056-0058, 0074-0075, 0080, 0089-0090, 0095-0097, 0113-0114, 0185, 0247,0257, 0396-0398, 0416, 0423, 0431-0432, 0451, 0469, 0486, 0490, 0492, 0499

Should an overweight landing be required, a long straight in approach, or a wide visual pattern, shouldbe flown in order to configure the aircraft for a stabilized approach.The stabilized approach technique should be used, and VAPP established at the FAF. The speed willbe reduced to reach VLS at runway threshold, to minimize the aircraft energy.The crew will refer to the corresponding RTOW chart, or to FCOM to find the approach and landingconfiguration given as a function of the approach climb limiting weight.If a go-around CONF 1+F is carried out following an approach CONF 3, VLS CONF 1+F may behigher than VLS CONF 3 +5 kt. The recommendation in such a case is to follow SRS orders whichwill accelerate the aircraft up to the displayed VLS. It should be noted, however, that VLS CONF 1+Fequates to 1.23 VS1G whereas the minimum go-around speed required by regulations is 1.13 VS1G.This requirement is always satisfied.




The crew should be aware that the transition from -3 ° flight path angle to go around climb gradientrequires a lot of energy and therefore some altitude loss.Taking into account the runway landing distance available, the use of brakes should be modulated toavoid very hot brakes and the risk of tire deflation.When the aircraft weight exceeds the maximum landing weight, structural considerations impose theability to touch down at 360 ft/min without damage. This means that no maintenance inspection isrequired if vertical speed is below 360 ft/min. If vertical speed exceeds 360 ft/min at touch down, amaintenance inspection is required.

Ident.: AO-090-00005692.0037001 / 24 JUN 08Criteria: 32-1196, 32-1232, 32-1336, J0071, P5518, 321-100, 321-200�


Should an overweight landing be required, a long straight in approach, or a wide visual pattern, shouldbe flown in order to configure the aircraft for a stabilized approach.At very high weights, VFE CONF1 is close to VLS clean. To select CONF 1, deselect A/THR,decelerate to (or slightly below) VLS and select CONF 1 when below VFE. When established at CONF1, the crew can reengage A/THR and use managed speed again.The stabilized approach technique should be used, and VAPP established at the FAF. The speed willbe reduced to reach VLS at runway threshold, to minimize the aircraft energy.




Ident.: AO-090-00005692.0038001 / 24 JUN 08Criteria: 32-1162, 32-1174, 32-1188, 32-1196, 32-1232, 32-1242, 32-1244, 32-1245, 32-1247, 32-1276, 32-1291, 32-1336, J0071, P3924, P4507,P4808, P5518, P7721, P8440, 319-100, 320-100, 320-200�

5 Applicable to: MSN 0005, 0029-0042, 0044, 0052-0055, 0059-0073, 0076-0078, 0081-0088, 0091-0094, 0098-0112, 0115-0184, 0186-0246,0248-0256, 0258-0363, 0365-0384, 0386-0395, 0399-0411, 0413-0415, 0417-0422, 0424-0430, 0435-0450, 0452-0457, 0459-0467, 0470-0472,0475-0476, 0478-0483, 0485, 0487, 0489, 0491, 0496-0497, 0500-0501, 0503-0504, 0506-0508, 0510-0512, 0523, 0525, 0527-0528,0530-0531, 0533-0534, 0537, 0539-0540, 0542-0543, 0545-0549, 0551, 0553-0554, 0556, 0558-0559, 0561-0562, 0565-0566, 0568-0569,0571-0575, 0577, 0579-0580, 0582, 0584-0585, 0587, 0589-0590, 0592, 0594, 0596, 0601-0603, 0605, 0607, 0611, 0613, 0615, 0617,0619, 0622, 0624, 0626, 0628, 0630, 0634-0635, 0638, 0640, 0643, 0645, 0648, 0650, 0653, 0655, 0657-0659, 0661-0662, 0665, 0667,0669-0671, 0673, 0676, 0678, 0681, 0683, 0685-0686, 0688, 0690, 0693, 0696, 0698, 0701-0712, 0714, 0716, 0718-0722, 0724, 0726,0728, 0730, 0732-0733, 0735-0737, 0739, 0741, 0743, 0745, 0747-0749, 0751-0754, 0756-0760, 0762, 0764, 0766, 0768, 0770, 0772,0774, 0776, 0778-0780, 0782-0784, 0786, 0788, 0791, 0793, 0795, 0797-0801, 0803-0805, 0807, 0809, 0812-0814, 0816-0818, 0820, 0822,0824-0826, 0828-0832, 0834, 0836, 0838-0840, 0842-0847, 0849-0851, 0854, 0856-0859, 0861-0863, 0865-0868, 0870-0874, 0876-0877,0879, 0881-0884, 0886, 0888, 0892-0900, 0902-0905, 0907, 0909, 0911-0912, 0914, 0916, 0918-0919, 0921-0923, 0925, 0927-0930, 0932,0934, 0936-0937, 0939, 0942-0945, 0947-0948, 0950-0953, 0955, 0957-0958, 0960, 0962, 0964-0967, 0969, 0971-0973, 0975, 0977-0978,0980-0982, 0984, 0986, 0988-0990, 0992, 0994, 0996-0997, 0999, 1001, 1003, 1005, 1007, 1009, 1011, 1013-1014, 1019, 1022, 1026, 1028,1030-1033, 1035, 1037, 1039-1041, 1044, 1047, 1050-1052, 1054-1055, 1057, 1059, 1061, 1063, 1065-1067, 1070, 1072, 1075-1077, 1079,1081, 1083-1085, 1087, 1093, 1097, 1099, 1101, 1104-1105, 1108-1110, 1112, 1114, 1117, 1119, 1121-1123, 1125, 1128, 1130, 1132, 1134-1135,1137-1138, 1141, 1143, 1146, 1148-1150, 1152, 1155-1156, 1158, 1162-1163, 1166-1168, 1170-1171, 1173, 1175, 1177, 1179, 1181-1183, 1187,1189, 1192, 1194, 1196, 1198, 1200, 1203, 1205-1206, 1208-1211, 1213, 1215, 1217, 1221, 1224, 1226, 1229, 1231, 1234-1235, 1237, 1240,1242-1246, 1248, 1251, 1253, 1255, 1257, 1259, 1262, 1264-1266, 1268, 1270, 1272, 1274-1275, 1277, 1280, 1282, 1284, 1286-1292, 1294,1296-1298, 1300-1302, 1304, 1306, 1308, 1310-1322, 1325-1327, 1330, 1332, 1334, 1337, 1339-1343, 1345, 1347, 1349, 1351, 1353-1355,1357, 1359-1361, 1363, 1365, 1367-1368, 1370-1372, 1376, 1378-1379, 1381-1383, 1385, 1387, 1389-1394, 1396, 1398, 1400-1402, 1405, 1407,1409, 1411, 1413, 1416, 1418-1420, 1422, 1424, 1426-1427, 1430, 1432, 1435, 1437, 1439, 1441, 1443, 1446, 1448, 1450, 1452, 1454, 1457,1459-1461, 1464, 1467, 1469-1470, 1473-1475, 1477-1478, 1480, 1482, 1484, 1486, 1488-1489, 1491, 1493, 1495, 1497, 1500, 1502, 1504,1506-1509, 1512, 1514, 1516, 1518, 1522-1523, 1526, 1528, 1530, 1532-1533, 1535, 1538, 1540, 1542, 1544-1546, 1548, 1550, 1553, 1555,1557, 1559-1562, 1564, 1566-1571, 1573, 1577-1586, 1588, 1591, 1593, 1595, 1597, 1600, 1605, 1609-1610, 1613, 1615, 1617, 1620-1621, 1624,1626-1628, 1630-1631, 1633, 1635, 1637, 1639, 1641, 1644, 1646-1650, 1652-1653, 1655, 1657, 1659, 1661-1665, 1667-1669, 1671-1674, 1676,1678, 1680, 1682-1689, 1692-1694, 1696-1697, 1700, 1702, 1705, 1708-1710, 1712, 1714-1715, 1717-1719, 1721, 1723, 1725, 1728, 1730-1732,1735-1739, 1741-1744, 1746-1747, 1749, 1751, 1754-1755, 1757-1762, 1764, 1767, 1769, 1771, 1773, 1775, 1777, 1780-1782, 1784-1785, 1787,1789-1790, 1792-1793, 1797, 1799, 1802-1806, 1809, 1812-1814, 1816, 1818, 1821-1823, 1825, 1827, 1829, 1832, 1834-1835, 1838, 1840-1842,1845, 1847, 1849, 1851-1852, 1854, 1856-1858, 1860-1865, 1867-1868, 1871, 1873-1874, 1876-1877, 1879, 1883, 1885-1886, 1888-1896,1898-1900, 1902-1904, 1906-1907, 1909-1915, 1917-1920, 1922, 1924, 1927, 1929-1931, 1933, 1935, 1937, 1940, 1942-1945, 1948-1949,1951, 1954, 1957-1958, 1961-1962, 1964-1965, 1968-1969, 1971, 1973, 1975, 1979-1981, 1983, 1986-1987, 1989, 1993, 1996-1998, 2001,2003-2004, 2006, 2008-2012, 2014, 2016, 2018-2020, 2022, 2024, 2027, 2029-2031, 2034, 2036, 2038, 2040, 2042, 2044, 2046, 2048-2049,2054, 2056, 2058, 2061, 2063, 2065, 2068, 2070, 2073, 2075, 2077, 2079, 2082, 2084-2085, 2088, 2090, 2092, 2094, 2097, 2099, 2102, 2104,2106, 2108, 2112, 2114, 2116, 2118, 2121, 2123, 2125, 2128, 2130, 2132-2169, 2171, 2173, 2175, 2177-2178, 2180, 2182-2183, 2185, 2187,2189, 2191, 2193, 2195, 2197, 2199, 2201, 2204, 2206-2207, 2210, 2212, 2215, 2217, 2219, 2221, 2223, 2225, 2227, 2229, 2231, 2233, 2235,2238-2239, 2242, 2244, 2246, 2248, 2250, 2252, 2254, 2256-2257, 2259, 2272, 2274-2275, 2278, 2280, 2282, 2284, 2286, 2288, 2291-2292,2294, 2297, 2299, 2301, 2307, 2310, 2312, 2314, 2316, 2322, 2325, 2327, 2329, 2331, 2334, 2336, 2338, 2340, 2343, 2345, 2347, 2349, 2352,2354, 2356, 2359, 2361, 2364, 2366, 2368, 2372, 2374, 2376, 2384, 2386, 2388, 2390-2391, 2393, 2395, 2397, 2399, 2401, 2403, 2405, 2407,2409, 2411, 2413, 2415, 2417, 2419, 2422-2423, 2425, 2428, 2430, 2432, 2434, 2437, 2439, 2441, 2443, 2445, 2447, 2449, 2451, 2453, 2455,2457, 2459, 2461, 2475, 2478-2479, 2482, 2484, 2486, 2489, 2491, 2493, 2496, 2498, 2502, 2504, 2506, 2509, 2511, 2513, 2515, 2517, 2520,2522, 2524, 2526, 2529, 2531, 2533, 2535, 2537, 2539-2540, 2542, 2562, 2564, 2566, 2569, 2571, 2573, 2576-2577, 2580, 2583-2584, 2587,2589, 2591, 2594, 2596, 2598, 2600, 2602, 2604, 2606, 2608-2609, 2612-2613, 2616, 2619-2620, 2623, 2626-2627, 2630, 2633, 2635, 2637,2640, 2642, 2645, 2647, 2649, 2651, 2654, 2656, 2658, 2661, 2663, 2665, 2668, 2670-2671, 2674, 2676, 2678, 2680, 2683, 2685, 2688-2689,2692, 2695-2696, 2699, 2701, 2703, 2705, 2708, 2710, 2712, 2714, 2717, 2719, 2721, 2724-2725, 2728, 2731-2732, 2734, 2737, 2740, 2743,2745, 2747, 2749, 2752-2753, 2755, 2758, 2760-2761, 2764, 2766, 2768, 2770, 2772, 2775-2776, 2778, 2781, 2783, 2785, 2787, 2789,2791-2792, 2794, 2796, 2798, 2800, 2802, 2804, 2807-2808, 2810, 2814, 2816-2817, 2820, 2822, 2824, 2826, 2828, 2830, 2832, 2834-2835,2838, 2840, 2842, 2844, 2846, 2848, 2851, 2853, 2855-2856, 2859, 2861, 2863, 2865, 2867, 2869, 2871, 2874-2875, 2877, 2880-2881, 2883,2885, 2896, 2899-2900, 2902, 2904, 2906, 2908-2909, 2911, 2914-2915, 2917, 2920, 2922, 2924, 2926, 2928, 2930, 2932, 2934, 2937, 2939,2941, 2943-2945, 2947, 2950, 2952-2953, 2956, 2958, 2960, 2962, 2964, 2966, 2968, 2970, 2973, 2975, 2977, 2980, 2982, 2984, 2986-2995,2998, 3000, 3002, 3004, 3006, 3008, 3010, 3012, 3014, 3016, 3018, 3021, 3023, 3025, 3027, 3029, 3031, 3033, 3035, 3037, 3039-3040,3042, 3044, 3047-3048, 3050, 3052, 3055-3056, 3058, 3060, 3063-3064, 3066, 3068, 3071-3072, 3074, 3076, 3079-3080, 3083, 3086-3087,3089, 3091, 3093, 3095, 3097, 3099, 3101, 3103, 3105, 3107, 3109, 3111, 3113, 3115, 3117, 3119, 3121, 3123, 3125, 3127, 3129, 3131-3132,3135-3136, 3138, 3140-3141, 3143, 3145, 3147-3162, 3164, 3166-3167, 3170, 3173-3174, 3177-3178, 3180, 3182-3183, 3185, 3187, 3189-3190,3192, 3194, 3196-3197, 3199, 3201, 3203, 3205-3206, 3208, 3210-3211, 3213, 3215, 3218-3219, 3221, 3223-3224, 3227-3228, 3230, 3232,3234, 3236-3237, 3239-3240, 3242, 3244, 3246, 3256-3257, 3259, 3261, 3263-3264, 3266, 3268, 3270, 3272-3273, 3275, 3277-3278, 3280,3282, 3284, 3286-3287, 3289, 3291, 3293, 3295-3296, 3299, 3301, 3303-3304, 3306, 3308, 3310, 3312-3314, 3316, 3318-3319, 3321, 3323,3325, 3327-3328, 3330, 3332, 3335, 3337-3338, 3341, 3343, 3345, 3348-3349, 3351, 3353-3354, 3357, 3359, 3361-3362, 3365-3366,3368, 3370, 3373-3374, 3376, 3378-3379, 3381, 3383-3384, 3386, 3389, 3391-3392, 3394, 3396, 3398, 3400, 3402, 3404, 3408-3410,3412, 3414, 3416, 3418, 3420, 3422-3423, 3425, 3427, 3430-3431, 3433, 3435, 3437, 3439-3440, 3444, 3446, 3448-3449, 3451, 3453,3455-3457, 3460-3461, 3464-3465, 3468, 3470, 3472-3490, 3492, 3494-3497, 3499, 3501-3503, 3505-3506, 3508, 3510-3511, 3514-3517,3519, 3521, 3524, 3526, 3528-3529, 3531-3532, 3535-3536, 3538, 3540-3541, 3543, 3545, 3547, 3549-3550, 3553-3554, 3556, 3558-3559,3562-3563, 3565, 3567-3568, 3570, 3572, 3574, 3576-3577, 3579, 3581-3582, 3594, 3596-3599, 3601, 3603, 3605, 3607, 3609-3611, 3613,3616, 3618, 3621-3622, 3624, 3626-3628, 3630-3631, 3640-3641, 3643-3644, 3646, 3648-3650, 3652, 3654, 3656, 3658-3659, 3662, 3664,3666-3668, 3670, 3672, 3674, 3676-3677, 3679, 3690, 3692-3693, 3695-3699, 3701, 3703, 3706-3707, 3709, 3711, 3713-3716, 3718-3719,3721, 3723-3724, 3726, 3729, 3731-3732, 3734, 3736, 3739, 3741, 3743, 3745, 3747-3748, 3750, 3753, 3755-3756, 3760, 3762, 3765, 3767,3769, 3771, 3773, 3780-3783, 3785-3787, 3789, 3791, 3793, 3795, 3800, 3802, 3804-3805, 3807, 3809, 3811-3813, 3815, 3817, 3823, 3829,3835, 3843, 3850, 3863, 3871, 3875, 3891, 3904, 3937, 3591, 3758, 3775-3778, 3797-3798, 3819, 3821, 3825, 3827, 3831, 3833, 3837, 3840,3846, 3848, 3852, 3855, 3857, 3859, 3861, 3866, 3868, 3873, 3877, 3880, 3882-3883, 3885, 3887, 3889, 3894, 3896, 3898, 3900, 3902,3906-3910, 3912-3915, 3917, 3919, 3921-3923, 3925, 3927, 3931, 3933, 3935, 3939, 3941-3943, 3945-3947, 3949, 3952-3954, 3956-3959,3965, 3967-3968, 3971-3972, 3984, 3995

Should an overweight landing be required, a long straight in approach, or a wide visual pattern, shouldbe flown in order to configure the aircraft for a stabilized approach.




The stabilized approach technique should be used, and VAPP established at the FAF. The speed willbe reduced to reach VLS at runway threshold, to minimize the aircraft energy.





CREW INCAPACITATIONIdent.: AO-090-00005696.0001001 / 22 MAY 08Criteria: SA�Applicable to: ALL

GENERAL

Crew incapacitation is a real safety hazard which occurs more frequently than many of the otheremergencies. Incapacitation can occur in many form varying from obvious sudden death to subtle,partial loss of function. It may not be preceded by any warning.

RECOGNITION

The keys to early recognition of the incapacitation are• Routine monitoring and cross checking of flight instruments• Crew members should have a very high index of suspicion of a subtle incapacitation• If one crew member does not feel well, the other crew must be advised




• Others symptoms e.g. incoherent speech, pale fixed facial expression or irregular breathing couldindicate the beginning of an incapacitation.

ACTION

The recovery from a detected incapacitation of the fit pilot shall follow the sequence below:

First phase• Assume control, return the aircraft to a safe flight path, announce "I have control", use the take-

over pb and engage the on side AP as required.• Declare an emergency to ATC• Take whatever steps are possible to ensure the incapacitated pilot cannot interfere with the

handling of the aircraft. This may include involving cabin crew to restrain the incapacitated pilot• Request assistance from any medically qualified passenger• Check if a type qualified company pilot is on board to replace the incapacitated crew member• Land as soon as practicable after considering all pertinent factors• Arrange medical assistance after landing giving many details about the condition of the affected

crewmember

Second phase• Prepare the approach and read the checklist earlier than usual• Request radar vectoring and prefer a long approach to reduce workload• Perform the landing from the fit pilot usual seat.

SUPPLEMENTARYINFORMATION


SUPPLEMENTARY INFORMATIONPRELIMINARY PAGES

TABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET SI-PLP-TOC. P 1/2FCTM 09 JAN 09

SI-PLP. PRELIMINARY PAGESTABLE OF CONTENTS........................................................................................................................................... 1/2SUMMARY OF HIGHLIGHTS.................................................................................................................................. 1/2

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SI-010. ADVERSE WEATHERGENERAL...............................................................................................................................................................1/16COLD WEATHER OPERATIONS AND ICING CONDITIONS............................................................................... 1/16TURBULENCE........................................................................................................................................................7/16WINDSHEAR.......................................................................................................................................................... 9/16VOLCANIC ASH................................................................................................................................................... 13/16

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SI-020. FLYING REFERENCEGENERAL.................................................................................................................................................................1/6THE ATTITUDE........................................................................................................................................................ 1/6THE FLIGHT PATH VECTOR.................................................................................................................................. 1/6GO-AROUND............................................................................................................................................................4/6

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SI-030. NAVIGATION ACCURACYGENERAL.................................................................................................................................................................1/8AIRCRAFT POSITION COMPUTATION.................................................................................................................. 1/8USE OF FMS........................................................................................................................................................... 3/8AIRCRAFT POSITION AWARENESS AND OPERATIONAL CONSEQUENCES................................................... 4/8

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SI-040. ZFW - ZFCG ENTRY ERRORSZFW - ZFCG ENTRY ERRORSGENERAL.................................................................................................................................................................1/8TECHNICAL BACKGROUND...................................................................................................................................2/8ZFW ENTRY ERROR AND OPERATIONAL CONSEQUENCES............................................................................5/8OPERATIONAL RECOMMENDATIONS.................................................................................................................. 6/8

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SI-060. TCASTECHNICAL BACKGROUND...................................................................................................................................1/4OPERATIONAL RECOMMENDATIONS.................................................................................................................. 2/4

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SI-070. USE OF RADARGENERAL...............................................................................................................................................................1/10FUNCTIONS ..........................................................................................................................................................2/10



TABLE OF CONTENTS

ENV A318/A319/A320/A321 FLEET SI-PLP-TOC. P 2/2FCTM 09 JAN 09

FUNCTIONS........................................................................................................................................................... 4/10OPERATIONAL RECOMMENDATIONS FOR WEATHER DETECTION............................................................... 6/10OTHER OPERATIONAL RECOMMENDATIONS................................................................................................... 9/10

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ENV A318/A319/A320/A321 FLEET SI-PLP-SOH. P 1/2FCTM 09 JAN 09

LocalizationTitle

Page ID Reason

SI-020GO-AROUND


SI-020GO-AROUND


SI-040GENERAL


SI-040GENERAL


SI-040TECHNICAL BACKGROUND


SI-040TECHNICAL BACKGROUND


SI-040ZFW ENTRY ERROR ANDOPERATIONAL CONSEQUENCES


SI-040ZFW ENTRY ERROR ANDOPERATIONAL CONSEQUENCES


SI-040OPERATIONALRECOMMENDATIONS


SI-040OPERATIONALRECOMMENDATIONS


SI-070FUNCTIONS

2/10 1 Solution actual effectivity changed:0005,3716,3734,3736,3741,3743,3747,3748,3752,3754,3757,3760,3762,3763,3767,3770,3771,3772,3774,3775,3777,3778,3779,3780,3781,3783,3786,3787,3788,3789,3790,3792,3793,3794,3795,3797,3799,3800,3801,3804,3805,3807,3808,3809,3810,3811,3812,3814,3817,3819,3822,3823,3824,3825,3826,3834,3835,3836,3837,3838,3843,3844,3845,3854,3856,3859,3868,3871,3873,3874,3876,3877,3882,3884,3888,3889,3891,3894,3899,3901,3902,3904,3905,3909,3912,3913,3916,3917,3918,3922,3923,3926,3927,3930,3933,3937,3946,3947,3948,3952,3953,3954,3955,3965,3968,3970added,0004,0006,0017,0036,1374,2153,2309,2310,2315,2500,2509,2529,2543,2549removed

SI-070FUNCTIONS

4/10 2 Solution actual effectivity changed:2153,2309,2310,2315,2509,2529,2543,2549,3591,3698,3723,3739,3745,3750,3753,3756,3758,3759,3761,3764,3765,3766,3768,3769,3773,3776,3782,3784,3785,3791,3796,3798,3802,3803,3806,3813,3815,3816,3818,3820,3821,3827,3828,3829,3830,3831,3832,3833,3839,3840,3841,3846,3847,3848,3849,3850,3851,3852,3853,3855,3857,3858,3860,3861,3862,3863,3864,3865,3866,3867,3869,3872,3875,3878,3879,3880,3881,3883,3885,3886,3887,3890,3892,3893,3895,3896,3897,3898,3900,3903,3906,3907,3908,3910,3911,3915,3919,3920,3921,3924,3925,3928,3931,3932,3934,3935,3936,3938,3939,3940,3941,3943,3944,3945,3949,3950,3951,3956,3959,3960,3962,3964,3966,3967,3969,3971,3972,3977,3981,3983,3984,3989,3993,3995,3996added

SI-070OPERATIONALRECOMMENDATIONS FORWEATHER DETECTION

6/10 3 Solution actual effectivity changed:0005,3734,3743,3748,3754,3757,3760,3763,3770,3772,3774,3777,3779,3780,3783,3788,3790,3795,3799,3800,3801,3805,3808,3810,3811,3812,3814,3824,3825,3826,3836,3843,3844,3845,3854,3856,3859,3868,3871,3873,3876,3884,3888,3889,3891,3901,3905,3909,3913,3917,3922,3930,3933,3946,3953added,0004,0006,0017,0036,1374,2091,2097,2153,2288,2309,2310,2315,2500,2509,2529,2543,2549removed




ENV A318/A319/A320/A321 FLEET SI-PLP-SOH. P 2/2FCTM 09 JAN 09

LocalizationTitle

Page ID Reason


7/10 4 Solution actual effectivity changed:2091,2097,2288,3716,3736,3741,3747,3752,3762,3767,3771,3775,3778,3781,3786,3787,3789,3792,3793,3794,3797,3804,3807,3809,3817,3819,3822,3823,3834,3835,3837,3838,3874,3877,3882,3894,3899,3902,3904,3912,3916,3918,3923,3926,3927,3937,3947,3948,3952,3954,3955,3965,3968,3970,3984added


8/10 5 Solution actual effectivity changed:2153,2309,2310,2315,2509,2529,2543,2549,3591,3698,3723,3739,3745,3750,3753,3756,3758,3759,3761,3764,3765,3766,3768,3769,3773,3776,3782,3784,3785,3791,3796,3798,3802,3803,3806,3813,3815,3816,3818,3820,3821,3827,3828,3829,3830,3831,3832,3833,3839,3840,3841,3846,3847,3848,3849,3850,3851,3852,3853,3855,3857,3858,3860,3861,3862,3863,3864,3865,3866,3867,3869,3872,3875,3878,3879,3880,3881,3883,3885,3886,3887,3890,3892,3893,3895,3896,3897,3898,3900,3903,3906,3907,3908,3910,3911,3915,3919,3920,3921,3924,3925,3928,3931,3932,3934,3935,3936,3938,3939,3940,3941,3943,3944,3945,3949,3950,3951,3956,3959,3960,3962,3964,3966,3967,3969,3971,3972,3977,3981,3983,3989,3993,3995,3996added


SUPPLEMENTARY INFORMATIONADVERSE WEATHER

ENV A318/A319/A320/A321 FLEET SI-010. P 1/16FCTM 08 JUL 08

GENERALIdent.: SI-010-00005700.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The adverse weather operation take into account the following topics:• Cold weather operations and icing conditions• Turbulence• Windshear• Volcanic ashes

COLD WEATHER OPERATIONS AND ICING CONDITIONSIdent.: SI-010-00005701.0001001 / 30 JUN 08Criteria: SA�Applicable to: ALL

PREFACE

Aircraft performance is certified on the basis of a clean wing. Ice accretion affects wingperformance. When the wing is clean, the airflow smoothly follows the shape of the wing. Whenthe wing is covered with ice, the airflow separates from the wing when the Angle-Of-Attack (AOA)increases. Therefore, the maximum lift-coefficient is reduced. As a result, the aircraft may stall at alower AOA, and the drag may increase.The flight crew must keep in mind that the wing temperature of the aircraft may be significantly lowerthan 0 °C, after a flight at high altitude and low temperature, even if the Outside Air Temperature(OAT) is higher than 0 °C. In such cases, humidity or rain will cause ice accretion on the upperwing, and light frost under the wing. (Only 3 mm of frost on the under side of the wing tank area isacceptable.)

EXTERIOR INSPECTION

When icing conditions on ground are encountered, and/or when ice accretion is suspected, theCaptain should determine, on the basis of the exterior inspection, whether the aircraft requiresground deicing/anti-icing treatment. This visual inspection must take into account all vital parts of theaircraft, and must be performed from locations that offer a clear view of these parts.

COCKPIT PREPARATION

The following systems may be affected in very cold weather:• The EFIS/ECAM (when the cockpit temperature is very low)• The IRS alignment (may take longer than usual, up to 15 min)

The probe and window heating may be used on ground. Heating automatically operates at lowpower.




AIRCRAFT GROUND DE-ICING/ANTI-ICING

DE-ICING/ANTI-ICING FLUID

Deicing/anti-icing fluids must be able to remove ice and to prevent its accumulation on aircraftsurfaces until the beginning of the takeoff. In addition, the fluids must flow off the surfaces of theaircraft during takeoff, in order not to degrade takeoff performance.Several types of fluids can be used. These fluids have different characteristics:

type 1 type 2, 3, 4Low viscosity High viscosity

Limited hold-over time Longer hold-over timeUsed mainly for de-icing Used for de-icing and anti-icing

The holdover time starts from the beginning of the application of the fluid, and depends onthe type of fluid, and on the nature and severity of precipitation. The flight crew should refer toapplicable tables as guidelines. These tables must be used in conjunction with the pre-takeoffcheck.

Depending upon the severity of the weather, de-icing/anti-icing procedure must be applied either:• In one step, via the single application of heated and diluted deicing/anti-icing fluid: This

procedure provides a short holdover time, and should be used in low moisture conditions only.The holdover time starts from the beginning of the application of the fluid.

• In two steps, by first applying the heated deicing fluid, then by applying a protective anti-icingfluid: These two sprays must be applied consecutively. The holdover time starts from thebeginning of the application of the second fluid.

PROCEDURES

The following outlines the various procedures to be applied before and after spraying:• All ENG and APU BLEED pushbuttons must be set to OFF and the DITCHING pushbutton

must be set to ON, to prevent any engine ingestion of deicing/anti-icing fluid.• The aircraft can be deiced/anti-iced, with the engine and/or the APU running or off. However,

the APU or the engine should not be started during spraying.• The aircraft must be deiced/anti-iced symmetrically on both sides.• Keep bleeds off after spraying for a few minutes.• After spraying, keep bleeds off for a few minutes, and perform a visual inspection of the aircraft

surfaces.• A deicing/anti-icing report must be filled out to indicate the type of fluid and when the spraying

began.

AFTER START

• Keep the engine bleeds off, with the engines running at higher N1.• Keep the APU running with the bleed off for a few minutes after spraying.




• The slats/flaps and flight controls can be moved, because they no longer have ice.

TAXI OUT

On contaminated runways, the taxi speed should be limited to 10 kt, and any action that coulddistract the flight crew during taxiing should be delayed until the aircraft is stopped.

The following factors should be taken into account:• At speeds below 10 kt, anti-skid de-activates.• Engine anti-ice increases ground idle thrust.• To minimize the risk of skidding during turns: Avoid large tiller inputs.• On slippery taxiways: It may be more effective to use differential braking and/or thrust, instead of

nosewheel steering.• On slush-covered, or snow-covered, taxiways: Flap selection should be delayed until reaching the

holding point, in order to avoid contaminating the flap/slat actuation mechanism.• When reaching the holding point: The "Before Takeoff down to the line" checklist must be

performed.• The flight crew must maintain the aircraft at an appropriate distance from the aircraft in front.• In icing conditions: When holding on ground for extended periods of time, or if engine vibration

occurs, thrust should be increased periodically, and immediately before takeoff, to shed any icefrom the fan blades.

For more details about this procedure, Refer to FCOM/PRO-NOR-SOP-09-A AFTER START - ENGANTI-ICE.

TAKEOFF

TAKEOFF PERFORMANCES

The use of FLEX thrust for takeoff on contaminated runways is prohibited.If anti-ice is used at takeoff, the crew will apply the related performance penalty.Slush, standing water, or deep snow reduces the aircraft takeoff performance because ofincreased rolling resistance and the reduction in tire-to-ground friction. A higher flap setting willincrease the runway limited takeoff weight, but will reduce second segment limited takeoff weight.

TAKEOFF ROLL

Before the aircraft lines up on the runway for takeoff, the flight crew must ensure that the airframehas no ice or snow.Then, before applying thrust, the Captain should ensure that the nosewheel is straight. If there isa tendency to deviate from the runway centerline, this tendency must be neutralized immediately,via rudder pedal steering, not via the tiller.On contaminated runways, the flight crew should ensure that engine thrust advancessymmetrically to help minimize potential problems with directional control.




MAXIMUM CROSS WIND

The following table provides the maximum crosswind that corresponds to the reported runway-friction coefficient:

Reported Braking Action Reported Runway-Fric-tion Coefficient

Equivalent Run-way Condition

Maximum Cross-wind (knots)

Good/Medium 0.39 to 0.36 1 29Medium 0.35 to 0.3 2/3 25

Medium/Poor 0.29 to 0.26 2/3 20Poor ≤0.25 3/4 15

Unreliable - 4/5 5

The equivalent runway condition numbers, in the above table, correspond to the following runwayconditions:1. Dry, damp, or wet runway (less than 3 mm waterdepth)2. Runway covered with slush3. Runway covered with dry snow4. Runway covered with standing water with risk of aquaplaning or wet snow5. Icy runway or high risk of aquaplaning

CLIMB/ DESCENT

Whenever icing conditions are encountered or expected, the engine anti-ice should be turned on.Although the TAT before entering clouds may not require engine anti-ice, flight crews should beaware that the TAT often decreases significantly, when entering clouds.In climb or cruise, when the SAT decreases to lower than -40 °C, engine anti-ice should be turnedoff, unless flying near CBs.If the recommended anti-ice procedures are not performed, engine stall, over-temperature, or enginedamage may occur,

If it is necessary to turn on the engine anti-ice, and if ice accretion is visible because engine anti-icewas turned on late, then apply the following procedure:• Set the ENGINE START selector to IGN• Retard one engine, and set the ENG ANTI-ICE pushbutton to ON• Smoothly adjust thrust, and wait for stabilization• Set the ENGINE START selector to NORM• Repeat this procedure for the other engine

Wing anti-ice should be turned on, if either severe ice accretion is expected, or if there is anyindication of icing on the airframe.




HOLDING

If holding is performed in icing conditions, the flight crew should maintain clean configuration. This isbecause prolonged flight in icing conditions with the slats extended should be avoided.

APPROACH

If significant ice accretion develops on parts of the wing that have not been deiced, the aircraftspeed must be increased (Refer to FCOM/PRO-SUP-30 OPERATIONS IN ICING CONDITIONS).When the temperature is lower than ISA -10, the target altitudes (provided by the ATC) must becorrected, by adding the values that are indicated in the table below:

Corrections to be AddedHeight ISA -10 ISA -20 ISA -30

500 50 70 1001 000 100 140 1902 000 200 280 3803 000 290 420 5704 000 390 570 7605 000 490 710 950

These corrections corresponds approximately to 4 x Delta ISA x Height (ft)/1000

LANDING

Obviously, landings should be avoided on very slippery runways. However, if it is not possible toavoid such landings, the following factors (linked to operations on contaminated runways) should beconsidered:• Braking action• Directional control

BRAKING ACTION

The presence of fluid contaminants on the runway has an adverse effect on braking performance,because it reduces the friction between the tires and the surface of the runway. It also creates alayer of fluid between the tires and the runway surface, and reduces the contact area. The landingdistances, indicated in the QRH, provide a good assessment of the real landing distances forspecific levels of contamination.A firm touchdown should be made and MAX reverse should be selected, as soon as the mainlanding gear is on ground. Using reversers on a runway that is contaminated with dry snow mayreduce visibility, particularly at low speeds. In such cases, reverse thrust should be reduced toidle, if necessary.The use of MED auto-brake is recommended, when landing on an evenly contaminated runway. Itis possible that the DECEL light on the AUTO BRK panel will not come on, as the predetermineddeceleration may not be achieved. This does not mean that the auto-brake is not working.




In the case of uneven contamination on a wet or contaminated runway, the autobrake maylaterally destabilize the aircraft. If this occurs, consider deselecting the autobrake.

Typical landing distance factors versus runway condition

DIRECTIONAL CONTROL

During rollout, the sidestick must be centered. This prevents asymmetric wheel loading, thatresults in asymmetric braking and increases the weathercock tendency of the aircraft.The rudder should be used for directional control after touchdown, in the same way as for anormal landing. Use of the tiller must be avoided above taxi speed, because it may result innosewheel skidding, and lead to a loss of directional control.When required, differential braking must be applied by completely releasing the pedal on the sidethat is opposite to the expected direction of the turn. This is because, on a slippery runway, thesame braking effect may be produced by a full or half-deflection of the pedal.

Landing on a contaminated runway in crosswind requires careful consideration. In such a case,directional control problems are caused by two different factors:• If the aircraft touches down with some crab and the reverse thrust is selected, the side force

component of reverse adds to the crosswind component and causes the aircraft to drift to thedownwind side of the runway.

• As the braking efficiency increases, the cornering force of the main wheels decreases. Thisadds to any problems there may be with directional control.

If there is a problem with directional control:‐ Reverse thrust should be set to idle, in order to reduce the reverse thrust side-force component.‐ The brakes should be released, in order to increase the cornering force.




‐ The pilot should return to the runway centerline, reselect reverse thrust, and resume braking(Refer to NO-160 ROLL OUT).

The concept of equivalent runway condition is used to determine the maximum recommendedcrosswind. The following table indicates the maximum recommended crosswinds related to thereported braking actions:

Reported Braking Action Reported RunwayFriction Coefficient

Equivalent Run-way Condition

Maximum Cross-wind (knots)

Good/Medium 0.39 to 0.36 1 29Medium 0.35 to 0.3 2/3 25

Medium/Poor 0.29 to 0.26 2/3 20Poor ≤0.25 3/4 15

Unreliable - 4/5 5

TAXI IN

During taxi-in, after landing, the flaps/slats should not be retracted. This is because retraction couldcause damage, by crushing any ice that is in the slots of the slats. When the aircraft arrives at thegate, and the engines are stopped, a visual inspection should be performed to check that the slats/flaps areas are free of contamination. They may then be retracted, with the electric pumps.

PARKING

At the end of the flight, in extreme cold conditions, cold soak protection is requested when a longerstop over is expected.

TURBULENCEIdent.: SI-010-00005703.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

PREFACE

The flight crew must use weather reports and charts to determine the location and altitude ofpossible CBs, storms, and Clear Air Turbulence (CAT). If turbulence is expected, the flight crew mustturn on the seatbelt signs, in order to prepare passengers and prevent injury.

TAKE-OFF

For takeoff in high turbulence, the flight crew must wait for the target speed +20 kt (limited to VFE-5)before retracting the slats/flaps (e.g. the flight crew must wait for F+20 kt before setting Flaps 1).




IN FLIGHT

USE OF RADAR

Areas of known turbulence, associated with CBs, must be avoided. Good management of theradar tilt is essential, in order to accurately assess and evaluate the vertical development of CBs.Usually, the gain should be left in AUTO. However, selective use of manual gain may help toassess the general weather conditions. Manual gain is particularly useful, when operating inheavy rain, if the radar picture is saturated. In this case, reduced gain will help the flight crew toidentify the areas of heaviest rainfall, that are usually associated with active CB cells. After usingmanual gain, it should be reset to AUTO, in order to recover optimum radar sensitivity. A weakecho should not be a reason for the flight crew to underestimate a CB, because only the wet partsof the CB are detected. The decision to avoid a CB must be taken as early as possible, and lateralavoidance should, ideally, be at 20 nm upwind.

USE OF AP AND A/THR

If moderate turbulence is encountered, the flight crew should set the AP and A/THR to ON withmanaged speed.If severe turbulence is encountered, the flight crew should keep the AP engaged. Thrust leversshould be set to turbulence N1 (Refer to QRH), and the A/THR should then be disconnected. Useof the A/THR is, however, recommended during approach, in order to benefit from the GS mini.If the aircraft is flown manually, the flight crew should be aware of the fact that flight controllaws are designed to cope with turbulence. Therefore, they should avoid the temptation to fightturbulence, and should not over-control the sidestick.

VMO/MMO EXCEEDANCE

In turbulence, during climb, cruise or descent, the aircraft may slightly exceed VMO/MMO with theautopilot (AP) engaged.To prevent such an exceedance, adapt speed or Mach target.If severe turbulence is known or forecasted, consider the use of turbulence speed.If the current speed is close to the VMO (maximum operating speed), monitor the speed trendsymbol on the PFD.

If the speed trend reaches, or slightly exceeds, the VMO limit:• Use the FCU immediately to select a lower speed target.

If the speed trend significantly exceeds the VMO red band, without high speed protectionactivation:• Select a lower target speed on the FCU and, if the aircraft continues to accelerate, consider

disconnecting the AP.• Before re-engaging the AP, smoothly establish a shallower pitch attitude.




If the aircraft accelerates above VMO with the AP engaged, the AP will disengage on reachingthe high speed protection. The high speed protection will apply a nose-up order up to 1.75 g, inaddition to pilot input during VMO recovery. Therefore, make a smooth pitch correction in order torecover proper speed.Speedbrakes may be used in case of high speed exceedance, but the flight crew should be awareof pitch influence. In addition, speedbrakes will be used with caution, close to the ceiling.High Speed Protection may also result in activation of the angle of attack protection. Dependingon the ELAC standard, the crew may have to push on the stick to get out of this protection law.In all events, check the AP engagement status, and re-engage it when appropriate. It may havetripped and the associated aural warning may have been superseded by the overspeed auralwarning.

CONSIDERATIONS ON CAT

Clear Air Turbulence (CAT) can be expected by referring to weather charts and pilot reports.However, the radar cannot detect CAT, because it is "dry turbulence".If CAT is encountered, the flight crew may consider avoiding it vertically, keeping in mind that thebuffet margin reduces as the altitude increases.

MISCELLANEOUS

• The flight crew must set the harness to on, check that the seat belts signs are on and use allwhite lights in thunderstorms.

• Turbulence speeds are indicated in the QRH.• It is not necessary to set the ENG START selector to IGN. In the case of an engine flameout,

the igniters will trigger automatically.

WINDSHEARIdent.: SI-010-00005705.0001001 / 21 MAY 08Criteria: SA�Applicable to: ALL

BACKGROUND INFORMATION

WINSHEAR PHENOMENON

The windshear is mostly due to cool shaft of air, like a cylinder between 0.5 nm and 1.5 nm widththat is moving downward. When the air encounters the ground:• Mushrooms horizontally, causing horizontal wind gradient• Curls inward at the edges, causing vertical air mass movement.

Flight safety is affected, because:• Horizontal wind gradient significantly affects lift, causing the aircraft to descend or to reach very

high AOA.




• Vertical air mass movement severely affect the aircraft flight path.

Windshear phenomenon

AWARENESS AND AVOIDANCE

Awareness of the weather conditions that cause windshear will reduce the risk of an encounter.Studying meteorological reports and listening to tower reports will help the flight crew to assessthe weather conditions that are to be expected during takeoff or landing.If a windshear encounter is likely, the takeoff or landing should be delayed until the conditionsimprove, e.g. until a thunderstorm has moved away from the airport.

STRATEGY TO COPE WITH WINDSHEAR

The windshear and microburst are hazardous phenomena for an aircraft at takeoff or landing. Thestrategy to cope with windshear is:• Increasing flight crew awareness through the Predictive Windshear System (if available)• Informing the flight crew of unexpected air mass variations through FPV and approach speed

variations• Warning the flight crew of significant loss of energy through "SPEED, SPEED, SPEED" and

"WINDSHEAR" aural warnings (if available).• Providing effective tools to escape the shear through ALPHA FLOOR protection, SRS pitch

order, high AOA protection and Ground Speed mini protection.

Increasing flight crew awareness (if available)

When the airshaft of a microburst reaches the ground, it mushrooms outward carrying with it alarge number of falling rain droplets. The radar can measure speed variations of the droplets,and as a result, assess wind variations. This predictive capability to assess wind variations isperformed by the Predictive Windshear System (PWS). The PWS operates automatically below2 300 ft AGL, regardless of whether the radar is turned on or off. OFF.

Informing flight crew

The FPV associated with the approach speed variations (GS mini protection) is an effectivemeans for informing the flight crew of unexpected air mass variations:Approach speed variations and lateral FPV displacement reflect horizontal wind gradient.Vertical FPV displacement reflects the vertical air mass movement.




bird and target speed - wind interpretation

Warning the flight crew

The "SPEED, SPEED, SPEED" low energy warning (if available) is based on the aircraft speed,acceleration and flight path angle. This warning attracts the PF eyes to the speed scale, andrequest rapid thrust adjustment. In windshear conditions, it is the first warning to appear, beforethe activation of the alpha floor. The following table provides some typical values of the speedat which the warning could occur in two different circumstances.

Deceleration Rate Flight Path Angle Warning-1 kt/second -3 ° VLS -7 kt-1 kt/second -4 ° VLS -1 kt

In addition, the aircraft has a reactive windshear warning system. This system triggers ifthe aircraft encounters windshear. In such a case, there is a "WINDSHEAR WINDSHEARWINDSHEAR" aural warning.

Providing effictive tools

There are three efficient tools to assist the flight crew to escape:• The alpha floor protection• the SRS AP/FD pitch law• The high angle of attack protection

When the alpha floor protection is triggered, the A/THR triggers TOGA on all engines. The FMAdisplays A FLOOR, that changes to TOGA LK, when the aircraft angle-of-attack has decreased.TOGA/LK can only be deselected by turning the A/THR off.The SRS pitch mode ensures the best aircraft climb performance. Therefore, the procedurerequests following the SRS pitch bar and possibly full aft stick, in order to follow the SRS ordersand minimize the loss of height.The high angle-of-attack protection enables the PF to safely pull full aft stick, if needed, inorder to follow the SRS pitch order, or to rapidly counteract a down movement. This providesmaximum lift and minimum drag, by automatically retracting the speed brakes, if they areextended.




OPERATIONAL RECOMMENDATIONS

TAKE-OFF

Predictive windshear ("WINDSHEAR AHEAD" aural warning), if available

If predictive windshear aural warning is generated on the runway before take-off, take-off mustbe delayed.If a predictive windshear aural warning is generated during the takeoff roll, the Captain mustreject the takeoff (the aural warning is inhibited at speeds greater than 100 kt).

If the predictive windshear aural warning is generated during initial climb, the flight crew must:• Set TOGA• Closely monitor the speed and the speed trend• Ensure that the flight path does not include areas with suspected shear• Change the aircraft configuration, provided that the aircraft does not enter windshear.

Reactive windshear (WINSHEAR, WINSHEAR, WINSHEAR aural warning) or windshear detectedby pilot observation

If the windshear starts before V1 with significant speed and speed trend variations and thecaptain decides that there is sufficient runway to stop the airplane, the captain must initiate arejected take-off.

If the windshear starts after V1, the crew will set TOGA and will apply the QRH checklistactions from memory. The following points should be stressed:• The configuration should not be changed until definitely out of the shear, because operating

the landing gear doors causes additional drag.• The PF must fly SRS pitch orders rapidly and smoothly, but not aggressively, and must

consider the use of full backstick, if necessary, to minimize height loss.• The PNF should call wind variation from the ND and V/S and, when clear of the shear, report

the encounter to ATC.

APPROACH

Predictive windshear (if available)

In case the "MONITOR RADAR DISPLAY" is displayed or the ADVISORY ICON appears,the flight crew should either delay the approach or divert to another airport. However, if theapproach is continued, the flight crew should consider the following:• The weather severity must be assessed with the radar display.• A more appropriate runway must be considered.• A Conf 3 landing should be considered.• The flight crew should increase VAPP displayed on MCDU PERF APP page up to a

maximum VLS +15 kt.




• Using the TRK/FPA or ILS, for an earlier detection of vertical path deviation should beconsidered.

• In very difficult weather conditions, the A/THR response time may not be sufficient tomanage the instantaneous loss of airspeed. Refer to NO-100 FINAL APPROACH for theapplicable technique description.

• In case the "GO AROUND WINDSHEAR AHEAD" message is triggered, the PF must setTOGA for go-around. The aircraft configuration can be changed, provided that the windshearis not entered. Full back stick should be applied, if required, to follow the SRS or minimizeloss of height.

Reactive windshear (if available)

In case of the "WINDSHEAR WINDSHEAR WINDSHEAR" aural warning, the PF must setTOGA for go-around. However, the configuration (slats/flaps, gear) must not be changed untilout of the shear. The flight crew must closely monitor the flight path and speed.

VOLCANIC ASHIdent.: SI-010-00005706.0001001 / 21 MAY 08Criteria: SA�Applicable to: ALL

PREFACE

Volcanic ash or dust consists of very abrasive particles, that may cause engine surge and severedamage to aircraft surfaces that are exposed to the airflow. For this reason, operations in volcanicash must be avoided. However, if such operations cannot be avoided, the operators should apply thefollowing recommendations.

GROUND OPERATIONS

PRELIMINARY COCKPIT PREPARATION

The use of APU should be avoided whenever possible and the use of the Ground Power Unit(GPU) should be preferred.The wipers will not be used for any reason.

EXTERIOR INSPECTION

Maintenance personnel must remove ash that has settled on exposed lubricated surfaces that canpenetrate seals or enter the engine gas path, air conditioning system, air data probes and otherorifices on the aircraft. They must clean the engines air inlet of any volcanic ash. In addition, theymust clean the 25 ft area around the engine inlet.




ENGINE START

The use of an external pneumatic supply should be preferred when possible. If not possible, theAPU may be used to start the engines.Before starting the engines, the crew must use dry cranking. This will blow out any ash that mayhave entered the booster area.

TAXI

The flight crew must move forward the thrust levers smoothly to the minimum required thrust totaxi, and must avoid any sharp or high-speed turns. The bleeds must be kept OFF.

TAKE-OFF

It is advisable to use the rolling takeoff technique, and smoothly apply thrust.

IN FLIGHT

CRUISE

The flight crew must avoid flying into areas of known volcanic ash. If a volcanic eruption isreported, while the aircraft is in flight, the flight must be rerouted to remain clear of the affectedarea. The volcanic dust may spread over several hundred miles. Whenever possible, the flightcrew should stay on the upwind side of the volcano.Depending on outside conditions (night flight, clouds), volcanic dust might not be visible.

However, several phenomena can indicate that the aircraft is flying through ash cloud, forexample:• Smoke or dust in the cockpit• Acrid odour similar to electrical smoke• Engine malfunction, e.g. a rising EGT• At night, the appearance of St Elmo fire, bright white or orange glow appearing in engine inlets

or sharp and distinct beams from the landing lights.

If an ash cloud is encountered, the applicable procedure is described in the QRH. The essentialactions to be taken are:• 180 ° turn if possible. This is the quickest way to escape, because the ash cloud lateral

dimension is not known• Protecting the engines:

‐ Set A/THR to OFF‐ Decrease engines thrust if possible and maximize engine bleed to increase the engine surge

margin‐ Start the APU for further engine restart, if required

• Protecting the flight crew and passengers:‐ Don the oxygen mask




‐ Consider oxygen for the passengers.• Monitoring the flight parameters:

‐ Monitor the EGT and fuel flow, because an engine part may be eroded‐ Monitor and cross-check the IAS because an IAS indication may be corrupted

A diversion to the nearest appropriate airport should be considered.

LANDING

The use of reverse should be avoided, unless necessary.


SUPPLEMENTARY INFORMATIONFLYING REFERENCE



Two flying references may be used on the PFD:• The attitude• The Flight Path Vector (FPV), called the "bird".

The pilot selects the flight reference with the HDG/VS TRK/FPA p/b on the FCU.

THE ATTITUDEIdent.: SI-020-00005710.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

When HDG/VS is selected on the FCU, "bird" is off, and the attitude is the flight reference with HDGand VS as basic guidance parameters.The attitude flight reference should be used for dynamic manoeuvres, for example, take-off or go-around. An action on the sidestick has an immediate effect on the aircraft attitude. The flight crew canmonitor this flight reference directly and accurately during these maneuvers.

THE FLIGHT PATH VECTORIdent.: SI-020-00005711.0001001 / 21 MAY 08Criteria: SA�Applicable to: ALL

When TRK/FPA is selected on the FCU, the "bird" (the FPV) is the flight reference with the TRK andFPA as basic guidance parameters.In dynamic manoeuvres, the "bird" is directly affected by the aircraft inertia and has a delayed reaction.As a result, the "bird" should not be used as a flight reference in dynamic manoeuvres.The "bird" is the flying reference that should be used when flying a stabilized segment of trajectory, e.g.a non Precision Approach or visual circuit.

INFORMATION PRESENTATION

The FPV appears on the PFD as a symbol, known as "the bird". The bird indicates the track andflight path angle in relation to the ground.The track is indicated on the PFD by a green diamond on the compass, in addition to the lateralmovement of the bird in relation to the fixed aircraft symbol. On the ND, the track is indicated by agreen diamond on the compass scale. The difference in angle between track and heading indicatesthe drift.




The flight path angle is indicated on the PFD by the vertical movement of the bird in relation to thepitch scale.

use of FPV

With the flight directors (FDs) selected ON, the Flight Path Director (FPD) replaces the HDG-VSFlight Director (FD). With both FDs pb set to off, the blue track index appears on the PFD horizon.

PRACTICAL USES OF THE FPV

As a general rule, when using the bird, the pilot should first change attitude, and then check theresult with reference to the bird.

NON-PRECISION APPROACH

The FPV is particularly useful for non-precision approaches. The pilot can select values for theinbound track and final descent path angle on the FCU. Once established inbound, only minorcorrections should be required to maintain an accurate approach path. The pilot can monitor thetracking and descent flight path, with reference to the track indicator and the bird.However, pilots should understand that the bird only indicates a flight path angle and track, anddoes not provide guidance to a ground-based radio facility. Therefore, even if the bird indicatesthat the aircraft is flying with the correct flight path angle and track, this does not necessarilymean that the aircraft is on the correct final approach path.

VISUAL CIRCUITS

The FPV can be used as a cross-reference, when flying visual circuits. On the downwind leg,the pilot should position the wings of the bird on the horizon, in order to maintain level flight. The




downwind track should be set on the FCU. The pilot should position the tail of the bird on the bluetrack index on the PFD , in order to maintain the desired track downwind.On the final inbound approach, the track index should be set to the final approach course of therunway. A standard 3 ° approach path is indicated, when the top of the bird's tail is immediatelybelow the horizon, and the bottom of the bird is immediately above the 5 ° nose down marker.

use of FPV in final approach

FINAL APPROACH

The bird is a very useful flight reference, because it provides the trajectory parameters, andquickly warns the pilot of downburst. In addition, together with the GS MINI protection, it isan excellent indicator of shears or wind variations. The position of the "bird" in relation to thefixed aircraft symbol provides an immediate indication of the wind direction. Therefore, whenapproaching the minima, the pilot knows in which direction to search for the runway.If the target approach speed symbol moves upward, this indicates that there is headwind gust. Ifthe bird drifts to the right, this indicates that there is wind from the left.

Bird and target speed- wind interpretation




RELIABILITY

The FPV is computed from IRS data, therefore, it is affected by ADIRS errors. An error may beindicated by a small track error, usually of up to ± 2 °. This can be easily determined during theapproach.The FPV is also computed from static pressure information. Therefore, the bird must be consideredas not reliable, if altitude information is not reliable.

GO-AROUNDIdent.: SI-020-00005712.0001001 / 26 MAR 08Criteria: P4319, P6197, SA�


For the go-around, the appropriate flight reference is the attitude, because go-around is a dynamicmaneuver. Therefore, if the "bird" is on, the PF will ask the PNF to select HDG/VS, in order to recoverthe FD bars.




Ident.: SI-020-00005712.0002001 / 26 MAR 08Criteria: 22-1058, P4319, SA�


For the go-around, the appropriate flight reference is the attitude, because go-around is a dynamicmaneuver. Therefore, when performing a go-around, regardless of the previously-selected flightreference, upon selection of TOGA, the FD bars are automatically restored in SRS/GA TRK modes,and the "bird" is automatically removed.


SUPPLEMENTARY INFORMATIONNAVIGATION ACCURACY



The primary function of the FMS is navigation i.e. to compute the aircraft's position as accurately aspossible. The validity of all the others functions depends upon the accuracy of the FMS position.The accuracy of the FMS navigation determines the flight crew's strategy for using the AP/FD modes,in addition to the ND display.

AIRCRAFT POSITION COMPUTATIONIdent.: SI-030-00005715.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

WITHOUT GPS PRIMARY

PRINCIPLE

The FMS position is computed from the three IRS positions, that are combined to provide aMIXIRS position. The radio position is also combined, if two DMEs, a VOR/DME or a GPSsupplemental are available. The GPS supplemental is considered to be an additional form ofNAVAID, and can be accepted, if it falls within the radio position or the MIXIRS position.

INITIALISATION

Refer to NO-020 ADIRS INITIALIZATION

TAKE-OFF

Each FMGC uses the MIXIRS position as its position, until the thrust levers are pushed forwardto TOGA. The FMS position is then updated to the runway threshold coordinates. The differencebetween the MIXIRS position and the FMS position is referred to as the TO BIAS. The TO BIAS isadded to the MIXIRS position, for the subsequent FMS position.

FMS position updating at take off




IN FLIGHT

The original TO BIAS is continuously updated with the current radio aid.updating BIAS principle

If the radio position is lost, the system uses the updated BIAS to determine the FMS position fromthe MIXIRS position.

NAVIGATION ACCURACY

The FMS computes the Estimated Position Error (EPE). The EPE is an estimate. To computethe EPE, the FMS considers the immediately available navigation means in the FMS positioncomputation and applies defined tolerances for each of them. These tolerances assume that thenavigation means are working properly. They ignore any possible excessive IRS drift or erroneouslocations of NAVAIDs. The MCDU PROG page displays the HIGH/LOW indications, according tothe EPE. These indications reflect the probable accuracy of the FMS navigation compared to thedetermined accuracy criteria.

WITH GPS PRIMARY

PRINCIPLE

The GPS interfaces directly with the IRS that outputs a GPIRS position. When a GPIRS positionis available, it overrides the RADIO position, if available. Therefore, the FMS position tends towardthe GPIRS position.

INITIALISATION

Refer to NO-020 ADIRS INITIALIZATION

TAKE-OFF

The FM position is automatically updated at the runway threshold. With FMS2, this automaticposition update is inhibited.

IN FLIGHT

The FM position tends to the GPIRS position as long as the GPS satellites are available.




NAVIGATION ACCURACY

The GPS position is characterized by two parameters:• integrity• accuracy

The integrity is a direct function of the number of satellites in view of the aircraft. If five or moresatellites are in view, several combinations of the satellite signal may be used to process "severalpositions" and to carry out reasonableness tests on the satellite signals themselves.Accuracy functions in direct connection with the satellite constellation in view of the aircraft. If thesatellites are low on horizon, or not in appropriate positions, accuracy will be poor. It is providedas a "figure of merit".If the GPS position fulfils both the integrity and the accuracy criteria, GPS PRIMARY is displayedon the MCDU PROG page and the GPS position is the best raw data position available.

SUMMARY

FM POSITIONFlight phase WITHOUT GPS PRIMARY WITH GPS PRIMARY

On groundbefore Takeoff MIXIRS GPIRSTakeoff Updated at runway threshold (shift) (1)

With RADIO Tends to RADIO GPIRSIn flightWithout RADIO MIXIRS + BIAS GPIRS

(1) The FMS position update at take-off is inhibited with FMS2 when GPS PRIMARY is active.

USE OF FMSIdent.: SI-030-00005717.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The navigation accuracy is managed through several MCDU pages:

PROG PAGE

This page indicates GPS PRIMARY.The PROG displays the estimated navigation accuracy in green. This provides the EPE, if GPSPRIMARY LOST, or is computed by the GPS, if GPS PRIMARY is displayedThe PROG page displays the required navigation accuracy in blue (this can be changed). Therequired navigation accuracy thresholds are determined, depending on the flight phase, or can bemanually entered. These thresholds are used to change from HIGH to LOW accuracy, or vice versa.These indications are used when flying within RNP airspace.




SELECTED NAVAIDS PAGE

The SELECTED NAVAID page is accessible from DATA/POSITION MONITOR/ FREEZE/SELNAVAIDS. It has a DESELECT prompt, that enables the flight crew to prevent the FMS from usingthe GPS data to compute the position, in the case of a major problem. GPS PRIMARY lost is thendisplayed on MCDU and ND. The GPS can be reselected using the same page.

PREDICTIVE GPS PAGE (IRS HONEYWELL ONLY)

The PREDICTIVE GPS page is accessible from PROG page. The GPS PRIMARY criteria dependupon the satellite constellation status (position and number) and this is predictable. The crew canassess the GPS PRIMARY status at destination or alternate.

ND/MCDU

A GPS PRIMARY message is displayed when GPS PRIMARY is again available. This message isclearable.A GPS PRIMARY LOST message is displayed when GPS PRIMARY is lost. This message isclearable on MCDU but not on ND.When the class of navigation accuracy is downgraded from HIGH to LOW (LOW to HIGH), a NAVACCUR DOWNGRADE (UPGRADE) is displayed on ND and MCDU.

AIRCRAFT POSITION AWARENESS AND OPERATIONAL CONSEQUENCESIdent.: SI-030-00005719.0001001 / 21 MAY 08Criteria: SA�Applicable to: ALL

NAVIGATION ACCURACY INDICATIONS

The navigation accuracy indications are available on the MCDU PROG page. The followingguidelines apply:• If GPS PRIMARY is displayed, no navigation cross-check is required• If GPS PRIMARY LOST, navigation cross-check is required in climb, in cruise, about every

45 min, before Top Of Descent, reaching TMA and IAF and whenever a navigation doubt occurs.• The crew will use, IRS only, LOW and NAV ACCUR DOWNGRAD messages as indications to

trigger a navigation accuracy check.

NAVIGATION ACCURACY CROSSCHECK TECHNIQUE

The principle consists in comparing the FMS position with the RADIO position (aircraft real position).




navigation accuracy cross check technique 1

Two different techniques may be used:• Either the crew will insert a radio ident in MCDU PROG page (which provides a bearing/distance

relative to FMS position) and will compare with raw data received from the NAVAID whichmaterializes the aircraft real position. This allows the error Epsilon to be quantified.

• On the ND, the flight crew compares: The position of the needle and its associated DME distance(the real position of the aircraft) with the position of the NAVAID symbol and its associateddistance, indicated by the range markers (these markers provide a bearing/distance, in relation tothe FMS position).

navigation accuracy cross check technique 2




OPERATIONAL CONSEQUENCES

The result of the navigation accuracy crosscheck dictates the strategy the pilot will apply for the useof the ND display, the AP/FD modes, and EGPWS.

NDPF PNF

AP/FD mode EGPWS

GPS PRIMARY - Arc or Rose NAV withraw data when required

Lateral and verticalmanaged modes

ON

Navigation accuracycheck positive(≤ 3 nm)

Arc or Rose NAV withraw data when required

Lateral and verticalmanaged modes

ONCruise

Navigation accuracycheck negative(>3 nm)

ARC or ROSE NAVmay be used with care

and with raw data

Lateral and ver-tical managed

modes with carewith raw data

OFF

Navigation accuracycheck positive(≤ 1 nm)

Arc or Rose NAV with raw data Lateral and verticalmanaged modes

ON

GPS PRIMA-RY LOST

Or No GPS

Approach (1)

Navigation accuracycheck negative(>1 nm)

ROSE VOR or ILS as required Lateral and verticalselected modes

OFF

(1) A GPS defined Non Precision Approach must be interrupted if GPS PRIMARY LOST message is displayed.

POSITION UPDATE

In case of an obvious and major map shift noticed by specific messages such as "CHECK A/CPOSITION, FM1/FM2 POS MISMATCH", the aircraft position may be updated on the MCDU PROGpage. Two techniques are available:The recommended technique is to carry out a FMS update over a beacon by pressing the UPDATEprompt once estimating that the aircraft overflies the beacon using the associated needle. Thepotential error induced is approximately 4 to 5 nm. When the position update is achieved, the EPE isautomatically set to a higher value and the navigation accuracy is low.The second technique consists in updating the FM position when flying over a Point/Bearing/Distance (P/B/D) with reference to beacon raw data (Needle + Distance) rather than the beaconitself. The potential for error is far less when the distance is greater than 60 nm. The flight crew willkeep in mind the potential 180 ° error on bearing.




FM position update in flight


SUPPLEMENTARY INFORMATIONZFW - ZFCG ENTRY ERRORSZFW - ZFCG ENTRY ERRORS


GENERALIdent.: SI-040-00005722.0001001 / 26 MAR 08Criteria: SA�


The aircraft Gross Weight (GW) and Centre of Gravity (CG) are computed independently by the FMand FAC:

GW and CG values FM computed are used for:• FM predictions and speeds• ECAM (GW)• MCDU (GW and CG)GW and CG values FAC computed are used for:• Flight control laws• Computation of characteristic speeds (VLS, F, S, GD) for display on PFD

A ZFW or ZFWCG entry error in MCDU INIT B page induces calculation errors that are to behighlighted.

Ident.: SI-040-00005722.0002001 / 26 MAR 08Criteria: SA, 318-100�


The aircraft Gross Weight (GW) and Centre of Gravity (CG) are computed independently by the FMand FAC:

GW and CG values FM computed are used for:• FM predictions and speeds• ECAM (GW)• MCDU (GW and CG)• Computation of characteristic speeds (VLS, F, S, GD) for display on PFDGW and CG values FAC computed are used for:• Flight control laws

A ZFW or ZFWCG entry error in MCDU INIT B page induces calculation errors that are to behighlighted.




TECHNICAL BACKGROUNDIdent.: SI-040-00005723.0001001 / 26 MAR 08Criteria: SA�


The GW and CG computation is as follows:1. The pilot enters the ZFW and ZFWCG in the MCDU INIT B page2. The FMGC computes the GW and CG from:

• The ZFW, ZFWCG inserted in the MCDU INIT B page• The fuel quantities from the Fuel Quantity Indicator (FQI)• The Fuel Flow from the FADEC.

3. This current GW and/or CG is used for:• FM predictions and speeds• ECAM (GW only)• MCDU (GW and CG)

4. The FAC computes its own GW and CG from aerodynamic data.5. GW and CG FAC computed are used for:

• Minor adjustments on the flight control laws• Characteristic speeds (VLS, F, S, Green dot) display on PFD.




Note: 1. On ground, FAC uses the GW FM computed.2. In flight, at low altitude (below 15 000 ft), low speed (below 250 kt) and flight parameters

stabilized, GW FAC computed comes from aerodynamic data. If these conditions are notmet, GW FAC computed equates to the last memorized GW - fuel used.

3. If the GW FM computed and FAC computed differs from a given threshold, a "CHECK GW"message appears on the MCDU scratchpad.



The GW and CG computation is as follows:1. The pilot enters the ZFW and ZFWCG in the MCDU INIT B page2. The FMGC computes the GW and CG from:

• The ZFW, ZFWCG inserted in the MCDU INIT B page• The fuel quantities from the Fuel Quantity Indicator (FQI)• The Fuel Flow from the FADEC.

3. This current GW and/or CG is used:• For FM predictions and speeds• For ECAM display (GW only)




• For MCDU (GW and CG)• By FAC for characteristic speed computation for PFD

4. The FAC computes its own GW and CG from aerodynamic data.5. GW and CG FAC computed are used for:

• Minor adjustments on the flight control laws

Note: 1. On ground, FAC takes the GW FM computed2. In flight, at low altitude (below 15 000 ft), low speed (below 250 kt) and flight parameters

stabilized, GW FAC computed comes from aerodynamic data. If these conditions are notmet, GW FAC computed equates to the last memorized GW - fuel used.

3. If the GW FM computed and FAC computed differs from a given threshold, a "CHECK GW"message appears on the MCDU scratchpad.




ZFW ENTRY ERROR AND OPERATIONAL CONSEQUENCESIdent.: SI-040-00005724.0001001 / 22 APR 08Criteria: SA�


If the pilot enters erroneous ZFW on MCDU INIT B page, this will affect as follows:GW and, to a lesser degree, CG, computed by FM are erroneous. This induces the followingconsequences:• The FM predictions and speeds are erroneous• Incorrect GW and CG on MCDU FUEL PRED page• Incorrect GW displayed on ECAMFAC GW, which is based on FM GW on ground, will be updated only once airborne through aspecific slow calculation using AOA information. Consequently,• Characteristic speeds on PFD at take-off are erroneous, but they are correct in flight• SRS mode guidance is affected if computed VLS is above V2 as inserted in the MCDU PERF

TAKE-OFF page.

Note: 1. In flight, if the FM and FAC GW differ from a given threshold, a "CHECK GW" message istriggered on the MCDU.

2. Valpha prot, Valpha max, Vsw are not affected since based on aerodynamic data.

ERRONEOUS FUEL ON BOARD ENTRY

As long as the engines are not started, the FM GW is erroneous and above-mentionedconsequences apply. Once the engines are started, the fuel figures are updated and downstreamdata update accordingly.It should be noted however, that the FOB on ECAM is correct since it is provided from FQI data.

Ident.: SI-040-00005724.0002001 / 22 APR 08Criteria: SA, 318-100�


If the pilot enters erroneous ZFW on MCDU INIT B page, this will affect as follows:GW and, to a lesser degree, CG, computed by FM are erroneous. This induces the followingconsequences:• The FM predictions and speeds are erroneous• Incorrect GW and CG on MCDU FUEL PRED page




• Incorrect GW displayed on ECAM• Characteristic speeds on PFD are erroneous• SRS mode guidance is affected if computed VLS is above V2 as inserted in the MCDU PERF

TAKE-OFF page.GW FAC computed, which is based on GW FM computed on ground, will be updated only onceairborne through a specific slow calculation using AOA information.

Note: 1. In flight, if the FM and FAC GW differ from a given threshold, a "CHECK GW" message istriggered on the MCDU.

2. Valpha prot, Vaalpha max, Vsw are not affected since based on aerodynamic data.

ERRONEOUS FUEL ON BOARD ENTRY

As long as the engines are not started, the FM GW is erroneous and above-mentionedconsequences apply. Once the engines are started, the fuel figures are updated and downstreamdata update accordingly.It should be noted however, that the FOB on ECAM is correct since it is provided from FQI data.

OPERATIONAL RECOMMENDATIONSIdent.: SI-040-00005726.0001001 / 26 MAR 08Criteria: SA�


ZFW entries should be cross-checked by both crew members to avoid entry error.If the "CHECK GW" amber warning is displayed on the MCDU, a significant discrepancy existsbetween the FM computed GW and the FAC computed GW.

The crew will compare the Load and Trim Sheet (LTS) figures with the FM GW and fuel used:• If an obvious entry error is detected, FM GW will be updated on the MCDU FUEL PRED page.• If FM and LTS GW are in accordance and appear to be correct, the FAC computed GW should be

suspected. (AOA sensor problem). Consequently, characteristic speeds on PFD are erroneous andshould be disregarded. Characteristic speeds should be extracted from QRH.

• If FM and LTS GW are in accordance but LTS GW is suspected, FAC and QRH characteristicspeeds should be compared (to validate FAC outputs) and the most appropriate applied.






ZFW entries should be cross-checked by both crew members to avoid entry error.If the "CHECK GW" amber warning is displayed on the MCDU, a discrepancy exists between the FMcomputed GW and the FAC computed GW.

The crew will compare the Load and Trim Sheet (LTS) figures with the FM GW and fuel used:• If an obvious entry error is detected, FM GW will be updated on the MCDU FUEL PRED page.• If FM and LTS GW are in accordance and appear to be correct, the FAC computed GW should be

suspected. (AOA sensor problem).• If FM and LTS GW are in accordance but LTS GW is suspected, characteristic speeds should be

extracted from QRH.


SUPPLEMENTARY INFORMATIONTCAS


TECHNICAL BACKGROUNDIdent.: SI-060-00005727.0001001 / 21 MAY 08Criteria: SA�Applicable to: ALL

GENERAL

A Traffic Alert and Collision Avoidance System (TCAS) provides the flight crew with trafficinformation and warnings of potential conflicts with vertical avoidance instructions. The TCAS canonly detect and indicate other traffic, that is equipped with a transponder.

The ND displays the traffic information, together with:• The bearing and range to the intruder• The intruder closure rate• The relative altitude difference.

If the TCAS considers the intruder to be a potential collision threat, it generates a visual and auralTraffic Advisory (TA). If it considers the intruder to be real collision threat, it generates a visual andaural Resolution Advisory (RA).

INTRUDER CLASSIFICATION

Intruder Display Type of col-lision threat

Aural warning Crew action

No threat traf-fic or others

-17 (w)

No threat - -

Proximate

-10 (w)

Consider asNo threat

- -

Traffic Ad-visory (TA)

-09 (a)

Potential threat "TRAFFIC" Establish visual contact.No evasive maneuver

Preventive, e.g."MONITOR V/S"

Do not alter your flight pathand keep VS out of red sector

Corrective, e.g. "CLIMB" Smoothly and firmly (0.25 g) fol-low VSI green sector within 5 s

Resolution Ad-visory (RA)

-06 (r)

Collision threat

Corrective, e.g."CLIMB NOW" or "IN-

CREASE CLIMB"

Smoothly and firmly (0.35 g) fol-low VSI green sector within 2.5 s




OPERATIONAL RECOMMENDATIONSIdent.: SI-060-00005731.0001001 / 25 JUN 08Criteria: SA�Applicable to: ALL

The flight crew should select• ABV in climb (+9 900 ft/-2 700 ft)• ALL in cruise (+2 700 ft/ -2 700 ft)• BELOW, if the cruise altitude is within 2 000 ftof FL 410, or in descent (+2 700 ft/ -9 900 ft)• THRT in heavy traffic terminal area• TA, in the case of:

‐ Engine failure‐ Flight with landing gear down‐ Known nearby traffic, that is in visual contact‐ Operations at specific airports, and during specific procedures that an operator identifies as

having a significant potential for not wanted and not appropriate RAs, e.g. closely spaced parallelrunways, converging runways.

Pilots should comply with the vertical speed limitations during the last 2 000 ft of a climb or descent.In particular, pilots should limit vertical speeds to 1 500 ft/min during the last 2 000 ft of a climb ordescent, especially when they are aware of traffic that is converging in altitude and intending to level off1 000 ft above or below the pilot's assigned altitude.

If a TA is generated:• The PF announces: "TCAS, I have controls".• The PF flies and announces the bearing and distance displayed on his ND.• The PNF looks outside to get visual contact.• No evasive maneuver should be initiated, only on the basis of a TA.

If a RA is generated:• The flight crew must always follow the TCAS RA orders in the correct direction, even:

‐ If the TCAS RA orders are in contradiction with the ATC instructions‐ At the maximum ceiling altitude with CLIMB, CLIMB or INCREASE CLIMB, INCREASE CLIMB

TCAS RA orders‐ If it results in crossing the altitude of the intruder.

CAUTION If a pilot does not follow a RA, he should be aware that the intruder may beTCAS equipped and may be maneuvering toward his aircraft in response to acoordinated RA. This could compromize safe separation.

• The PF disconnects the AP, and smoothly and firmly follows the Vertical Speed Indicator (VSI) greensector within 5 s, and requests that both FDs be disconnected.




Note: Both FDs must be disconnected once APs are disconnected:‐ To ensure autothrust speed mode‐ To avoid possible confusion between FD bar orders and, TCAS aural and VSI orders

• The PNF disconnects both FDs, but will not try to see intruders.• The PF will avoid excessive maneuvers, and keep the Vertical Speed outside the red area of the VSI

and within the green area. If necessary, the PF must use the full speed range between Valpha maxand Vmax.

• The PNF must notify ATC.• The flight crew should never maneuver in the opposite direction of the RA, because TCAS

maneuvers are coordinated.• In final approach, i.e. "CLIMB", "CLIMB NOW", "INCREASE CLIMB", the flight crew will initiate a go-

around.

When clear of conflict:• The flight crew must resume normal navigation, in accordance with ATC clearance, and using the

AP, as required.


SUPPLEMENTARY INFORMATIONUSE OF RADAR

ENV A318/A319/A320/A321 FLEET SI-070. P 1/10FCTM 09 JAN 09


The weather radar has two main functions:• Weather detection• Mapping.

Weather detection is the primary function. For weather detection, the radar detects precipitationdroplets. The strength of the echo is in proportion to the droplet size, composition and quantity (e.g.the reflection of water particles is five times greater than ice particles of the same size). Therefore, theweather radar does not detect weather that has small droplets (e.g. clouds or fog), or that does nothave droplets (e.g. clear air turbulence).Mapping is the secondary function. For mapping, the echo takes into account the difference betweenincoming and outgoing signals. Any significant difference in the signal is easily mapped (e.g.mountains or cities), but a small difference in the signal is not mapped (e.g. calm sea or even ground).




FUNCTIONSIdent.: SI-070-00005733.0001001 / 26 MAR 08Criteria: SA�

1 Applicable to: MSN 0002-2084, 2086-2089, 2091-2110, 2113-2129, 2131-2147, 2149-2152, 2154-2253, 2255-2256, 2258-2296, 2298-2305,2307-2308, 2311-2312, 2314, 2316-2333, 2335-2342, 2344, 2347, 2349-2353, 2355-2360, 2362-2395, 2397-2402, 2404-2423, 2425-2428,2430, 2432, 2435-2443, 2445-2469, 2471-2472, 2474-2475, 2477-2483, 2486-2489, 2491-2498, 2501-2505, 2507, 2512-2518, 2520-2524,2526-2528, 2530-2531, 2535-2540, 2542, 2544, 2547-2548, 2550, 2552-2553, 2556-2557, 2559, 2561-2565, 2568, 2570-2583, 2585-2589,2591-2593, 2595-2596, 2598-2602, 2604-2609, 2611-2621, 2623-2636, 2638, 2640-2647, 2650-2653, 2655, 2658, 2662, 2664-2665,2667, 2669-2671, 2674-2678, 2681-2682, 2686, 2690-2691, 2695, 2700, 2702-2703, 2705-2707, 2709-2710, 2712-2713, 2715, 2717, 2721,2724-2729, 2731-2732, 2735-2736, 2738-2742, 2744-2745, 2747-2748, 2750-2756, 2759, 2761-2767, 2769, 2773-2779, 2781-2783, 2785-2788,2790, 2794-2795, 2798-2800, 2802-2804, 2806-2809, 2811-2812, 2814-2815, 2817-2818, 2821, 2823, 2827, 2829-2832, 2836-2837, 2840,2843, 2845, 2848, 2850-2852, 2854, 2856-2858, 2860, 2864, 2866, 2868, 2870-2876, 2878, 2880, 2884, 2886-2889, 2892, 2894, 2897,2900-2901, 2903, 2906, 2908, 2910, 2912, 2914, 2916, 2918-2923, 2925, 2927-2928, 2930, 2933-2934, 2936, 2938-2941, 2943, 2945-2949,2951-2952, 2954, 2957, 2959, 2961-2962, 2964-2965, 2967, 2969-2972, 2977, 2982, 2984, 2988, 2992-2994, 2996-2999, 3001, 3003,3008-3010, 3012, 3014-3015, 3020, 3023-3025, 3028-3030, 3034, 3036-3041, 3044, 3048, 3051-3054, 3059, 3061-3063, 3067, 3070,3072-3073, 3075, 3078, 3081-3084, 3087-3092, 3095-3096, 3098-3102, 3104-3110, 3112, 3118-3120, 3122-3123, 3125-3127, 3130, 3133-3135,3137-3138, 3143-3152, 3155, 3157, 3160-3164, 3166, 3169, 3174, 3176-3177, 3179, 3181, 3183-3185, 3187, 3189-3191, 3203-3205, 3207-3209,3212, 3214-3216, 3219, 3221, 3224, 3228, 3230-3231, 3235-3239, 3244, 3246, 3252, 3254-3255, 3257-3258, 3263, 3267, 3269-3273, 3275,3280-3281, 3283, 3286-3288, 3290, 3292-3293, 3296-3298, 3300-3305, 3310-3312, 3314, 3316-3317, 3319-3322, 3324, 3326, 3332-3334,3336-3337, 3340-3342, 3344, 3347-3348, 3350-3351, 3354, 3356, 3359, 3361, 3363, 3367, 3371-3374, 3376-3377, 3379-3381, 3384,3389-3390, 3396, 3398-3402, 3405, 3409-3411, 3413, 3416-3417, 3419-3420, 3422, 3425-3426, 3429-3433, 3437-3438, 3441-3443, 3445,3451, 3455, 3460-3461, 3465-3466, 3468-3470, 3472, 3474-3475, 3479-3481, 3483, 3487-3488, 3492, 3495-3496, 3498-3499, 3503, 3506,3508-3509, 3511-3514, 3516-3517, 3524-3525, 3529-3531, 3535, 3537, 3539, 3542-3545, 3547, 3550-3551, 3553-3558, 3562, 3567, 3569,3571-3574, 3579, 3585, 3601-3603, 3606-3608, 3613, 3615, 3617, 3619-3622, 3627, 3631-3632, 3634-3635, 3637, 3640-3642, 3644, 3646,3649-3652, 3654, 3657, 3659, 3663, 3667-3668, 3671, 3673-3675, 3677, 3683-3684, 3686-3688, 3690, 3692-3693, 3697, 3699, 3702-3703,3706-3707, 3711, 3713, 3716-3721, 3724, 3726, 3731, 3734-3736, 3738, 3741-3744, 3746-3748, 3751-3752, 3754-3755, 3757, 3760, 3762-3763,3767, 3770-3772, 3774-3775, 3777-3781, 3783, 3786-3790, 3792-3795, 3799-3801, 3804-3805, 3807-3812, 3814, 3817, 3822-3826, 3843-3845,3854, 3871, 3888-3889, 3891, 3904-3905, 3937, 3797, 3819, 3834-3838, 3856, 3859, 3868, 3873-3874, 3876-3877, 3882, 3884, 3894, 3899,3901-3902, 3909, 3912-3913, 3916-3918, 3922-3923, 3926-3927, 3930, 3933, 3946-3948, 3952-3955, 3965, 3968, 3970

The flight crew uses the following controls to operate the radar:

TILT

"Tilt" is the angle between the antenna radar and the horizon, irrespective of the aircraft's pitch andbank angles. The antenna stabilizes by using IRS data.

To help avoid weather, it is important to effectively manage the tilt, taking into account the flightphase and the ND range.Usually, it is the appropriate tilt value that provides ground returns on the top of the ND.In case of overscanning, a cell may not be detected or may be underestimated, when the radarbeam scans the upper part of the cell. This occurs because, at high altitude, this cell may have iceparticles, and therefore the reflection of these particles is weak.If AUTO TILT function is installed, selecting AUTO ensures a proper tilt management along the flight.




GAIN

Gain control is mostly used in AUTO/CAL mode. The detection or evaluation of cells will always startin AUTO/CAL gain mode.However, the gain may be manually tuned to detect the strongest part of a cell displayed in red onthe ND. If the gain is slowly reduced, the red areas (level 3 return) will slowly become yellow areas(level 2 return), and the yellow areas will become green areas (level 1). The last part of the cell toturn yellow is the strongest area.The gain must then be reset to AUTO/CAL mode.

MODE

The operation modes are WX, WX+T, TURB, MAP.WX+T or TURB modes are used to locate the wet turbulence area. TURB mode detects wetturbulence within 40 nm, and is not affected by the gain. TURB mode should be used to isolateturbulence from precipitation.

GCS The Ground Clutter Suppression (GCS) operates in WX mode, and inhibits the ground echoes onthe ND.It is sometimes difficult to differentiate between weather and ground returns. A change in tilt rapidlychanges the shape and color of ground returns and eventually makes them disappear. This is notthe case for weather.

RCT The React (RCT) function is used temporarily to help detect weather or buildups beyond of theweather already detected.

PWS

Refer to SI-010 WINDSHEAR on adverse weather.




FUNCTIONSIdent.: SI-070-00005733.0002001 / 26 MAR 08Criteria: 34-1334, 34-1348, 34-1416, P7929, SA�

2 Applicable to: MSN 2085, 2090, 2112, 2130, 2148, 2153, 2254, 2257, 2297, 2306, 2309-2310, 2313, 2315, 2334, 2343, 2345-2346, 2348,2354, 2361, 2396, 2403, 2424, 2429, 2431, 2433-2434, 2444, 2470, 2473, 2476, 2484-2485, 2490, 2499, 2506, 2508-2511, 2519, 2525,2529, 2532-2534, 2541, 2543, 2545-2546, 2549, 2551, 2554-2555, 2558, 2560, 2566-2567, 2569, 2584, 2590, 2594, 2597, 2603, 2610,2622, 2637, 2639, 2648-2649, 2654, 2656-2657, 2659-2661, 2663, 2666, 2668, 2672-2673, 2679-2680, 2683-2685, 2687-2689, 2692-2694,2696-2699, 2701, 2704, 2708, 2711, 2714, 2716, 2718-2720, 2723, 2730, 2733-2734, 2737, 2743, 2746, 2749, 2757-2758, 2760, 2768,2770-2772, 2780, 2784, 2789, 2791-2793, 2796-2797, 2805, 2810, 2813, 2816, 2819-2820, 2822, 2824-2826, 2828, 2833-2835, 2838-2839,2841-2842, 2844, 2846-2847, 2849, 2853, 2855, 2859, 2861-2863, 2865, 2867, 2869, 2877, 2879, 2881-2883, 2885, 2890-2891, 2893,2895-2896, 2898-2899, 2902, 2904-2905, 2907, 2909, 2911, 2913, 2915, 2917, 2924, 2926, 2929, 2931-2932, 2935, 2937, 2942, 2944,2950, 2953, 2955-2956, 2958, 2960, 2963, 2966, 2968, 2973-2976, 2978-2981, 2983, 2985-2987, 2989-2991, 2995, 3000, 3002, 3004-3007,3011, 3013, 3016-3019, 3021-3022, 3026-3027, 3031-3033, 3035, 3042-3043, 3045-3047, 3049-3050, 3055-3058, 3060, 3064-3066,3068-3069, 3071, 3074, 3076-3077, 3079-3080, 3085-3086, 3093-3094, 3097, 3103, 3111, 3113-3117, 3121, 3124, 3128-3129, 3131-3132, 3136,3139-3142, 3153-3154, 3156, 3158-3159, 3165, 3167-3168, 3170-3173, 3175, 3178, 3180, 3182, 3186, 3188, 3192-3202, 3206, 3210-3211,3213, 3217-3218, 3220, 3222-3223, 3225-3227, 3229, 3232-3234, 3240-3243, 3245, 3247-3251, 3253, 3256, 3259-3262, 3264-3266, 3268,3274, 3276-3279, 3282, 3284-3285, 3289, 3291, 3294-3295, 3299, 3306-3309, 3313, 3315, 3318, 3323, 3325, 3327-3331, 3335, 3338-3339,3343, 3345-3346, 3349, 3352-3353, 3355, 3357-3358, 3360, 3362, 3364-3366, 3368-3370, 3375, 3378, 3382-3383, 3385-3388, 3391-3395,3397, 3403-3404, 3406-3408, 3412, 3414-3415, 3418, 3421, 3423-3424, 3427-3428, 3434-3436, 3439-3440, 3444, 3446-3450, 3452-3454,3456-3459, 3462-3464, 3467, 3471, 3473, 3476-3478, 3482, 3484-3486, 3489-3491, 3493-3494, 3497, 3500-3502, 3504-3505, 3507, 3510,3515, 3518-3523, 3526-3528, 3532-3534, 3536, 3538, 3540-3541, 3546, 3548-3549, 3552, 3559-3561, 3563-3566, 3568, 3570, 3575-3578,3580-3584, 3586-3600, 3604-3605, 3609-3612, 3614, 3616, 3618, 3623-3626, 3628-3630, 3633, 3636, 3643, 3645, 3647-3648, 3653,3655-3656, 3658, 3660-3662, 3664-3666, 3669-3670, 3672, 3676, 3678-3682, 3685, 3689, 3691, 3694-3696, 3700-3701, 3704-3705,3708-3710, 3712, 3714-3715, 3722-3723, 3725, 3727-3730, 3732-3733, 3737, 3739-3740, 3745, 3749-3750, 3753, 3756, 3761, 3764-3766,3768-3769, 3773, 3776, 3782, 3784-3785, 3791, 3796, 3798, 3802-3803, 3806, 3813, 3815-3816, 3820-3821, 3839-3841, 3860-3867, 3875,3878-3881, 3883, 3890, 3892-3893, 3903, 2801, 3638-3639, 3698, 3758-3759, 3818, 3827-3833, 3846-3853, 3855, 3857-3858, 3869, 3872,3885-3887, 3895-3898, 3900, 3906-3908, 3910-3911, 3915, 3919-3921, 3924-3925, 3928, 3931-3932, 3934-3936, 3938-3945, 3949-3951,3956-3964, 3966-3967, 3969, 3971-3996

The flight crew uses the following controls to operate the radar:

TILT

"Tilt" is the angle between the antenna radar and the horizon, irrespective of the aircraft's pitch andbank angles. The antenna stabilizes by using IRS data.

To help avoid weather, it is important to effectively manage the tilt, taking into account the flightphase and the ND range.Usually, it is the appropriate tilt value that provides ground returns on the top of the ND.In case of overscanning, a cell may not be detected or may be underestimated, when the radarbeam scans the upper part of the cell. This occurs because, at high altitude, this cell may have iceparticles, and therefore the reflection of these particles is weak.Selecting AUTO ensures a proper tilt management along the flight.




Note: In cruise, MULTISCAN function provides a large view of the weather ahead, ie display ofweather cells located on and below aircraft path. Before envisaging a route change in frontof an ambiguous or unexpected weather display, the crew should confirm the potentialconflicts with aircraft path, using temporarily manual tilt.

GAIN

Manual gain selection (+8) must be used when MULTISCAN selector is set to AUTO.However, the gain may be tuned to detect the strongest part of a cell displayed in red on the ND.If the gain is slowly reduced, the red areas (level 3 return) will slowly become yellow areas (level 2return), and the yellow areas will become green areas (level 1). The last part of the cell to turn yellowis the strongest area.The gain must then be reset to +8.

MODE

The operation modes are WX, WX+T, TURB, MAP.WX+T or TURB modes are used to locate the wet turbulence area. TURB mode detects wetturbulence within 40 nm, and is not affected by the gain. TURB mode should be used to isolateturbulence from precipitation.

GCS The Ground Clutter Suppression (GCS) operates in WX mode, and inhibits the ground echoes onthe ND.It is sometimes difficult to differentiate between weather and ground returns. A change in tilt rapidlychanges the shape and color of ground returns and eventually makes them disappear. This is notthe case for weather.

RCT The React (RCT) function is used temporarily to help detect weather or buildups beyond of theweather already detected.

PWS

Refer to SI-010 WINDSHEAR on adverse weather.




OPERATIONAL RECOMMENDATIONS FOR WEATHER DETECTIONIdent.: SI-070-00005734.0001001 / 26 MAR 08Criteria: P9355, SA�

3 Applicable to: MSN 0002-0763, 0765-1772, 1774-1877, 1879-1952, 1954-1955, 1957-1966, 1968-2054, 2056-2063, 2065-2075, 2077-2084,2086-2089, 2092-2096, 2098-2110, 2113-2129, 2131-2147, 2149-2152, 2154-2253, 2255-2256, 2258-2287, 2289-2296, 2298-2305, 2307,2311-2312, 2314, 2316-2325, 2327-2329, 2331-2333, 2335-2336, 2338-2340, 2344, 2347, 2349-2353, 2356-2360, 2362-2374, 2376-2378,2380-2395, 2397-2402, 2404-2417, 2420, 2422-2423, 2425-2428, 2430, 2432, 2435-2437, 2440, 2442-2443, 2445-2468, 2471-2472, 2474-2475,2477-2483, 2486-2489, 2491-2498, 2502-2505, 2507, 2512-2518, 2520-2524, 2526-2528, 2530-2531, 2535-2539, 2542, 2544, 2547-2548,2550, 2552-2553, 2556-2557, 2559, 2561-2565, 2568, 2570-2583, 2585-2589, 2591-2593, 2595, 2598-2602, 2604-2608, 2611-2615,2617-2621, 2624-2625, 2627-2636, 2638, 2640-2647, 2650-2652, 2655, 2658, 2664-2665, 2667, 2669-2671, 2675-2677, 2681-2682, 2686,2690-2691, 2695, 2700, 2702-2703, 2705-2707, 2709-2710, 2712-2713, 2715, 2717, 2721, 2724-2725, 2727-2729, 2731-2732, 2735,2738-2739, 2741-2742, 2744-2745, 2747, 2750-2755, 2759, 2763-2767, 2769, 2774-2775, 2777, 2779, 2781-2783, 2786-2788, 2790, 2795,2802-2804, 2806, 2808-2809, 2812, 2814-2815, 2817-2818, 2821, 2827, 2829, 2831-2832, 2836-2837, 2840, 2845, 2848, 2850, 2852, 2854,2856-2858, 2860, 2864, 2866, 2871-2874, 2876, 2880, 2884, 2886-2888, 2892, 2894, 2900-2901, 2906, 2908, 2910, 2914, 2916, 2918-2919,2921-2923, 2927, 2930, 2933, 2936, 2938-2940, 2943, 2945-2946, 2948-2949, 2951-2952, 2959, 2961, 2964, 2967, 2969-2972, 2977, 2982,2992, 2994, 2998, 3001, 3003, 3008-3009, 3012, 3014, 3020, 3023, 3025, 3028-3030, 3034, 3036, 3038-3039, 3041, 3044, 3048, 3051,3053, 3059, 3061-3062, 3067, 3072-3073, 3075, 3082, 3084, 3088-3092, 3096, 3098-3100, 3104-3106, 3110, 3112, 3118-3120, 3122-3123,3125, 3133-3134, 3137, 3144, 3147-3150, 3160, 3162-3164, 3176, 3183-3184, 3189-3190, 3214, 3216, 3219, 3224, 3228, 3231, 3236, 3238,3244, 3258, 3263, 3269-3270, 3272, 3275, 3280, 3286-3287, 3292, 3296-3297, 3302, 3304, 3311-3312, 3316, 3319, 3322, 3332-3333, 3342,3348, 3356, 3363, 3371-3372, 3374, 3379, 3381, 3389-3390, 3399, 3401-3402, 3411, 3413, 3416, 3419-3420, 3426, 3431-3432, 3437-3438,3441-3442, 3451, 3466, 3469-3470, 3474, 3479, 3483, 3488, 3495-3496, 3508-3509, 3513-3514, 3517, 3524, 3530, 3535, 3537, 3542-3544,3547, 3554-3556, 3569, 3571-3572, 3585, 3602, 3606, 3608, 3615, 3617, 3621-3622, 3632, 3634-3635, 3637, 3641-3642, 3657, 3659, 3663,3667-3668, 3671, 3673-3675, 3683, 3688, 3690, 3702, 3707, 3717, 3720, 3724, 3734-3735, 3738, 3742-3743, 3746, 3748, 3751, 3754, 3757,3760, 3763, 3770, 3772, 3774, 3777, 3779-3780, 3783, 3788, 3790, 3795, 3799-3801, 3805, 3808, 3810-3812, 3814, 3824-3826, 3843-3845,3854, 3871, 3888-3889, 3891, 3836, 3856, 3859, 3868, 3873, 3876, 3884, 3901, 3905, 3909, 3913, 3917, 3922, 3930, 3933, 3946, 3953




Note: It is difficult to differentiate between weather returns and ground returns: A change in TILTcauses the shape and color of ground returns to change rapidly. These ground returnseventually disappear. This is not the case for weather returns.

Ident.: SI-070-00005734.0002001 / 07 JAN 09Criteria: 34-1316, 34-1395, P7929, P8233, P9355, SA�

4 Applicable to: MSN 0764, 1773, 1878, 1953, 1956, 1967, 2055, 2064, 2076, 2091, 2097, 2288, 2308, 2326, 2330, 2337, 2341-2342, 2355,2375, 2379, 2418-2419, 2421, 2438-2439, 2441, 2469, 2501, 2540, 2596, 2609, 2616, 2623, 2626, 2653, 2662, 2674, 2678, 2726, 2736, 2740,2748, 2756, 2761-2762, 2773, 2776, 2778, 2785, 2794, 2798-2800, 2807, 2811, 2823, 2830, 2843, 2851, 2868, 2870, 2875, 2878, 2889,2897, 2903, 2912, 2920, 2925, 2928, 2934, 2941, 2947, 2954, 2957, 2962, 2965, 2984, 2988, 2993, 2996-2997, 2999, 3010, 3015, 3024,3037, 3040, 3052, 3054, 3063, 3070, 3078, 3081, 3083, 3087, 3095, 3101-3102, 3107-3109, 3126-3127, 3130, 3135, 3138, 3143, 3145-3146,3151-3152, 3155, 3157, 3161, 3166, 3169, 3174, 3177, 3179, 3181, 3185, 3187, 3191, 3203-3205, 3207-3209, 3212, 3215, 3221, 3230, 3235,3237, 3239, 3246, 3252, 3254-3255, 3257, 3267, 3271, 3273, 3281, 3283, 3288, 3290, 3293, 3298, 3300-3301, 3303, 3305, 3310, 3314, 3317,3320-3321, 3324, 3326, 3334, 3336-3337, 3340-3341, 3344, 3347, 3350-3351, 3354, 3359, 3361, 3367, 3373, 3376-3377, 3380, 3384, 3396,3398, 3400, 3405, 3409-3410, 3417, 3422, 3425, 3429-3430, 3433, 3443, 3445, 3455, 3460-3461, 3465, 3468, 3472, 3475, 3480-3481, 3487,3492, 3498-3499, 3503, 3506, 3511-3512, 3516, 3525, 3529, 3531, 3539, 3545, 3550-3551, 3553, 3557-3558, 3562, 3567, 3573-3574, 3579,3601, 3603, 3607, 3613, 3619-3620, 3627, 3631, 3640, 3644, 3646, 3649-3652, 3654, 3677, 3684, 3686-3687, 3692-3693, 3697, 3699, 3703,3706, 3711, 3713, 3716, 3718-3719, 3721, 3726, 3731, 3736, 3741, 3744, 3747, 3752, 3755, 3762, 3767, 3771, 3778, 3781, 3786-3787, 3789,3792-3794, 3804, 3807, 3809, 3817, 3822-3823, 3874, 3904, 3937, 3775, 3797, 3819, 3834-3835, 3837-3838, 3877, 3882, 3894, 3899, 3902,3912, 3916, 3918, 3923, 3926-3927, 3947-3948, 3952, 3954-3955, 3965, 3968, 3970, 3984

FLIGHT PHASE DETECTION AND MONITORING PROCEDURES COMMENTSTAXI Clear on parking area, set ND to lowest range, TILT DOWN then UP;

Check appearance/disappearance of ground returns.Reselect AUTO after scanning.

Tilt antenna checka(away from people)

TAKE OFF If weather is suspected, SLOWLY SCAN up to +15 °C, then reselect AUTO. Scanning alongdeparture path

IN FLIGHT Use TURB to ISOLATE Turbulence – GAIN to AUTO Poor ground re-turn over calm

sea / even ground

Note: Weather and ground returns are difficult to differentiate: a change in TILT rapidly changes theshape and color of ground returns and eventually cause them to disappear which is not thecase for weather.




Ident.: SI-070-00005734.0003001 / 26 MAR 08Criteria: 34-1334, 34-1348, 34-1416, P7929, SA�

5 Applicable to: MSN 2085, 2090, 2112, 2130, 2148, 2153, 2254, 2257, 2297, 2306, 2309-2310, 2313, 2315, 2334, 2343, 2345-2346, 2348,2354, 2361, 2396, 2403, 2424, 2429, 2431, 2433-2434, 2444, 2470, 2473, 2476, 2484-2485, 2490, 2499, 2506, 2508-2511, 2519, 2525,2529, 2532-2534, 2541, 2543, 2545-2546, 2549, 2551, 2554-2555, 2558, 2560, 2566-2567, 2569, 2584, 2590, 2594, 2597, 2603, 2610,2622, 2637, 2639, 2648-2649, 2654, 2656-2657, 2659-2661, 2663, 2666, 2668, 2672-2673, 2679-2680, 2683-2685, 2687-2689, 2692-2694,2696-2699, 2701, 2704, 2708, 2711, 2714, 2716, 2718-2720, 2723, 2730, 2733-2734, 2737, 2743, 2746, 2749, 2757-2758, 2760, 2768,2770-2772, 2780, 2784, 2789, 2791-2793, 2796-2797, 2805, 2810, 2813, 2816, 2819-2820, 2822, 2824-2826, 2828, 2833-2835, 2838-2839,2841-2842, 2844, 2846-2847, 2849, 2853, 2855, 2859, 2861-2863, 2865, 2867, 2869, 2877, 2879, 2881-2883, 2885, 2890-2891, 2893,2895-2896, 2898-2899, 2902, 2904-2905, 2907, 2909, 2911, 2913, 2915, 2917, 2924, 2926, 2929, 2931-2932, 2935, 2937, 2942, 2944,2950, 2953, 2955-2956, 2958, 2960, 2963, 2966, 2968, 2973-2976, 2978-2981, 2983, 2985-2987, 2989-2991, 2995, 3000, 3002, 3004-3007,3011, 3013, 3016-3019, 3021-3022, 3026-3027, 3031-3033, 3035, 3042-3043, 3045-3047, 3049-3050, 3055-3058, 3060, 3064-3066,3068-3069, 3071, 3074, 3076-3077, 3079-3080, 3085-3086, 3093-3094, 3097, 3103, 3111, 3113-3117, 3121, 3124, 3128-3129, 3131-3132, 3136,3139-3142, 3153-3154, 3156, 3158-3159, 3165, 3167-3168, 3170-3173, 3175, 3178, 3180, 3182, 3186, 3188, 3192-3202, 3206, 3210-3211,3213, 3217-3218, 3220, 3222-3223, 3225-3227, 3229, 3232-3234, 3240-3243, 3245, 3247-3251, 3253, 3256, 3259-3262, 3264-3266, 3268,3274, 3276-3279, 3282, 3284-3285, 3289, 3291, 3294-3295, 3299, 3306-3309, 3313, 3315, 3318, 3323, 3325, 3327-3331, 3335, 3338-3339,3343, 3345-3346, 3349, 3352-3353, 3355, 3357-3358, 3360, 3362, 3364-3366, 3368-3370, 3375, 3378, 3382-3383, 3385-3388, 3391-3395,3397, 3403-3404, 3406-3408, 3412, 3414-3415, 3418, 3421, 3423-3424, 3427-3428, 3434-3436, 3439-3440, 3444, 3446-3450, 3452-3454,3456-3459, 3462-3464, 3467, 3471, 3473, 3476-3478, 3482, 3484-3486, 3489-3491, 3493-3494, 3497, 3500-3502, 3504-3505, 3507, 3510,3515, 3518-3523, 3526-3528, 3532-3534, 3536, 3538, 3540-3541, 3546, 3548-3549, 3552, 3559-3561, 3563-3566, 3568, 3570, 3575-3578,3580-3584, 3586-3600, 3604-3605, 3609-3612, 3614, 3616, 3618, 3623-3626, 3628-3630, 3633, 3636, 3643, 3645, 3647-3648, 3653,3655-3656, 3658, 3660-3662, 3664-3666, 3669-3670, 3672, 3676, 3678-3682, 3685, 3689, 3691, 3694-3696, 3700-3701, 3704-3705,3708-3710, 3712, 3714-3715, 3722-3723, 3725, 3727-3730, 3732-3733, 3737, 3739-3740, 3745, 3749-3750, 3753, 3756, 3761, 3764-3766,3768-3769, 3773, 3776, 3782, 3784-3785, 3791, 3796, 3798, 3802-3803, 3806, 3813, 3815-3816, 3820-3821, 3839-3841, 3860-3867, 3875,3878-3881, 3883, 3890, 3892-3893, 3903, 2801, 3638-3639, 3698, 3758-3759, 3818, 3827-3833, 3846-3853, 3855, 3857-3858, 3869, 3872,3885-3887, 3895-3898, 3900, 3906-3908, 3910-3911, 3915, 3919-3921, 3924-3925, 3928, 3931-3932, 3934-3936, 3938-3945, 3949-3951,3956-3964, 3966-3967, 3969, 3971-3983, 3989-3996

FLIGHT PHASE DETECTION AND MONITORING PROCEDURES COMMENTSTAXI Clear on parking area, set ND to lowest range, TILT DOWN then UP;

Check appearance/disappearance of ground returns.Reselect AUTO after scanning.

Tilt antenna check(away from people)

TAKE OFF If weather is suspected, SLOWLY SCAN up to +15 °C, then reselect AUTO. Scanning alongdeparture path

IN FLIGHT Use TURB to ISOLATE Turbulence Poor ground re-turn over calm

sea / even ground

Note: 1. GAIN must be manually set to +8, when MULTISCAN selector is set to AUTO.2. MULTISCAN AUTO mode provides an efficient ground clutter rejection. During operations

in good or non-significant weather, no weather pattern will be displayed on ND's. In suchsituation, the crew ascertains correct radar operation, using temporarily MANUAL TILT.

3. The crew monitors weather radar display in AUTO, and confirms any ambiguous orunexpected weather display using manual tilt according to standard techniques.




OTHER OPERATIONAL RECOMMENDATIONSIdent.: SI-070-00005736.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

WEATHER AVOIDANCE

• When weather is suspected, scan for it by varying the radar tilt. If AUTOTILT or MULTISCANfunction is available, reselect AUTO after scanning.

• Do not underestimate a thunderstorm, even if echo is weak (only wet parts are detected)• Avoid all red + magenta cells by at least 20 nm• Deviate upwind instead of downwind (less probability of turbulence or hail)• Do not attempt to fly below a storm even visual (turbulence, shear, altimetry)• Use TURB detection to isolate turbulence from precipitation• There may be severe turbulence, up to 5 000 ft above a cell• Storms with tops above 35 000 ft are hazardous• Frequent and vivid lightning indicates a high probability of severe turbulence.

WEATHER PENETRATION

In the case of storm penetration, the flight crew must take full advantage of the radar. For flight crewguidelines, in the case of turbulence, Refer to SI-010 TURBULENCE.

MAPPING

TILT and GAIN have to be adjusted harmoniously, because the ground returns vary greatly with theangle of the radar beam which illuminates them.• Use MAP to detect PROMINENT TERRAIN (mountain, city, and coastline)• Adjust TILT and GAIN - Mapping coverage varies with tilt and aircraft altitude.

TILT ANGLE AREA SCANNED AT FL 3303 ° DN 72 nm to 190 nm0 ° DN 47 nm to 190 nm7 ° DN 36 nm to 70 nm10 ° DN 26 nm to 41 nm

However, flight crew should NOT USE the weather radar as a terrain avoidance system.

PREVENTINGIDENTIFIED RISKS


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ENV A318/A319/A320/A321 FLEET PIR-PLP-TOC. P 1/2FCTM 09 JAN 09

PIR-PLP. PRELIMINARY PAGESTABLE OF CONTENTS........................................................................................................................................... 1/2

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PIR-010. PREVENTING IDENTIFIED RISKSINTRODUCTION...................................................................................................................................................... 1/4NORMAL OPERATIONS..........................................................................................................................................2/4SYSTEM OPERATIONS / FAILURES...................................................................................................................... 3/4

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PREVENTING IDENTIFIED RISKSPREVENTING IDENTIFIED RISKS

ENV A318/A319/A320/A321 FLEET PIR-010. P 1/4FCTM 08 JUL 08

INTRODUCTIONIdent.: PIR-010-00005742.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

The aim of this chapter is to highlight some of the risks encountered by flight crews, in order toimprove:‐ Flight crewmembers' awareness of these risks‐ Risk management.

These risks are categorized according to either:‐ Flight phases, for the risks related to normal operations, or‐ ATA chapters, for the risks more specifically related to the flight crews' interaction with systems, or to

system failures.

For each risk, the following table provides:‐ The flight phase or ATA chapter related to the risk‐ A description of the risk‐ A description of the consequences, if the flight crew does not correctly manage the risk‐ The type of consequences (who or what is affected by the risk), illustrated by one of these 6

symbols:• "CONTROL": Aircraft handling or control may be affected• "NAV": Navigation may be affected• "GROUND PERSONNEL": Possibility of injury to ground personnel• "FLIGHT": it may not be possible to complete the flight, there may be a risk of diversion.• "AIRCRAFT": Possibility of damage to the aircraft• "PAX": Possibility of injury to passengers.

‐ A reference to the FCTM chapter, section, and/or paragraph, where the related explanations andrecommendations (for prevention and/or recovery) are located.

RISK SYMBOLS

CONTROL NAV GROUNDPERSONNEL

FLIGHT AIRCRAFT PAX




NORMAL OPERATIONSIdent.: PIR-010-00005743.0001001 / 21 APR 08Criteria: SA�Applicable to: ALL

Flight Phase Risk Consequences Refer toFCTMPREP During takeoff briefing,

the flight crew does notcheck that the FMS SID(including the constraints)is correct.

Erroneous trajectory Refer to NO-020 COCK-PIT PREPARATION

TAKEOFF The flight crew calls out“THRUST SET” beforereaching N1 value

Engine check not valid Refer to NO-050 TakeoffRoll

CLIMB /DE-SC

The flight crew uses theV/S knob without settinga target

Climb or descent does not stop

DESC In managed descent, theflight crew uses the speedbrakes, in an attempt todescend below the com-puted profile

Unless the aircraft is above the com-puted profile, the autothrust increas-es thrust to remain on the computedprofile. The expected increased rateof descent will not be reached. In ad-dition, fuel consumption will increase

Refer to NO-080 GUID-ANCE AND MONITOR-ING

DESC The flight crew does notset the TERR ON NDswitch to ON

Reduced situational awareness Refer to NO-080 PREF-ACE

APPR The flight crew activatesapproach phase withoutcrosschecking with eachother

The other flight crewmember mayperceive the speed change as undue,and may react to it

Refer to NO-010 COM-MUNICATION

APPR The flight crew clears theF-PLN using the DIR TOor DIR TO RAD IN func-tions, although the aircraftis in radar vectoring

NAV mode is armed. If this mode set-ting is not relevant, it may lead to anerroneous trajectory

Refer to NO-100 INITIALAPPROACH and Refer toNO-100 INTERMEDIATEAPPROACH

APPR The flight crew does notsufficiently monitor rawdata

Any erroneous computation leads toan erroneous trajectory

Refer to NO-100 FINALAPPROACHRefer to NO-120 FINALAPPROACH





Continued from previous pageFlight Phase Risk Consequences Refer toFCTMILS APPR Glide slope intercep-

tion from above: G/S notrearmed

The aircraft descends through theglide slope axis, without intercepting it

Refer to NO-110 FINALAPPROACH

NPA APPR When the aircraft reachesthe minimum altitude, theflight crew sets the bird toON and the AP to OFF,but does not set the FDsto OFF.

The FDs orders may not be correctbelow the minima.

Refer to OP-030 AUTOPI-LOT/FLIGHT DIRECTORRefer to NO-120 REACH-ING THE MINIMA

SYSTEM OPERATIONS / FAILURESIdent.: PIR-010-00005745.0001001 / 26 MAR 08Criteria: SA�Applicable to: ALL

ATA Risk Consequences Csqce type Refer to FCTM22 The flight crew uses the in-

stinctive disconnect push-button on the thrust leversto disconnect autothrust,without reducing the Throt-tle Lever Angle (TLA)

Immediate and undue speed increase Refer to OP-030 AU-TOTHRUST (A/THR)

22 Alpha floor/TOGA LOCK,with no disconnection ofautothrust

TOGA thrust is maintained, with an un-due speed increase, and may lead tooverspeed

Refer to OP-030 AU-TOTHRUST (A/THR)

22 The flight crew does notuse the correct knob tochange heading or speed

Trajectory not correct

22 The flight crew does notsequence the F/PLN

Erroneous computation (e.g. time, fuel)and trajectory

Refer to NO-120 INTER-MEDIATE APPROACH

At takeoff:When flaps/slats are locked, if the flightcrew does not select the current speed,the aircraft continues to accelerate andpossibly exceeds MAX Speed

27 The flight crew does notselect the speed after slator flap failure

In approach:When flaps/slats are locked, if the flightcrew does not select the current speed,the aircraft continues to deceleratedown to a speed that is not consistentwith the real aircraft configuration

Refer to AO-027ABNORMAL FLAPS/SLATS CONFIGURA-TION





Continued from previous pageATA Risk Consequences Csqce type Refer to FCTM27/32 In the case of flight with

slats/flaps extended orlanding gear extended, theflight crew takes into ac-count the FMS predictions

Erroneous computation (i.e. time, fuel),because the FMS does not take into ac-count the abnormal configuration

Refer to AO-027ABNORMAL FLAPS/SLATS CONFIGURA-TION

28 The flight crew does notcheck fuel before fuelcrossfeed

Fuel loss Refer to AO-028 FUELLEAK

34 Error in the use of RMP Loss of transmission to ATC due to anerroneous manipulation (particularlywhen SEL is on)

34 The flight crew performsthe TCAS procedure, butdoes not set the FDs toOFF

The autothrust mode remains in THRCLB or THR DES, which are not the ap-propriate modes. This may lead to flightcontrol protection activation

Refer to SI-060 OPERA-TIONAL RECOMMEN-DATIONS

34 The flight crew selectsADR to OFF using theADIRS rotary selector, in-stead of the ADR pushbut-ton

Irreversible loss of redundancy (the as-sociated IR is lost, and cannot be recov-ered until the end of the flight)

Refer to AO-034 ADR/IRS FAULT

70 In the case of an enginefailure after takeoff, theflight crew does not sta-bilize the aircraft on theflight path before perform-ing ECAM actions

Performing the ECAM actions before theaircraft is stabilized on the flight path,reduces efficiency due to the PF’s highworkload, and may lead to a trajectoryerror

Refer to AO-020 EN-GINE FAILURE AFTERV1

70 In the case of an enginefailure in cruise, the flightcrew presses the EO CLRkey on the MCDU

Pressing the EO CLR key on the MCDUis an irreversible action that leads to theloss of single engine computation (dis-crepancy between the computation andreal aircraft status)

Refer to AO-020 EN-GINE FAILURE DUR-ING CRUISE

80 For EMERGENCY DE-SCENT, the flight crewturns but does not pullthe knobs, or does both,but not in the correct se-quence, with no FMAcrosscheck

The flight crew does not detect that thedescent is not engaged. Delayed de-scent leads to limited oxygen for pas-sengers

Refer to OP-030 AU-TOPILOT/FLIGHT DI-RECTOR

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