Airbus A320-200 · A320-200 MSN. TBA Page 7 of 12 MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER...

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SPECIFICATION SUMMARY Airbus A320-200 Rev.: No. 3 Date: 26-SEP-2018 Confidentiality and Disclaimer: All rights reserved. This document is the sole property of t h e S e l l e r . This document has been drafted and distributed for information purposes only. This document may not be reproduced or (re) distributed or otherwise utilized in part or whole without the express prior written permission of t h e S e l l e r . While the information presented in this document is given in good faith based upon the most current information available to t h e S e l l e r , changes or modifications with respect to the subject aircraft and the associated records and documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regarded as establishing any obligation on the part of t h e S e l l e r or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated records and documentation.

Transcript of Airbus A320-200 · A320-200 MSN. TBA Page 7 of 12 MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER...

Page 1: Airbus A320-200 · A320-200 MSN. TBA Page 7 of 12 MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY ATA 22 - Automatic Flight Controls FMGC Thales Avionics C13043AA06

SPECIFICATION SUMMARY

Airbus A320-200

Rev.: No. 3 Date: 26-SEP-2018

Confidentiality and Disclaimer:

All rights reserved. This document is the sole property of t h e S e l l e r . This document has been drafted and distributed for information purposes only. This document may not be reproduced or (re) distributed or otherwise utilized in part or whole without the express prior written permission of t h e S e l l e r . While the information presented in this document is given in good faith based upon the most current information available to t h e S e l l e r , changes or modifications with respect to the subject aircraft and the associated records and documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regarded as establishing any obligation on the part of t h e S e l l e r or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated records and documentation.

Page 2: Airbus A320-200 · A320-200 MSN. TBA Page 7 of 12 MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY ATA 22 - Automatic Flight Controls FMGC Thales Avionics C13043AA06

A320-200 MSN. TBA Page 2 of 12

WEIGHTS, OPERATIONAL Metric US Customary

Maximum Taxi Weight (MTW) 77`400 (Kg) 170`637 (Lbs)

Maximum Take Off Weight (MTOW) 77`000 (Kg) 169`755 (Lbs)

Maximum Landing Weight (MLW) 66`000 (Kg) 145`505 (Lbs)

Maximum Zero Fuel Weight (MZFW) 62`500 (Kg) 137`788 (Lbs)

Minimum Weight (MW) 37`230 (kg) 82`079(Lbs)

Operator`s Empty Weight (OEW) 41`484 (kg) 91`456 (Lbs)

Maximum Structural Payload * 20`200 (kg) 44`533 (Lbs)

Fuel Capacity (FC) 23`859 (Liters) 6`303 (USG) * ESTIMATED

AIRCRAFT IDENTIFICATION

Aircraft Model A320-214

Manufacturer Serial Number TBA

Manufacture Date SEP – 2007

Aircraft Registration TBA

Engines Model CFM56-5B4/P

APU Model GTCP-131-9[A]

DELIVERY SUMMARY

Certification: EASA

Airframe: Fresh from C, 6Y & 12Y-check

Engines: As IS, installed on the aircraft & within the limits of the manufacturer;

MPA Run and BSI to be performed

APU: Serviceable

Landing Gears: As IS, Serviceable & Airworthy

Components: Serviceable & Airworthy

Painting: Painted in White

Interior Conf.: Clean, Normal wear & tear

Airworthiness Directives:

In compliance on the delivery date

Documents & Records:

Up to date, in English

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A320-200 MSN. TBA Page 3 of 12

AIRFRAME STATUS Total Airframe Hours 36`803

Total Cycles 16`203

Status Date 12-AUG-2018 NOTE: AVERAGE UTILISATION 280 FH & 120 FC PER MONTHS

MAINTENANCE STATUS C - Check interval 7`500 FH / 5`000 FC / 24 MO

6Y - Check interval 72 MO

12Y - Check interval 144 MO

Last C - Check 27-NOV-2016 at 32`784 FH & 13`890 FC

Last 6Y – Check 06-MAY-2013 at 21`760FH & 8`530 FC

Last 12Y – Check N/A

Next C – Check 26-NOV-2018

Next 6Y – Check 05-MAY-2019

Next 12Y - Check 11-SEP-2019

ENGINE / APU DETAILS Engine 1 Engine 2 APU

Manufacturer CFMI CFMI Honeywell

Model CFM56-5B4/P CFM56-5B4/P GTCP-131-9[A]

Thrust Rate 27`000 Lbs 27`000 Lbs

ENGINE / APU STATUS Engine 1 Engine 2 APU

Serial Number TBA TBA TBA

Total Time Since New 42`798 35`429 13`725

Total Cycles Since New 16`693 15`674 23`942

Last Shop Visit In Shop 05-SEP-2013 05-MAR-2014

Hours Since Last Shop Visit 21`836 13`651 6`194

Cycles Since Last Shop Visit 8`483 7`131 9`010

Last Overhaul NONE NONE NONE

Hours Since Last Overhaul N/A N/A N/A

Cycles Since Last Overhaul N/A N/A N/A

First LLP Limiter 3`307 4`326 6`058

Status Date 04-JUN-2018 19-AUG-2018 19-AUG-2018 NOTE: AVERAGE UTILISATION 280 FH & 120 FC PER MONTHS

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ENGINE Pos.#1 - LLP

ENGINE TYPE: TSN: 42.798 EFH TSLSV: 21`836 EFH DATE:

CFM56-5B4 CSN: 16.693 EFC CSLSV: 8`483 EFC 04.jun.2018

NO. PART NAME PART NUMBER TOTAL HOURS

TOTAL CYCLES

LIFE LIMIT CYCLES

REMAINING CYCLES

LPC ROTOR ASSY

1 ) SHAFT, FAN 338-010-601-0 42`798 16`693 30`000 13`307

2 ) DISK STG.1, FAN 338-001-504-0 42`798 16`693 30`000 13`307

3 ) SPOOL, BOOSTER 338-001-906-0 42`798 16`693 30`000 13`307

HPC ROTOR ASSY

4 ) FRONT SHAFT, HPC 1386M56P03 42`798 16`693 20`000 3`307

5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G07 42`798 16`693 20`000 3`307

6 ) HPC ROTOR DISK STG 3 2116M23P01 42`798 16`693 20`000 3`307

7 ) HPCR SPOOL ASSY STG 4-9 2048M20G03 42`798 16`693 20`000 3`307

8 ) CDP ROTATING REAR AIR SEAL 2116M25P01 42`798 16`693 20`000 3`307

HPT ROTOR ASSY

9 ) HPT ROTOR FRONT SHAFT 2048M21P03 42`798 16`693 20`000 3`307

10 ) HPT FRONT ROTATING AIR SEAL 2116M20P02 42`798 16`693 20`000 3`307

11 ) DISK - HPT ROTOR 1498M43P07 42`798 16`693 20`000 3`307

12 ) HPT REAR SHAFT 1864M90P05 42`798 16`693 20`000 3`307

LPT ROTOR ASSY

13 ) LPT SHAFT 338-010-005-0 42`798 16`693 25`000 8`307

14 ) LPT ROTOR DISK STG 1 336-001-804-0 42`798 16`693 25`000 8`307

15 ) LPT ROTOR DISK STG 2 336-001-909-0 42`798 16`693 25`000 8`307

16 ) LPT ROTOR DISK STG 3 336-002-006-0 42`798 16`693 25`000 8`307

17 ) LPT ROTOR DISK STG 4 336-002-105-0 42`798 16`693 25`000 8`307

18 ) LPT ROTOR SUPPORT 338-077-502-0 42`798 16`693 25`000 8`307

NOTE: AVERAGE UTILISATION 280 FH & 120 FC PER MONTHS

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ENGINE Pos.#2 - LLP

ENGINE TYPE: TSN: 35.429 EFH TSLSV: 0 EFH DATE:

CFM56-5B4 CSN: 15.674 EFC CSLSV: 0 EFC 19.aug.2018

NO. PART NAME PART NUMBER TOTAL HOURS

TOTAL CYCLES

LIFE LIMIT CYCLES

REMAINING CYCLES

LPC ROTOR ASSY

1 ) SHAFT, FAN 338-010-601-0 35`429 15`674 30`000 14`326

2 ) DISK STG.1, FAN 338-001-504-0 35`429 15`674 30`000 14`326

3 ) SPOOL, BOOSTER 338-001-906-0 35`429 15`674 30`000 14`326

HPC ROTOR ASSY

4 ) FRONT SHAFT, HPC 1386M56P03 35`429 15`674 20`000 4`326

5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G07 35`429 15`674 20`000 4`326

6 ) HPC ROTOR DISK STG 3 2116M23P01 35`429 15`674 20`000 4`326

7 ) HPCR SPOOL ASSY STG 4-9 2048M20G03 35`429 15`674 20`000 4`326

8 ) CDP ROTATING REAR AIR SEAL 2116M25P01 35`429 15`674 20`000 4`326

HPT ROTOR ASSY

9 ) HPT ROTOR FRONT SHAFT 2048M21P03 35`429 15`674 20`000 4`326

10 ) HPT FRONT ROTATING AIR SEAL 2116M20P02 35`429 15`674 20`000 4`326

11 ) DISK - HPT ROTOR 1498M43P07 35`429 15`674 20`000 4`326

12 ) HPT REAR SHAFT 1864M90P05 35`429 15`674 20`000 4`326

LPT ROTOR ASSY

13 ) LPT SHAFT 338-010-005-0 35`429 15`674 25`000 9`326

14 ) LPT ROTOR DISK STG 1 336-001-804-0 35`429 15`674 25`000 9`326

15 ) LPT ROTOR DISK STG 2 336-001-909-0 35`429 15`674 25`000 9`326

16 ) LPT ROTOR DISK STG 3 336-002-006-0 35`429 15`674 25`000 9`326

17 ) LPT ROTOR DISK STG 4 336-002-105-0 35`429 15`674 25`000 9`326

18 ) LPT ROTOR SUPPORT 338-077-502-0 35`429 15`674 25`000 9`326

NOTE: AVERAGE UTILISATION 280 FH & 120 FC PER MONTHS

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A320-200 MSN. TBA Page 6 of 12

LDG DETAILS NLG LH MLG RH MLG Part Number NA28008-11 201581001 201581002

Serial Number TBA TBA TBA

Position NLG LH MLG RH MLG

Hours Since New 34`190 34`190 34`190

Cycles Since New 17`347 17`347 17`347

Last Overhaul Date 11-JUL-2017 04-JUL-2017 30-JUN-2017

Cycles Since Overhaul 817 817 817

Remaining Cycles 19`183 19`183 19`183

Overhaul Due Date 11-JUL-2027 04-JUL-2027 30-JUN-2027

Overhaul Interval 20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

20`000 CYC

or 10 Years

Brakes & Part Number Messier C202255XX

Status Date 19-AUG-2018 19-AUG-2018 19-AUG-2018 NOTE: AVERAGE UTILISATION 280 FH & 120 FC PER MONTHS

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A320-200 MSN. TBA Page 7 of 12

MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY

ATA 22 - Automatic Flight Controls FMGC Thales Avionics C13043AA06 2 FAC Thales Avionics B397BAM0624 2 FCU Thales Avionics C12850AC02 1 MCDU Thales Avionics C19266DA01 2

ATA 23 – Communication HF Transceiver Honeywell 964-0452-012 1 VHF Transceiver Honeywell 064-50000-0505 3 Cockpit Voice Recorder Honeywell 980-6022-001 1 PRAM / iPRAM (Integrated PRAM) Panasonic RD-AX7675-51 1 Tape Reproducer or CD Player (Audio Entertainment)

Panasonic RD-AX7095-01 1

Tape Reproducer or DVD Player (Video Entertainment)

Panasonic RD-AV1216-01 1

Audio Management Unit TEAM AMU4031SA140204 1 ATA 31 - Indication and Recording System FDR –Flight Data Recorder Honeywell 980-4700-042 1 FDIU – Flight Data Interface Unit Thales Avionics C12860AA02 1 FDIMU – Flight Data Interface and Management Unit

Sagem ED48A100 1

Multi-Use Printer Honeywell 8055515-4501 1

ATA 34 – Navigation ADIRU – Air Data Inertial Reference Unit Northrop Grumman 465020-03030316 3 ISIS – Integrated Standby Instrument System

Thales C16221VA01 1

Enhanced Ground Proximity Warning Computer

Honeywell 965-1676-003 1

Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell 940-0351-005 1 ATC Mode S Transponder Honeywell 066-01127-1402 2 DME Interrogator Honeywell 066-50013-0202 2 VOR Receiver Honeywell 066-50012-0212 2 MMR – Multi-Mode Receiver Thales TLS755-01-0102A 2 Radio Altimeter Transceiver Honeywell 066-50007-0232 2 ADF Receiver Honeywell 066-50014-0202 1

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MODIFICATION STATUS COMPLIANCE NOTEs AIRBUS STD. SPEC. D000 02000 / ISSUE Yes

EASA TCDS EASA.A.064

NOISE Abatement Compliance Yes Stage IV iaw. ICAO Annex 16, Volume I, Part II

Approach Category Yes CAT III B

ETOPS Yes 90 min

Over Water capability Yes

Sharklets/Winglets No

Auxiliary Fuel Capacity No

Fuel Tank Inerting System (AIRBUS) No EASA – P by 01-JAN-2012; R – Not required

FAA – P by 28-DEC-2010 / R 100% Fleet by 26-DEC-2017

Nitrogen Gas System (BOEING) No

Reinforced Cockpit Door Yes

Cockpit 4th occupant seat Yes

Cargo Fire Suppression Yes

Cargo Loading System No

Cockpit Door Surveillance System Yes

EGPWS Yes

RVSM Yes

TCAS 7.1 Yes EASA – P on 12-MAR-2014 / R on 01-DEC-2015

FAA – Not required

Enhanced Surveillance (EHS) Mode S, ATC Transponder Yes

Elementary Surveillance (ELS) Yes

ATC Mode S Transponder ADS-B Out DO 260B capability No EASA – P on 08-JUN-2016 & R on 07-JUN-2020

FAA – P & R on 01-JAN-2020

Predictive Windshear Yes

Head Up Display (HUD) No EASA / FAA – Not mandatory

CAAC – R - 10% Fleet by 2015 & R - 100% by 2025

Area Navigation (BRNAV & PRNAV) Yes BRNAV = +/- 5 NM RNAV5 & PRNAV = +/- 1 NM RNAV1

Aircraft Performance Based Navigation (PBN) Capability

A/C PBN APPROVAL = RNP APCH (to LNAV/VNAV) Yes

EASA – 3 Phase Approach – Various dates

FAA – Not required

GPS Installed Yes

FM Immunity Yes

VHF 8.33 kHz Chanel spacing Yes EASA – Mandatory above FL195

FAA – Not mandatory

FANS 1/A Installed & Activated No EASA & FAA on NAT between FL350-390

FANS B+ Installed & Activated No

ATN B1 Data Link (CPDLC) Installed Yes EASA – P & R on 05-FEB-2020 for AC > JAN-2003

and R on 01-JAN-2023 for AC < JAN-2003

FAA – Not required

SATCOM Installed No EASA – Not mandatory

FAA – Mandatory, if ETOPS > 180 Mins

CAAC – R - 50% Fleet by 2015 & R - 100% by 2017

CVR with Data Link Recording Yes EASA – P on 08-APR-2014 / R on 01-JAN-2016 CAT.IDE.A195

FAA – P & R on 12-DEC-2010

SSCVR 2Hrs + ULB 90 Days Yes EASA – P & R by 01-JUN-2018

FAA – ULB < 30 Days by 01-DEC-2015 & < 90 Days by 01-

DEC-2015

SSFDR + ULB 90 Days Yes

Low Frequency Underwater Locator Device (ULD) No EASA – P & R by 01-JAN-2019 CAT.IDE.A190

FAA / CAAC – Not required

ELT 121.5 / 406 MHz - Fixed Yes

ELT 121.5 / 243 / 406 MHz - Portable Yes

NOTE: P – PRODUCTION & R - RETROFIT

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A320-200 MSN. TBA Page 9 of 12

INTERIOR CONFIGURATION Galleys 2 (G1; G5) Catering Standard ATLAS

Lavatories 3 (A; D; E) Ovens/Water Boilers/Coffey Makers 3+5+0

Attendant Seats 6 (2+4) Cargo Configuration Bulk

In Flight Entertainment Yes Cockpit Configuration Standard (2+2)

Seats Quantity Manufacturer Part Number

Economy Class 168 B/E Aerospace 1013165-XXX

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CARGO CONFIGURATION Cargo Configuration Bulk Designee (Fire Detection/Protection) class C

Cargo Volume 37.42 3Metres Containers No

Load Limitation 9`435 Kg Main Cargo Door(s) 71” x 48”

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A320-200 MSN. TBA Page 11 of 12

EMERGENCY EQUIPMENT

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A320-200 MSN. TBA Page 12 of 12

PERFORMANCE

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