Challenger 300 Airplane Flight Manual (Imperial)

MODEL BD-100-1A10

CUSTOMER SUPPORT PUBLICATION No. 100-1

Learjet 45 AFM Introduction

DOT APPROVED

AIRPLANE FLIGHT MANUAL

IMPERIAL

CSP 100-1 Nov 20/2007REV 10

For Training Purposes Only

Learjet 45 AFM Introduction

Airplane Flight Manual

CSP 100-1


RECORD OF REVISIONS

DOT Approved Apr 28/2005 Airplane Flight Manual 00-01-01REV 3 CSP 100-1

5/19/05

The Airplane Flight Manual is valid only when all the issued revisions areincorporated. Record the date you insert each revision in your manual.

Revision /DOT

ApprovalPages Affected Description of Revision

DATEIncorporated

/Signature

REV-1W. JUPP13 May,

2004

Front Matter:Approval Page00-01-01 thru 00-01-0800-02-01 thru 00-02-0300-03-01 thru 00-03-05

Add note for FAA/JAA approval.Update Record of Revisions.Update Record of Temporaries.Update List of Effective Pages.

Chapter 1 - Introduction:01-01-01 Reword text. Add Chapter 8.Chapter 2 - Limitations:

02-00-01 & 02-00-02 Update TOC.02-01-01 Reword text. Add RVSM and

wing anti-ice text (TR-11). Delete engine anti-ice text.

02-01-02 Remove flight op temp limits. Delete engine and wing anti-ice text and note.

02-01-03 (Added) Page added for text flow.02-02-01 & 02-02-0202-02-03 (Added)

Update weights and add CG chart and effectivities.

02-03-01 Revise format. Add caution.02-03-03 Increase press alt limit (TR-7).02-04-01 Delete unnecessary text.

Remove autopilot limitation.02-04-02 Update FMS info & software no.02-04-03 Update FMS info & software no.02-04-04 Update FMS info. Add Stdby

compass limit (TR-15). Update TAWS info. Remove towbarless towing limit (TR-21).

02-04-05 (Added) Add electrical/hydraulic text and battery temperature limits.

02-05-01 Delete Minimum Takeoff Fuel. (Duplicate info on 02-05-02).Add JP-4/JET B to list of approved fuels (TR-12).

02-05-02 Update pres. refuel data (TR-16). Correct Gravity Refuel data.

02-06-01 Delete manual ignition req. Update operating limits (TR-10).

02-06-02 Update Ground Start Env. (TR-10)

02-06-03 Update APU alt. limit (TR-25).

REV 3


RECORD OF REVISIONS

00-01-02 Airplane Flight Manual DOT Approved Apr 28/2005CSP 100-1 REV 3

5/19/05

REV-1 Chapter 3 - Emergency:(Cont) 03-00-02 & 03-00-03 Update TOC (TR-10).

W. JUPP13 May,

03-12-01 Correct O2 switch nomenclature. Add prolonged Ops warning.

2004 03-12-02 Change Cabin Delta P value (TR-8).03-12-03 & 03-12-04 Add verbiage to procedure.03-17-02 Delete note.03-19-01 thru 03-19-03 Update CAS & other text (TR-10).03-23-03 Note that stall pusher is not appli-

cable to JAA (TR-3). Change sequence of procedure.

03-23-04 thru 03-23-06 Update nomenclature.03-25-01 Update nomenclature. Change

gear to MLG downlock assist.03-27-01 Added rhombus.03-28-02 & 03-28-03 Update nomenclature. Deleted

note.03-29-01 & 03-29-02 Update nomenclature.03-32-07 Update nomenclature.03-32-08 Update nomenclature. Revise

Relight time (TR-28).03-32-09 Revise Relight time (TR-28).03-34-01 Update nomenclature. Delete

note for manual pressurization (TR-9).

03-34-03 Update CAS list and text (TR-10).03-34-04 Insert notes for standby compass

(TR-15).03-34-05 Update CAS list and text (TR-10).03-34-07 Delete LAV SMOKE (TR-17) and

delete page 03-34-08 per text flow. Update O2 switch (TR-10).

Chapter 4 - Normal:

04-00-01 Update TOC.04-02-02 Change panel to door.04-02-03 Modify Fuel water Drain proce-

dure and insert first flight symbol.

04-02-04 Insert note for wear pins. Change panel to door.

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS


5/19/05

REV-1(Cont)

04-02-06 Modify fuel water drain procedure and insert first flight symbol.

W. JUPP13 May,

2004

04-02-07 Remove notes for FLAPS FAULT (A) (TR-13), and FLT SPOILERS DEPLOY (C).

04-02-08 Delete unnecessary text. Reword air data note. Delete step 16 TAWS WARN TERRAIN switch. Add RAM AIR switch checks.

04-02-09 Delete notes for APU GEN OVERLOAD (C) and SEC STAB TRIM FAIL (C). Add Therapeutic Oxy. Update format for Altimeter.

04-03-01 Delete ignition switch step.04-03-02 Delete ignition switch steps.

(TR-10). Update page reference.04-03-03 Delete (Two Engines).

04-03-04 Delete (Two Engines) and notes, chg text sequence(TR-10).

04-03-05,04-03-06 (Deleted)04-03-07 (Deleted)

Text flow change. Delete entire BEFORE TAXI (One Engine) and TAXI AND BEFORE TAKEOFF (One Engine) procedure.

04-04-01 Change N LDG/ TAXI light switch to OFF. Delete Caution for engine anti-ice (TR-10). Change Altimeter Set text. Add note for VOR way-point.

04-04-02 Update nomenclature.04-05-01 Delete Note for REVERSER FAIL

(C) (TR-10).04-05-02 Delete IGNITION switch. Delete

APU BLEED switch (TR-10).04-05-03 (Deleted) Delete QUICK TURN-AROUND

(No Eng Shutdown) procedure.Chapter 5 - Non-Normal:

05-10-06 Update TOC (TR-10).05-12-01 Delete note for AIR COND TEMP

HIGH (C).

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS


5/19/05

REV-1(Cont)

05-12-04 Update procedure for Manual Ditching.

W. JUPP13 May,

05-12-05 Delete notes for AIR COND TEMP HIGH (C).

2004 05-14-01 Add Yaw Damper Fail Note.05-17-01 Update CAS list (TR-10). Add note

for stby compass limit (TR-15).05-17-02 & 05-19-02 Update CAS list (TR-10).05-19-03 Clarify STALL PUSHER OFF not

applicable to JAA aircraft. Update CAS list (TR-10).

05-19-04 & 05-19-05 Update CAS list (TR-10). Add EMER LTS switch procedures.

05-23-01 Update nomenclature.05-23-02 thru 05-23-04 Delete/update notes.

05-23-05 & 05-23-06 Update nomenclature.05-23-09 Clarify STALL PUSHER OFF not

applicable to JAA aircraft.05-24-01 Change FUEL PUMP switch Off

to AUTO.05-25-01 Update nomenclature.05-25-04 Update nomenclature.

05-28-01 Delete BRAKE FAULT (TR-10).05-28-02 Move text.05-28-03 Remove on landing from first

step of NWS FAIL.05-29-01 & 05-29-02 Update nomenclature.

05-32-01 & 05-32-02 Add L (R) ENG DSPL MISCOMP (C) procedure.

05-32-03 Add (C) after IGN EI to distin-guish from green message.

05-32-06 Add IGNITION switch procedure (TR-6).

05-32-07 Remove notes on idle times. Update Relight times and text (TR-28).

05-32-08 Add N2 table for Windmill Airstart. Update Relight times and text(TR-28).

05-40-02 Update TOC (TR-10).

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS


5/19/05

REV-1(Cont)

05-57-01 Remove L (R) ENGINE ANTI-ICE FAULT (A), (TR-10).

W. JUPP 05-62-01 Add Note.

13 May, 2004

Chapter 6 -Performance:

Update and reformat tables, charts and text (TR-14).

06-00-01 thru 06-00-11 Same as above.06-01-01 thru 06-01-09 Same as above.

06-01-10 Add effectivity.06-01-11 Add Noise Levels & effectivity.06-01-12 thru 06-01-23 Update and reformat tables,

charts and text (TR-14).06-10-01 thru 06-10-43

06-20-01 thru 06-20-1806-21-01 thru 06-21-4306-22-01 thru 06-22-48

06-23-01 thru 06-23-4306-24-01 thru 06-24-4906-25-01 thru 06-25-04

06-30-01 thru 06-30-0406-40-01 thru 06-40-0406-41-01 thru 06-41-08

06-42-01 thru 06-42-0806-43-01 thru 06-43-0906-50-01 thru 06-50-08

Chapter 7- SupplementsSupp 1 - Operation onContaminated Runways:

Update/reformat tables, charts, and text (TR-14).

07-00-01

07-01-00-0107-01-11-01 thru07-01-11-1407-01-12-01 thru07-01-12-1407-01-13-01 thru07-01-13-2607-01-14-01 thru07-01-14-2607-01-21-01 thru07-01-21-14

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS


5/19/05

REV-1(Cont)

07-01-22-01 thru07-01-22-14

Update/reformat tables, charts, and text (TR-14).

W. JUPP13 May,

07-01-23-01 thru07-01-23-26

2004 07-01-24-01 thru07-01-24-26

07-01-31-01 thru07-01-31-09Supp 2 - MMEL Items: Add Supplement 2 (TR-19).07-02-00-0107-02-01-01 thru07-02-01-12Chapter 8 - Appendices: Add Chapter 8.

08-00-0108-01-00-01 08-01-01-0108-01-02-0108-01-23-0108-01-27-0108-01-32-0108-01-33-0108-01-51-0108-01-52-0108-01-53-0108-01-55-0108-01-57-0108-01-78-01

Add Appendices TOC.Add APPENDIX 1 Configuration Deviation List (CDL), (TR-18).

REV-2W. JUPP

Front Matter:Approval Page00-01-01 thru 00-01-08

Remove MTOW from this page.Update Record of Revisions.

09 Dec, 00-02-01 thru 00-02-04 Update Record of Temporaries.

2004 00-03-01 thru 00-03-06 Update List of Effective Pages.Chapter 2 - Limitations:02-00-0102-02-0102-02-0202-02-0302-03-0202-03-0302-05-02

Update TOC.Add weights and effectivities.Add effectivity.Add CG chart with effectivity.Update Airspeed/Mach chart.Remove Crosswind Limitation.Add JP-4, JET B to Temp Limita-tions list.

Revision /DOT


DATEIncorporated

/Signature

REV 3


RECORD OF REVISIONS


5/19/05

REV-2 (Cont)

W. JUPP09 Dec,

2004

Chapter 3 - Normal:04-03-02

Chapter 6 -Performance:06-00-01 and 06-00-0206-01-01 thru 06-01-11

Move XBLEED switch from External to Crossbleed Engine Start, and added steps (RS-8).

Update TOC.Add lb/gal vol. conversion table, Update page and fig. numbers.

06-01-1206-01-13 thru 06-01-2406-01-25 (Added)06-20-0306-21-06 thru 06-21-1606-22-02 thru 06-22-1206-23-06 thru 06-23-1606-23-18 thru 06-23-2806-23-30 thru 06-23-4006-24-02 thru 06-24-1206-24-14 thru 06-24-2406-24-26 thru 06-24-3606-24-40 thru 06-24-4506-25-02 thru 06-25-0506-30-02 thru 06-30-0506-41-02 thru 06-41-0706-41-0806-42-02 thru 06-42-0706-42-0806-43-06 and 06-43-07

Add Demonstrated Crosswinds.

Update page and fig. numbers.Add note for V1.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Update MTOW data.Delete page.Update MTOW data.Delete page.Update MTOW data.

Chapter 7 - SupplementsSupp 1 - Operation onContaminated Runways:07-00-0107-01-00-01 thru07-01-00-0407-01-00-06 thru07-01-00-0807-01-00-0907-01-01-0107-01-01-02 thru07-01-01-0507-01-11-02 thru07-01-11-1207-01-12-02 thru07-01-12-12

Update Log of Supplements.

Update TOC.

Update TOC.Add page.Update Text.

Update MTOW data.

Update MTOW data.

Update MTOW data.

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS


5/19/05

REV-2 (Cont)

W. JUPP09 Dec,

2004

07-01-13-02 thru07-01-13-1407-01-13-15 thru07-01-13-2607-01-14-02 thru07-01-14-1207-01-14-14 thru07-01-14-2607-01-15-01 thru07-01-15-2607-01-21-02 thru07-01-21-1207-01-22-02 thru07-01-22-1207-01-23-02 thru07-01-23-1407-01-23-15 thru07-01-23-2607-01-24-02 thru07-01-24-1207-01-24-14 thru07-01-24-2607-01-25-01 thru07-01-25-2607-01-31-0207-01-32-01 thru07-01-32-0307-01-33-01 thru07-01-33-0307-01-34-01 thru07-01-34-03

Update MTOW data.

Delete pages.

Update MTOW data.

Update MTOW data.

Add page. Update data.

Update MTOW data.

Update MTOW data.

Update data.

Delete page.

Update data.

Update MTOW data.

Add page. Update data.Update MTOW data.

Update section number and data.

Update section number and data.

Update section number and data.REV-3

W. JUPP28 Apr, 2005

02-04-0203-19-0203-34-0303-34-0504-02-0804-03-0305-10-0405-10-0505-12-0205-12-06(Continued)

To meet the requirements of theHoneywell FADEC v10b, andRockwell Collins v6.0 softwareupgrades.

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS

DOT Approved Aug 16/2005 Airplane Flight Manual 00-01-09REV 4 CSP 100-1

9/12/05

REV-3 (Cont)

W. JUPP28 Apr, 2005

05-19-02thru 05-19-05

05-24-0105-27-0505-27-05.105-27-0605-27-0705-32-0305-40-0105-40-0205-43-0105-54-0105-62-01

08-01-02-0108-01-27-0108-01-32-0108-01-33-0108-01-51-0108-01-52-0108-01-53-0108-01-55-0108-01-57-0108-01-57-02

Add information to meet therequirements of the HoneywellFADEC v10b, and RockwellCollins v6.0 software upgrades.

Replace the verbiage structur-ally limited weights withmaximum certified weights inthe CDL. (RS-9)

REV-4 W. JUPP16 Aug,

2005

02-06-02 Remove reference to Adden-dum II - ENGINE OIL SERVIC-ING.

03-23-03 Correct the circuit breaker panelnumbers.

07-01-31-03

07-01-31-0407-00-01,07-03-00-01,07-03-01-01 thru07-03-01-07

Add Correction Chart for ActualLanding Distance - ICE - 30 .Delete duplicate data.Add Supplement-3 to the AFMfor CAT II Operations. (TR-23)

02-06-0302-06-04

Replacement of the APU StarterClutch for Improved ColdWeather Operation. (TR-26)

03-27-0103-27-02

Revise WING ANTI-ICE LEAK(W) procedure. (TR-29)

02-04-02 Update FMS Limitations for air-craft with/and without SB 100-11-01 installed. (TR-33)

Revision /DOT


DATEIncorporated

/Signature

REV 4


RECORD OF REVISIONS

00-01-10 Airplane Flight Manual DOT Approved Aug 16/2005CSP 100-1 REV 4

9/12/05

REV-4 (Cont)

W. JUPP16 Aug,

2005

02-01-03

02-04-02

02-03-0402-06-0102-06-02

Reference FCOM vol. 1, Sup-plement-1 for cold weatheroperations.FMS - Incorporate a directive toreset FUEL USED after re-installing batteries.

Expand the temperature limita-tions for ground exposure forapplicable aircraft. (TR-34)

03-19-01thru03-19-04,03-23-04thru03-23-06,03-25-0103-25-02,03-28-01thru03-28-03,03-29-0103-29-02,03-32-07,04-04-0104-04-02,05-10-0305-10-04,05-19-0105-19-02,05-23-05thru05-23-07,05-25-01thru05-25-03,05-25-0505-25-06,05-29-0105-29-02

Specify by aircraft effectivity theprocedures and associated CASmessages for the HydraulicMotor Driven Generator(HMDG) for pre/post PSEUsoftware version 10 upgrade.Also to incorporate proceduresto minimize the possibility ofcascade failures of generators,and to allow recovery ofgenerators taken off bus due toan internal failure of a DirectCurrent Motor-Driven Pump(DCMP). (TR-35)

Revision /DOT


DATEIncorporated

/Signature

REV 4


RECORD OF REVISIONS


10/11/06

REV-4 (Cont)

W. JUPP16 Aug,

2005

03-19-01thru03-19-04

05-25-0105-25-02

Correct aircraft effectivities andprocedures for the HydraulicMotor Driven Generator(HMDG) for pre/post PSEUsoftware v10 upgrade.Correct procedures to minimizethe possibility of cascade fail-ures of generators, and to allowrecovery of generators taken offbus due to an internal failure ofa (DCMP) Direct Current Motor-driven Pump.(TR-35-1)

06-00-10,06-20-09thru06-20-12,06-25-06

Add information for Final Seg-ment Net Climb Gradient.(TR-36)

02-00-0102-03-03

Add a takeoff limitation toemphasize requirement for anaerodynamically clean airplaneduring cold weather operation.(TR-37)

02-04-02 Incorporate information forverification of V-speed data forSingle and Dual FMS. (TR-38)

05-28-0205-28-0505-40-0205-58-01

Modifiy the GEAR SYS FAIL (C)& WOW FAIL (C) procedures,and add a PROX SYS FAULT(A) procedure in the AFM.(TR-39)

05-23-01 Add a CAUTION to the FLAPSFAIL (C) procedure regarding anunreliable Low Speed Cue indi-cation. (TR-40)

07-02-00-0107-02-01-0107-02-01-1207-02-01-1307-02-01-14

Update Supp. 2 - MMEL, forOne AHRS Channel inopera-tive, and Radio Altimeter Inoper-ative. Correct the NosewheelSteering data. (RS-7)

04-03-0304-05-02

Add the option of performingfirst flight anti-ice system checksat Before Taxi, or After Landing.(RS-11)

Revision /DOT


DATEIncorporated

/Signature


RECORD OF REVISIONS

00-01-12 Airplane Flight Manual DOT Approved Sep 29/2006CSP 100-1 REV 7

10/11/06

REV-5 W. JUPPFeb 08,

2006

02-06-03 Revise APU Altitude Limitationsregarding Bleed Air for ECS,with/without SB100-21-05.(RS-16)

REV-6 W. JUPPJul 31, 2006

02-00-01 and -0206-00-0103-19-0205-12-0305-19-0205-19-04 and -05

Update TOC.Update TOC.Raise altitude limit from 25,000to 31,000 ft. (RS-10)

05-10-0505-19-0205-27-05 and -05.105-27-06

Change CAS messagefrom: L (R) WING A/ICE FAIL,to: L (R) WING ANTI-ICE FAIL.(RS-15)

05-54-01 Add a step to monitor the wingfuel quantity when the GRAVITYXFLOW valve fails to close.(RS-18)

03-19-0103-19-0203-19-03

Delete references to PTU.(Information is covered in anSB). (RS-20)

03-34-07 Add a step to close the lavatorydoor to control smoke migration.(TR-41)

02-03-0302-03-04

Add crosswind limitations forSAAU airplanes. (TR-42)

02-03-04 thru02-03-0602-04-02 thru 02-04-0803-00-0103-17-01 thru 03-17-0503-23-0603-25-01 03-29-01 and 03-29-02 03-32-01 06-01-12

Add data for airplanes on the RFand CIS countries registry.(TR-43)

REV-7 W. JUPPSep 29,

200602-04-06A05-10-0205-17-03 and 05-17-04

Add Limitations for IntegratedFlight Information System (IFIS)Update TOC.Add data for IFIS. (RS-22)

Revision /DOT


DATEIncorporated

/Signature

REV 7


RECORD OF REVISIONS

DOT Approved Nov 20/2007 Airplane Flight Manual 00-01-13REV 10 CSP 100-1

12/12/07

The Airplane Flight Manual is valid only when all the issued revisions areincorporated. Record the date you insert each revision in your manual.

Revision /DOT


DATEIncorporated

/Signature

REV-8 W. JUPPApr 18, 2007

02-01-01

02-01-02 & -03& TR-20

02-04-06

Adds statements to supportAC 90-100 En Route and Termi-nal RNAV Operations. (RS-14)To update effectivities, andpermenantly incorporate TR-20into the manual. (RS-28, TR-20)To update PRNAV limitations andadd FMS information for runwayswith a displaced threshold.(RS-24)

REV-9 W. JUPPJun 08, 2007

04-02-02 To add a step at the walkaroundinspection, [for FAA registeredairplanes], to ensure that torquelink quick disconnect is con-nected. (RS-29)

REV-10 W. JUPPNov 20,

2007

Approval Page - Brazil02-04-06A03-12-0203-12-02A05-12-0205-12-02A05-12-03

02-01-01

02-05-01

03-12-0303-12-04

08-01-02-01

To add information for Brazilianregistered airplanes. (RS-34)

To update AC 90-100 to revisionAC 90-100A. (RS-30)

To update approved fuel anti-icing additives. (RS-19)

To increase wait time for Trim AirLeak/Pack Leak. (RS-33)

To add requirement for listing allmissing parts in the FlightRelease prior to aircraft dispatch.(RS-21)

REV 10


INTRODUCTION

DOT Approved Aug 01/2007 Airplane Flight Manual 00-02-01CSP 100-1

8/6/07

RECORD OF TEMPORARY REVISIONSIt is the responsibility of the aircraft owner and operator to maintain their basicAFM with the temporary revisions applicable to their aircraft.

TR # Sectionor Page

Description DOT Approval

Status

TR-1 06-01-13 Performance Corrections - Engine and Wing Anti-Ice ON Bleed Configurations

W. JuppMay 30/03

Superseded by TR-14

TR-2 07-01-05 Performance Corrections - Engine and Wing Anti-Ice ON Bleed Configurations

W. JuppMay 30/03

Superseded by TR-14

TR-3 03-23-0303-34-0305-19-0305-23-09

Specify that Stall Pusher Off is NOT applicable to JAA air-craft

W. JuppJuly 18/03

Superseded by REV 1

TR-4 03-23-02 For JAA aircraft only W. JuppJuly 18/03

ActiveFor JAAAircraft

TR-5 05-28-0305-28-04

INBD or OUTBD BRAKES FAIL (C) procedure change, based on discovery of some BCU failure modes

W. JuppJuly 18/03

Canceled at REV 1

TR-6 05-32-06 ENGINE AIRSTART, BEFORE START, IGN switch procedures

W. JuppJuly 29/03

Superseded by REV 1

TR-7 02-03-03 IASC v92175A020200High Alt to FL 10

W. JuppOct 17/03

Superseded by REV 1

TR-8 03-12-02 IASC v92175A020200,Cabin Delta P to -0.5 psid or less

W. JuppOct 17/03

Superseded by REV 1

TR-9 03-34-01 IASC v92175A020200, Delete Note (depressurization)

W. JuppOct 17/03

Superseded by REV 1

TR-10 02-01-0102-04-0102-04-0202-04-0302-04-0402-06-0102-06-0203-00-0203-00-0303-19-0103-34-0303-34-0503-34-07

FADEC v9BRC v5.0RC v5.0RC v5.0RC v5.0FADEC v9BFADEC v9BRC v5.0RC v5.0RC v5.0RC v5.0RC v5.0RC v5.0

W. JuppOct 17/03

Superseded by REV 1


INTRODUCTION

00-02-02 Airplane Flight Manual DOT Approved Aug 01/2007CSP 100-1

8/6/07

TR-10(Cont)

04-03-0104-03-0204-03-0404-03-0604-03-0704-04-0104-05-0104-05-0205-10-0605-17-0105-17-0205-19-0205-19-0305-19-0405-19-0505-28-0105-40-0205-57-01

FADEC v9BFADEC v9BFADEC v9BFADEC v9BFADEC v9BFADEC v9BFADEC v9BFADEC v9BRC v5.0FADEC v9BFADEC v9BRC v5.0RC v5.0RC v5.0RC v5.0RC v5.0FADEC v9BFADEC v9B

W. JuppOct 17/03

Superseded by REV 1

TR-11 02-01-01 Add RVSM limits to the LIMITATIONS Chapter.

W. JuppNov 14/03

Superseded by REV 1

TR-12 02-05-01 Add JP-4/JET B to the list ofapproved fuels in the LIMITA-TIONS Chapter.

W. JuppMay 18/04

Superseded by REV 1

TR-13 04-02-07 Remove FLAPS FAULT (A) to conform to FCU v4.2 software

W. JuppOct 17/03

Superseded by REV 1

TR-14 Chapters6 & 7

Update Performance and Contaminated Runway Per-formance Chapters

W. JuppOct 17/03

Superseded by REV 1

TR-15 02-04-0403-34-0405-17-01

Add limitation to require L (R) WSHLD/WINDOW turned off while viewing Standby Compass

W. JuppOct 17/03

Superseded by REV 1

TR-16 02-05-02 Change maximum usable fuel load for pressure refueling

W. JuppOct 17/03

Superseded by REV 1

TR-17 03-34-07 Remove the LAV SMOKE (W) procedure

W. JuppNov 11/03

Superseded by REV 1

TR-18 Chapter 8 CDL - Appendix 1 W. JuppMar 31/04

Superseded by REV 1

TR-19 07-00-0107-02-0007-02-01

thru07-02-12

Add Supplemental Informa-tion for the MMEL

W. JuppNov 10/03

Superseded by REV 1

TR # Sectionor Page


Status


INTRODUCTION


8/6/07

TR-20 02-01-02 Add requirements for use of ice detector as primary means of wing anti-icing oper-ation

W. JuppApr 18/07

Superseded by REV 8

TR-21 02-04-04 Remove Towbarless Towing from the Limitations Chapter

W. JuppJan 08/04

Superseded by REV 1

TR-23 07-03-00-01,07-03-01-01

thru07-03-01-07

Add Supplement-3 to the AFM for CAT II Operations

W. JuppJan 03/05

Superseded by REV 4

TR-25 02-06-03 Revise APU Max Alt Limita-tions

W. JuppMar 26/04

Superseded by REV 1

TR-26 02-06-03 Replacement of the APUStarter Clutch for ImprovedCold Weather Operation

W. JuppNov 10/04

Superseded by REV 4

TR-27 02-03-0306-00-0106-01-12

07-01-00-0107-01-00-05

Delete the increased speed requirements and penalties associated with using TYPE II and TYPE IV anti-icing fluids

W. JuppMar 26/04

Superseded by REV 1

TR-28 03-32-0803-32-0905-32-0705-32-08

Revise Windmill Relight times, and make other miscel-laneous changes

W. JuppApr 01/04

Superseded by REV 1

TR-29 03-27-0103-27-02

Revise WING ANTI-ICE LEAK (W) procedure

W. JuppNov 18/04

Superseded by REV 4

TR-30 03-19-0203-19-0305-10-0305-19-01

To specify procedures and associated CAS messages for the Hydraulic Motor Driven Generator (HMDG) for pre/post PSEU software v10 upgrade.

W. JuppSep 14/04

Superseded by REV 4

TR-32 02-04-02 Specify System Limitations foraircraft with DATALINKinstalled.

W. JuppMar 03/05

Superseded by REV 3

TR-33 02-04-02 To update FMS Limitations foraircraft with/and without SB100-11-01 installed.

W. JuppFeb 24/05

Superseded by REV 4

TR # Sectionor Page


Status


INTRODUCTION

00-02-04 Airplane Flight Manual DOT Approved Aug 01/2007CSP 100-1

8/6/07

TR-34 02-01-03

02-04-02

02-03-0402-06-0102-06-02

To reference FCOM vol. 1,Supplement-1 for cold weath-er operations.

FMS - To incorporate adirective to reset FUEL USEDafter re-installing batteries.

To expand the temperaturelimitations for ground expo-sure for applicable aircraft.

W. JuppDec 17/04

Superseded by REV 4

TR-35 03-19-0203-19-0303-19-0403-23-0303-23-0403-23-0503-23-0603-23-0703-25-0103-25-0203-28-0203-28-0303-28-0403-29-0103-29-0203-32-0704-04-0104-04-0205-10-0305-19-0105-19-0205-23-0605-23-0705-25-0105-25-0205-25-0505-25-0605-29-0105-29-02

To specify by aircraft effectivitythe procedures and associat-ed CAS messages for theHydraulic Motor Driven Gen-erator (HMDG) for pre/postPSEU software v10 upgrade.

Also to incorporate proce-dures to minimize thepossibility of cascade failuresof generators, and to allowrecovery of generators takenoff-bus due to an internalfailure of a Direct CurrentMotor-Driven Pump (DCMP).

W. JuppDec 17/04

Superseded by REV 4

TR # Sectionor Page


Status


INTRODUCTION


10/22/07

TR35-1

03-19-02thru

03-19-04

05-25-0105-25-02

To correct aircraft effectivityand procedures for theHydraulic Motor Driven Gen-erator (HMDG) for pre/postPSEU software v10 upgrade.

To correct procedures tominimize possibility of cas-cade failures of generators,and to allow recovery ofgenerators taken off-bus dueto an internal failure of a DirectCurrent Motor-Driven Pump(DCMP).

W. JuppApr 07/05

Superseded by REV 4

TR-36 06-00-1006-20-0906-20-1006-20-1106-20-1206-25-06

Add information for Final Seg-ment Net Climb Gradient.

W. JuppApr 08/05

Superseded by REV 4

TR-37 02-00-0102-03-03

Add a takeoff limitation toemphasize the requirementfor an aerodynamically cleanairplane during cold weatheroperation.

W. JuppMay 06/05

Superseded by REV 4

TR-38 02-04-02 Incorporate information forverification of V-speed data forSingle and Dual FMS.

W. JuppJan 31/05

Superseded by REV 4

TR-39 05-28-0205-28-0505-40-0205-58-01

To modify the GEAR SYS FAIL (C) & WOW FAIL (C) pro-cedures, and add a PROX SYS FAULT (A) procedure in the AFM.

W. JuppMar 02/05

Superseded by REV 4

TR-40 05-23-01 To add a CAUTION to the FLAPS FAIL (C) procedure regarding an unreliable Low Speed Cue indication.

W. JuppApr 11/05

Superseded by REV 4

TR-41 03-34-07 To add a step to CARGOSMOKE (W) for closinglavatory door to controlsmoke migration.

W. JuppApr 13/06

Superseded by REV 6

TR # Sectionor Page


Status


INTRODUCTION

00-02-06 Airplane Flight Manual DOT Approved Oct 11/2007CSP 100-1

10/22/07

TR-42 02-03-03 To add crosswind limitationsfor SAA of Ukraine regis-tered airplanes.

W. JuppMar 31/06

Superseded by REV 6

TR-43 02-03-03 02-04-02 02-04-0603-17-01 03-17-02 03-23-06 03-25-01 03-29-01 03-29-02 03-32-01 06-01-12

To add data for airplanes onthe RF and CIS countriesregistry.

W. JuppMay 15/06

Superseded by REV 6

TR-44 02-04-08 03-19-03 03-23-0403-23-05 03-23-06 03-25-02 03-28-02 03-29-01 03-29-02 03-32-07 03-34-03 03-34-05 04-02-09 04-04-02 04-05-02 05-17-03 05-23-02 05-23-06 05-25-02 05-25-05 05-29-0105-29-02

To add data for operation with hydraulic pumps OFF to prevent possible pump overheat.

W. JuppAug 01/07

Superseded by

TR-44-1

TR # Sectionor Page


Status


TR # SECTIONOR PAGE DESCRIPTIONDOT

APPROVAL STATUS

TR441 020408031903032304032305032306032502032802032901032902033201033202033203033204033205033207033210033403033405040209040401040402040502051703052302052306052502052505052901052902053201053202053203053205053208055401064306

To add data for restricteduse of the hydraulic pumpsto prevent possible pumpoverheat, on airplanes20003 to 20190 notincorporating ServiceBulletin 1002911.

W. JuppOct 11/07

Active

TR45 020501020502

To add bulk fuel temp limits,data for Russian &Ukrainian fuel, and JP8.

W.JuppJan 22/08

Active

TR46 052801052802055801

To update GEARDISAGREE (C), GEAR SYSFAIL (C), and PROX SYSFAULT (A) procedures forthe PSEU V12 upgrade.

R.W. WalkerMar 27/08

Active

INTRODUCTION

DOT Approved Mar 27/2008 000207Airplane Flight Manual

CSP 1001

RECORD OF TEMPORARY REVISIONS


TR # SECTIONOR PAGE DESCRIPTIONDOT

APPROVAL STATUS

TR47 02010302040103250104040205230105290207030101

To address glidepath limits,and provide data forapproaches between 3.5and 4.5 degrees.

R.W. WalkerMay 06/08

Active

TR48 020603 To remove the requirementfor APU inspection whenAPU SHUTDOWN (A) isdisplayed during preflight.


Active

TR49 020406 To provide clarification ofRNAV limitationsterminology.


Active

INTRODUCTION

DOT Approved May 06/2008000208 Airplane Flight Manual

CSP 1001For Training Purposes Only

LIST OF EFFECTIVE PAGES



Dates of issue for Original and Revised pages are:

Use this List of Effective Pages to determine the current status of the Airplane FlightManual. Pages affected by the current revision are indicated by an asterisk (*) immedi-ately preceding the page number.

Original................................................... O .........................................May 30/2003Revision ................................................... 1 ..........................................May 13/2004Revision ................................................... 2 ........................................... Dec 09/2004Revision ................................................... 3 ...........................................Apr 28/2005Revision ................................................... 4 .......................................... Aug 16/2005Revision ................................................... 5 ............................................Feb 08/2006Revision ................................................... 6 ............................................. Jul 31/2006Revision ................................................... 7 ........................................... Sep 29/2006Revision ................................................... 8 ...........................................Apr 18/2007Revision ................................................... 9 ............................................Jun 08/2007Revision .................................................. 10 ......................................... Nov 20/2007

The pages in this manual and this list show the aircraft applicability of thepages. Only the pages applicable to the aircraft assigned to this AirplaneFlight Manual must be retained. Pages not applicable to the aircraft may beremoved from this manual.

Page Revision Aircraft Affected

*Title Page ..................................... 10 AllApproval Page.............................2 All

*Approval Page-Brazil (Added) 10 All00-01-01 thru 00-01-08 ................ 3 All00-01-09......................................... 4 All00-01-10 and 00-01-11.................. 4 All00-01-12......................................... 7 All

*00-01-13........................................ 10 All00-02-01 thru 00-02-06 ................ 8 All

*00-03-01 thru 00-03-07 ............... 10 AllIntroduction

01-00-01........................................ O All01-01-01......................................... 1 All 01-01-02 thru 01-01-04 ............... O All

Limitations

02-00-01 and 02-00-02 ................. 6 All*02-01-01........................................ 10 All

02-01-02 and 02-01-03 ................. 8 All 02-02-01 thru 02-02-03 ................ 2 All 02-03-01......................................... 1 All02-03-02......................................... 2 All02-03-03 thru 02-03-06 ................ 6 All02-04-01......................................... 4 All02-04-02 thru 02-04-05 ................ 6 All02-04-06......................................... 8 All

REV 10For Training Purposes Only


00-03-02 Airplane Flight Manual DOT Approved Nov 20/2007CSP 100-1 REV 10

LIST OF EFFECTIVE PAGES (Cont)


*02-04-06A .................................... 10 All02-04-07 and 02-04-08 ................. 6 All

*02-05-01 ....................................... 10 All02-05-02 ........................................ 2 All02-06-01 and 02-06-02 ................. 4 All02-06-03 ........................................ 5 All02-06-04 ........................................ 4 All

Emergency Procedures

03-00-01 ........................................ 6 All03-00-02 and 03-00-03 ................. 1 All03-01-01 ........................................O All03-12-01 ........................................ 1 All

*03-12-02 ....................................... 10 All*03-12-02A(Added) ..................... 10 All*03-12-03 and 03-12-04 ................ 10 All03-15-01 ........................................O All03-17-01 thru 03-17-05 ................ 6 All03-19-01 thru 03-19-03 ................ 6 All03-20-01 ........................................O All03-23-01 and 03-23-02 .................O All03-23-03 thru 03-23-05 ................ 4 All03-23-06 ........................................ 6 All03-25-01 ........................................ 6 All03-25-02 ........................................ 4 All03-27-01 and 03-27-02 ................. 4 All03-28-01 thru 03-28-03 ................ 4 All03-29-01 and 03-29-02 ................. 6 All03-32-01 ........................................ 6 All03-32-02 thru 03-32-06 ................O All03-32-07 ........................................ 4 All03-32-08 and 03-32-09 ................. 1 All03-32-10 ........................................O All03-33-01 .......................................O All03-34-01 and 03-34-02 ................. 1 All03-34-03 ........................................ 3 All03-34-04 ........................................ 1 All03-34-05 ........................................ 3 All03-34-06 ........................................O All03-34-07 ........................................ 6 All03-35-01 and 03-35-02 .................O All

Normal Procedures

04-00-01 ........................................ 1 All04-01-01 ........................................O All04-02-01 ........................................O All04-02-02 ........................................ 9 All




LIST OF EFFECTIVE PAGES (Cont)Page Revision Aircraft Affected

04-02-03 and 04-02-04 ................. 1 All04-02-05........................................ O All04-02-06 and 04-02-07 ................. 1 All04-02-08......................................... 3 All04-02-09......................................... 1 All04-03-01......................................... 1 All04-03-02......................................... 2 All04-03-03......................................... 4 All04-03-04 and 04-03-05 ................. 1 All04-04-01 and 04-04-02 ................. 4 All04-04-03........................................ O All04-05-01......................................... 1 All04-05-02......................................... 4 All

Non-Normal Procedures

05-00-01........................................ O All05-10-01........................................ O All05-10-02......................................... 7 All05-10-03 and 05-10-04 ................. 4 All05-10-05......................................... 6 All05-10-06......................................... 1 All05-10-07........................................ O All05-11-01 ........................................ O All05-12-01......................................... 1 All

*05-12-02 and 05-12-03 ................ 10 All*05-12-02A (Added).....................10 All*05-12-03........................................ 10 All

05-12-04 and 05-12-05 ................. 1 All05-12-06......................................... 3 All05-12-07........................................ O All05-14-01 and 05-14-02 ................ O All05-15-01 and 05-15-02 ................ O All05-17-01 and 05-17-02 ................. 1 All05-17-03 and 05-17-04 ................. 7 All05-17-05........................................ O All05-18-01 and 05-18-02 ................ O All05-19-01......................................... 4 All05-19-02......................................... 6 All05-19-03......................................... 3 All05-19-04 and 05-19-05 ................. 6 All05-21-01 and 05-21-02 ................ O All05-23-01 and 05-23-02 ................. 4 All05-23-03......................................... 1 All05-23-05 thru 05-23-09 ................ 4 All05-24-01......................................... 3 All05-24-02........................................ O All





05-25-01 thru 05-25-03 ................ 4 All05-25-04 ........................................ 1 All05-25-05 and 05-25-06 ................. 4 All05-27-01 thru 05-27-04 ................O All05-27-05 ........................................ 6 All05-27-05.1 ..................................... 6 All05-27-06 ........................................ 6 All05-27-07 ........................................ 3 All05-28-01 ........................................ 1 All05-28-02 ........................................ 4 All05-28-03 and 05-28-04 ................. 1 All05-28-05 ........................................ 4 All05-29-01 and 05-29-02 ................. 4 All05-30-01 ........................................O All05-32-01 and 05-32-02 ................. 1 All05-32-03 and 05-32-04 ................. 3 All05-32-05 ........................................O All05-32-06 thru 05-32-08 ................ 1 All05-40-01 ........................................O All05-40-02 ........................................ 4 All05-41-01 ........................................O All05-44-01 ........................................O All05-45-01 ........................................O All05-47-01 ........................................O All05-52-01 ........................................O All05-54-01 ........................................ 6 All05-54-02 ........................................O All05-55-01 ........................................O All05-57-01 ........................................ 1 All05-58-01 ........................................ 4 All05-62-01 ........................................ 3 All

Performance Data

06-00-01 ........................................ 6 All06-00-02 ........................................ 2 All06-00-03 thru 06-00-09 ................ 1 All06-00-10 ........................................ 4 All06-00-11 and 06-00-12 ................. 1 All06-01-01 thru 06-01-08 ................ 1 All06-01-09 thru 06-01-11 ................ 2 All06-01-12 ........................................ 6 All06-01-13 thru 06-01-15 ................ 1 All06-01-16 thru 06-01-25 ................ 2 All06-10-01 thru 06-10-43 ................ 1 All06-20-01 and 06-20-02 ................. 1 All06-20-03 ........................................ 2 All





06-20-04 thru 06-20-08 ................ 1 All06-20-09 thru 06-20-12 ................ 4 All06-20-13 thru 06-20-18 ................ 1 All06-21-01 thru 06-21-05 ................ 1 All06-21-06 thru 06-21-16 ................ 2 All06-21-17......................................... 1 All06-21-18 thru 06-21-28 ................ 2 All06-21-29......................................... 1 All06-21-30 thru 06-21-40 ................ 2 All06-21-41 thru 06-21-43 ................ 1 All06-22-01......................................... 1 All06-22-02 thru 06-22-12 ................ 2 All06-22-13......................................... 1 All06-22-14 thru 06-22-24 ................ 2 All06-22-25......................................... 1 All06-22-26 thru 06-22-36 ................ 2 All06-22-37 thru 06-22-39 ................ 1 All06-22-40 thru 06-22-45 ................ 2 All06-22-46 thru 06-22-48 ................ 1 All06-23-01 thru 06-23-05 ................ 1 All06-23-06 thru 06-23-16 ................ 2 All06-23-17......................................... 1 All06-23-18 thru 06-23-28 ................ 2 All06-23-29......................................... 1 All06-23-30 thru 06-23-40 ................ 2 All06-23-41 thru 06-23-43 ................ 1 All06-24-01......................................... 1 All06-24-02 thru 06-24-12 ................ 2 All06-24-13......................................... 1 All06-24-14 thru 06-24-24 ................ 2 All06-24-25......................................... 1 All06-24-26 thru 06-24-36 ................ 2 All06-24-37 thru 06-24-39 ................ 1 All06-24-40 thru 06-24-45 ................ 2 All06-24-46 thru 06-24-49 ................ 1 All06-25-01......................................... 1 All06-25-02 thru 06-25-05 ................ 2 All06-25-06......................................... 4 All06-30-01......................................... 1 All06-30-02 thru 06-30-05 ................ 2 All06-40-01 thru 06-40-05 ................ 1 All06-41-01......................................... 1 All06-41-02 thru 06-41-07 ................ 2 All06-41-08......................................... 1 All06-42-01......................................... 1 All06-42-02 thru 06-42-07 ................ 2 All




LIST OF EFFECTIVE PAGES (Cont)


06-42-08 ........................................ 1 All06-43-01 thru 06-43-05 ................ 1 All06-43-06 and 06-43-07 ................. 2 All06-43-08 and 06-43-09 ................. 1 All06-50-01 thru 06-50-08 ................ 1 All

Supplements

07-00-01 ........................................ 4 AllSupplement-1 Operation On

Contaminated Runways

07-01-00-01 thru 07-01-00-04...... 2 All07-01-00-05 ................................... 1 All07-01-00-06 thru 07-01-00-09...... 2 All07-01-01-01 thru 07-01-01-05...... 2 All07-01-11-01 ................................... 1 All07-01-11-02 thru 07-01-11-12 ...... 2 All07-01-11-13 and 07-01-11-14....... 1 All07-01-12-01 ................................... 1 All07-01-12-02 thru 07-01-12-12...... 2 All07-01-12-13 and 07-01-12-14 ...... 1 All07-01-13-01 ................................... 1 All07-01-13-02 thru 07-01-13-14...... 2 All07-01-14-01 ................................... 1 All07-01-14-02 thru 07-01-14-12...... 2 All07-01-14-13 ................................... 1 All07-01-14-14 thru 07-01-14-26...... 2 All07-01-15-01 thru 07-01-15-26...... 2 All07-01-21-01 ................................... 1 All07-01-21-02 thru 07-01-21-12...... 2 All07-01-21-13 and 07-01-21-14 ...... 1 All07-01-22-01 ................................... 1 All07-01-22-02 thru 07-01-22-12...... 2 All07-01-22-13 and 07-01-22-14 ...... 1 All07-01-23-01 ................................... 1 All07-01-23-02 thru 07-01-23-14...... 2 All07-01-24-01 ................................... 1 All07-01-24-02 thru 07-01-24-12...... 2 All07-01-24-13 ................................... 1 All07-01-24-14 thru 07-01-24-26...... 2 All07-01-25-01 thru 07-01-25-26...... 2 All07-01-31-01 ................................... 1 All07-01-31-02 ................................... 2 All07-01-31-03 ................................... 4 All07-01-32-01 thru 07-01-32-03...... 2 All07-01-33-01 thru 07-01-33-03...... 2 All07-01-34-01 thru 07-01-34-03...... 2 All





Supplement-2 Supplemental Informationfor the MMEL

07-02-00-01 ................................... 4 All07-02-01-01 ................................... 4 All07-02-01-02 thru 07-02-01-11 ...... 1 All07-02-01-12 thru 07-02-01-14...... 4 All

Supplement-3 Category II Operations

07-03-00-01 ................................... 4 All07-03-01-01 thru 07-03-01-07...... 4 All

Appendices

08-00-01......................................... 1 AllAppendix-1 Configuration Deviation List (CDL)

08-01-00-01 ................................... 1 All08-01-01-01 ................................... 1 All

*08-01-02-01 .................................. 10 All08-01-23-01 ................................... 1 All08-01-27-01 ................................... 3 All08-01-32-01 ................................... 3 All08-01-33-01 ................................... 3 All08-01-51-01 ................................... 3 All08-01-52-01 ................................... 3 All08-01-53-01 ................................... 3 All08-01-55-01 ................................... 3 All08-01-57-01 and 08-01-57-02....... 3 All08-01-78-01 ................................... 1 All


INTRODUCTION

TABLE OF CONTENTS

DOT Approved May 30/2003 Airplane Flight Manual 01-00-01CSP 100-1

7/1/04

GENERAL 01-01-01

The Manual ..................................................................... 01-01-01Revising The Manual ...................................................... 01-01-02Temporary Revisions ..................................................... 01-01-02Numbered Revisions ...................................................... 01-01-02Performance Data .......................................................... 01-01-03Notes, Cautions, and Warnings ..................................... 01-01-03Manual Conventions ....................................................... 01-01-03Circuit Breakers............................................................... 01-01-04


INTRODUCTION

DOT Approved May 30/2003 Airplane Flight Manual 01-01-01REV 1 CSP 100-1

7/1/04

GENERAL

THE MANUAL

The manual consists of this Introduction and the following seven basic chap-ters (for expanded checklists refer to the Flight Crew OperatingManual Vol. 1):

NOTE: Boldfaced text is used for emphasis or to show priority.

Chapter 1 INTRODUCTION contains information on the use and the statusof this manual.

Chapter 2 LIMITATIONS must be observed during operation of the aircraft,except where a deviation is specifically authorized.

Chapter 3 EMERGENCY PROCEDURES contains the operating proce-dures for use during critical conditions.

Chapter 4 NORMAL PROCEDURES contains the designated operatingprocedures for day-to-day operations.

Chapter 5 NON-NORMAL PROCEDURES contains the designated oper-ating procedures for non-emergency failure conditions.

Chapter 6 PERFORMANCE defines the aircraft performance.

Chapter 7 SUPPLEMENTS supercedes or is in addition to the AFM withinformation that may be the result of a Supplemental Type Certificate, or ap-proved changes to the AFM limitations, procedures or performance without aSupplemental Type Certificate.

Chapter 8 APPENDICES provides additional information required by theinstallation of optional equipment, or for specific operations such as Configu-ration Deviation List etc.

REV 1


INTRODUCTION

01-01-02 Airplane Flight Manual DOT Approved May 30/2003CSP 100-1

7/1/04

REVISING THE MANUAL

Temporary Revisions or Numbered Revisions must be incorporated in themanual as soon as they are received.

TEMPORARY REVISIONS

Temporary Revisions may be issued to facilitate quick transmission of data.Temporary Revisions must be retained in the Flight Manual until removed bysome other authority usually a superseding Temporary Revision or aNumbered Revision.

NUMBERED REVISIONS

Numbered Revisions issued against the Flight Manual differ from TemporaryRevisions in that the pages contained in the Numbered Revision supersede likepages in the Flight Manual.

A vertical bar in the margin indicates a change in content from the previousversion of the Flight Manual. The vertical bars may not appear on pages thatcontain changes to graphs or tables. Additionally, when a changed page isthe result of a rearrangement of material due to a change on a previous page,no vertical bar will appear.


INTRODUCTION

DOT Approved May 30/2003 Airplane Flight Manual 01-01-03CSP 100-1

7/1/04

PERFORMANCE DATA

The performance data in Chapter 6 of this manual provides performance datafor all aircraft with the same model designation rather than performance datafor a specific serial number aircraft. Therefore, due to serial number changesor the incorporation of Service Bulletins, performance charts may be issuedagainst this Flight Manual which are not applicable to the specific aircraftassigned to the Flight Manual. Charts not effective for a particular aircraft maybe removed from the Flight Manual for that aircraft and need not be retained.The airplane effectivity of each chart is listed on the page containing the chartand in the List of Effective Pages.

NOTES, CAUTIONS, AND WARNINGS

NOTE: Notes highlight specific operating conditions or steps of a proce-dure.

CAUTION: Cautions call attention to operating procedures which, if notstrictly observed, may result in damage to equipment.

WARNING: Warnings call attention to operating procedures which, if notstrictly adhered to, may result in personal injury or loss oflife.

MANUAL CONVENTIONS

ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS)

EICAS indications will be presented by all capital letters within their appropri-ate display fields. Messages are displayed in the manual to represent the mes-sage as seen in the cockpit. If the message can be either left or right, themessage will be preceded with L (R). CAS messages are followed by theappropriate letter to designate priority of the message: (W) for warning, (C) forcaution, (A) for advisory, and (S) for status messages.


INTRODUCTION

01-01-04 Airplane Flight Manual DOT Approved May 30/2003CSP 100-1

7/1/04

CIRCUIT BREAKERS

Circuit breakers will be identified by their name R DC PUMP and the loca-tion on the circuit breaker panel CB1 A7.

CB1 A7

Circuit breaker panel Row Column

Panel Panel locationCB1 behind pilots seatCB2 behind copilots seatCB3 left avionics rackCB4 right avionics rackCB5 left aft equipment bayCB6 right aft equipment bay

If a circuit breaker trips, it may not be reset, unless recovering the effectedfunction is absolutely required for flight.


LIMITATIONS

TABLE OF CONTENTS

DOT Approved Jul 31/2006 Airplane Flight Manual 02-00-01REV 6 CSP 100-1

9/25/06

GENERAL 02-01-01BASIC LIMITATIONS 02-01-01

Kinds of Operation ......................................................... 02-01-01Minimum Flight Crew ..................................................... 02-01-03

WEIGHT AND C.G. LIMITATIONS 02-02-01Maximum Ramp Weight.................................................. 02-02-01Maximum Certified Takeoff Weight ................................. 02-02-01Maximum Certified Landing Weight ................................ 02-02-01Maximum Zero Fuel Weight ............................................ 02-02-01Minimum Flight Weight.................................................... 02-02-01CENTER-OF-GRAVITY (Fig. 02-02-01) ......................... 02-02-02CENTER-OF-GRAVITY (Fig. 02-02-02) ......................... 02-02-03

SPEED LIMITATIONS 02-03-01Maximum Operating Speed VMO/MMO............................ 02-03-01Maneuvering Speed (VA)................................................. 02-03-01Rough Air Penetration Speed (VRA)................................ 02-03-01Maximum Landing Gear Operating

Speed Retraction (VLO RET) ......................................... 02-03-01Maximum Landing Gear Operating

Speed Extension (VLO EXT) .......................................... 02-03-01Maximum Landing Gear Extended Speed (VLE) ............. 02-03-01Maximum Flap Extended Speed (VFE) ........................... 02-03-01Minimum Operating Speed ............................................. 02-03-02Tire Speed ...................................................................... 02-03-02AIRSPEED/MACH LIMITATIONS (Fig. 02-03-01) .......... 02-03-02

OPERATIONAL LIMITATIONS 02-03-03Takeoff and Landing ....................................................... 02-03-03Cold Weather Operations................................................ 02-03-04En Route ........................................................................ 02-03-05Maneuvering Load Factors ............................................ 02-03-05Operation with Type II, III, & IV Anti-Icing Fluids............. 02-03-05Maneuvers ...................................................................... 02-03-05ALTITUDE/TEMPERATURE

LIMITATIONS (Fig. 02-03-02) ..................................... 02-03-06

REV 6 For Training Purposes Only

LIMITATIONS

TABLE OF CONTENTS

02-00-02 Airplane Flight Manual DOT Approved Jul 31/2006CSP 100-1 REV 6

9/25/06

SYSTEMS LIMITATIONS 02-04-01Air Conditioning and Pressurization ................................02-04-01Autoflight .........................................................................02-04-01Avionics ..........................................................................02-04-02Electrical .........................................................................02-04-07Flight Controls .................................................................02-04-08Hydraulics........................................................................02-04-08Landing Gear, Wheels & Brakes .....................................02-04-08

FUEL LIMITATIONS 02-05-01Minimum Takeoff Fuel.....................................................02-05-01Approved Fuels ..............................................................02-05-01Approved Fuel Additives .................................................02-05-01Fueling ............................................................................02-05-01Fuel Transfer Systems ....................................................02-05-01Usable Fuel Load ............................................................02-05-02Gravity Refuel..................................................................02-05-02Minimum Fuel Quantity For Go-Around ..........................02-05-02Maximum Fuel Imbalance ...............................................02-05-02Temperature Limitations..................................................02-05-02

POWERPLANT LIMITATIONS 02-06-01Engine Type ...................................................................02-06-01Engine Operation ...........................................................02-06-01ENGINE OPERATING LIMITATIONS (Fig. 02-06-01) ....02-06-01GROUND START ENVELOPE (Fig. 02-06-02) ..............02-06-02Oil ....................................................................................02-06-02Thrust Reversers.............................................................02-06-02

AUXILIARY POWER UNIT (APU) LIMITATIONS 02-06-03APU Type ........................................................................02-06-03Maximum Altitude............................................................02-06-03APU Start ........................................................................02-06-03APU Operation ................................................................02-06-03Approved Fuels/Oils ........................................................02-06-03


LIMITATIONS


12/12/07

GENERAL

Observance of the limitations in this Airplane Flight Manual is mandatory.

BASIC LIMITATIONS

KINDS OF OPERATION

This airplane is certificated to the applicable regulations in the transport cate-gory and is eligible for the following kinds of operations when the appropriateinstruments and equipment required by the airworthiness and operating re-quirements are installed and approved and are operable.

This airplane is approved for:

- VMC (Visual Meteorological Conditions)- IMC (Instrument Meteorological Conditions)- Day- Night- Icing

The airplane is certified capable of RVSM operations in accordance with theFAA Interim guidance material on the approval of operations/aircraft forRVSM operations. 91-RVSM, dated June 30, 1999 and the JAA TemporaryGuidance Leaflet, TGL No.6, revision 1, RVSM.

NOTE: Compliance with the material above does not constitute an opera-tional approval.

RVSM operations must not be commenced or continued unless all of therequired equipment specified below is operational:

Compliance with AC 90-100A U.S. TERMINAL AND EN ROUTE AREANAVIGATION (RNAV) OPERATIONS

When equipped with an operating FMS and GPS, the aircraft meets thefunctional and the +/- 1 nm accuracy requirements of AC 90-100A, U.S. Ter-minal and En Route Area Navigation (RNAV) Operations.

NOTE: Compliance with the material above does not constitute an opera-tional approval.

RVSM Required Equipment ListEquipment Requirements for RVSM

Autopilot (1) Must be operational.Altitude Alerting System Must be operational.

Altitude Reporting Transponder (2) One must be operationalAir Data Computers (2) Two must be operational

REV 10 For Training Purposes Only

LIMITATIONS


11/30/07

OPERATION IN ICING CONDITIONS

Do not hold in icing conditions with flaps extended.

Super-Cooled Large Droplet Icing:

Flight in super-cooled large droplet icing (SLD) conditions may, but not nec-essarily be indicated by ice accretion on the side windows.

When side window icing is observed:

- Wing and engine anti-icing systems must be on.- Leave icing conditions as soon as possible.

Engine Anti-Ice Systems:

Ground operations. The engine anti-icing system must be ON when theoutside air temperature (OAT) on the ground and for takeoff is 10 C (50 F)or below and visible moisture in any form is present (such as fog with visibilityof one mile (1500 m) or less, rain, snow, sleet, or ice crystals).

The engine anti-icing system must also be ON when the OAT is 10 C (50 F)or below when operating on ramps, taxiways, or runways where surface snow,ice, standing water, or slush is present.

Flight operations. Icing conditions exist when the static air temperature(SAT) in flight is 10 C (50 F) to -40 C (-40 F) and visible moisture in anyform is present (such as clouds, rain, snow, sleet, or ice crystals).

The engine anti-icing system must be ON when the ICE DETECTED CASmessage is on, or in icing conditions.

Wing Anti-Ice System:

Ground operations. The wing anti-icing system must be ON for takeoff whenthe OAT is 5 C (41 F) or below and visible moisture in any form is present(such as fog with visibility of one mile (1500 m) or less, rain, snow, sleet, orice crystals).

The wing anti-icing system must also be ON when the OAT is 5 C (41 F) orbelow when operating on ramps, taxiways, or runways where surface snow,ice, standing water, or slush is present.

REV 8


ACTION

Insert this temporary revision in front of page 020103 in the LIMITATIONSchapter of the Airplane Flight Manual.

INSTRUCTIONS: Add the following new paragraph before MINIMUM FLIGHT CREW:

APPROACHES

Operations with a glidepath angle of 4.5 degrees or greater is prohibited. Operationswith glidepath angles exceeding that shown in Figure 020101 are prohibited.

CF

M02

01_0

01

Figure 020101

LIMITATIONS

TEMPORARY REVISION TR-47

To address glidepath limits, and provide data for approaches between 3.5 and4.5 degrees.

DOT Approved May 06/2008

TR47


CSP 1001

REASON FOR ISSUE

Temporary revision to advise the crew of the following:


LIMITATIONS


4/18/07

Flight operations. Icing conditions exist when the (SAT) in flight is 10 C(50 F) to -40 C (-40 F) and visible moisture in any form is present (such asclouds, rain, snow, sleet, or ice crystals).

COLD WEATHER OPERATIONS

Airplane operations in cold weather conditions must be conducted in accor-dance with the Flight Crew Operating Manual - Volume 1, Supplement 1 -COLD WEATHER OPERATIONS.

DITCHING

This airplane is certified for ditching when the appropriate safety equipment isinstalled per applicable regulations.

MINIMUM FLIGHT CREWThe minimum flight crew shall consist of a pilot and a copilot.

For aircraft 20001 thru 20143 not incorporating Service Bulletin 100-30-04the following applies:

The wing anti-icing system must also be ON when:

- the ICE DETECTED CAS message is on, OR- in icing conditions.

EFFECTIVITY

For aircraft 20144 and subsequent, and aircraft 20001 thru 20143 incorpo-rating Service Bulletin 100-30-04 the following applies:

The wing anti-icing system must also be ON when:

- the ICE DETECTED CAS message is on, OR- in icing conditions and the airspeed is less than 210 KIAS.

EFFECTIVITY


LIMITATIONS

DOT Approved Dec 09/2004 Airplane Flight Manual 02-02-01REV 2 CSP 100-1

2/22/05

WEIGHT AND C.G. LIMITATIONSMAXIMUM RAMP WEIGHT ................................................... 38 650 lb

17 532 kg

MAXIMUM CERTIFIED TAKEOFF WEIGHT ......................... 38 500 lb17 463 kg

MAXIMUM ZERO FUEL WEIGHT ......................................... 26 100 lb11 839 kg

On aircraft 20051 and subsequent, and aircraft incorporating Service Bulletin100-11-01 (Replacement of Airspeed Limits Placard for MTOW Increase to38 850 lb/17 622 kg), the following weights are applicable:

MAXIMUM RAMP WEIGHT ................................................... 39 000 lb17 690 kg

MAXIMUM CERTIFIED TAKEOFF WEIGHT ......................... 38 850 lb17 622 kg

MAXIMUM ZERO FUEL WEIGHT ......................................... 27 000 lb12 247 kg

MAXIMUM CERTIFIED LANDING WEIGHT ......................... 33 750 lb15 309 kg

MINIMUM FLIGHT WEIGHT .................................................. 23 100 lb10 478 kg

All weights in excess of Maximum Zero Fuel Weight must consist of fuel.

The Maximum Takeoff Weight (MTOW) and/or Maximum Landing Weight(MLW) may be further limited due to performance considerations.

EFFECTIVITY

REV 2For Training Purposes Only

LIMITATIONS

02-02-02 Airplane Flight Manual DOT Approved Dec 09/2004CSP 100-1 REV 2

2/22/05

CENTER-OF-GRAVITY

The center of gravity of the airplane for all flight conditions must be main-tained within the applicable CENTER-OF-GRAVITY ENVELOPE below. Forspecific details on the Center of Gravity Envelope, refer to the Weight & Bal-ance Manual CH 300 WBM.

NOTE: The airplane must be loaded in accordance with the loading instruc-tions associated with the weight and balance manual CH300 WBM.The effect of landing gear retraction on the CG position isnegligible.

Figure 02-02-01

22000

24000

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20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45

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MRW 38 650 lb (17 532 kg)MTOW 38 500 lb (17 463 kg)

MLW 33 750 lb (15 309 kg)

MZFW 26 100 lb (11 839 kg)

MFW 23 100 lb (10 478 kg)

EFFECTIVITYFor aircraft 20002 thru 20050 not incorporating Service Bulletin 100-11-01(Replacement of Airspeed Limits Placard for MTOW Increase to 38 850 lb/17 622 kg), Figure 02-02-01 is applicable.


LIMITATIONS

DOT Approved Dec 09/2004 Airplane Flight Manual 02-02-03REV 2 CSP 100-1

2/22/05

Figure 02-02-02

22000

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MRW 39 000 lb (17 690 kg)

MTOW 38 850 lb (17 622 kg)

MLW 33 750 lb (15 309 kg)

MZFW 27 000 lb (12 247 kg)

MFW 23 100 lb (10 478 kg)MFW 23 100 lb (10 478 kg)

EFFECTIVITYFor aircraft 20051, and subsequent, and aircraft incorporating Service Bulletin100-11-01 (Replacement of Airspeed Limits Placard for MTOW Increase to38 850 lb/17 622 kg), Figure 02-02-02 is applicable.


LIMITATIONS

DOT Approved May 30/2003 Airplane Flight Manual 02-03-01REV 1 CSP 100-1

7/1/04

SPEED LIMITATIONS

MAXIMUM OPERATING SPEED (VMO/MMO)

VMO (up to 8000 ft) ...................................................................................... 300 KIAS

VMO (8001 to 29 475 ft)............................................................... 320 KIAS

MMO (Above 29 475 ft) ....................................................................0.83 MI

VMO/MMO may not be deliberately exceeded in any regime of flight (climb,cruise, or descent), unless a higher speed is specifically authorized for flighttest or training operations.

MANEUVERING SPEED (VA)

VA is the highest speed that full roll and yaw control can be applied withoutoverstressing the aircraft. Full application of rudder and aileron controls aswell as maneuvers that involve angles of attack near the stall, must be confinedto speeds below VA.

Refer to the applicable figure titled Airspeed/Mach Limitations in this sectionfor VA.

CAUTION: Rapid and large alternating control inputs, especially in com-bination with large changes in pitch, roll, or yaw (e.g. largesideslip angles) may result in structural failures at any speed,even including below VA.

ROUGH AIR PENETRATION SPEED (VRA)

VRA .................................................................................................. 265 KIAS/0.75 MI

MAXIMUM LANDING GEAR OPERATING SPEED RETRACTION

VLO RET...................................................................................... 200 KIAS

MAXIMUM LANDING GEAR OPERATING SPEED EXTENSION

VLO EXT...................................................................................... 250 KIAS

MAXIMUM LANDING GEAR EXTENDED SPEED (VLE)

VLE ............................................................................................. 250 KIAS

MAXIMUM FLAP EXTENDED SPEED (VFE)

VFE- Flaps 10 ................................................................................ 210 KIAS- Flaps 20 ................................................................................ 210 KIAS- Flaps 30 ................................................................................ 175 KIAS

REV 1


LIMITATIONS

02-03-02 Airplane Flight Manual DOT Approved Dec 09/2004CSP 100-1 REV 2

2/22/05

SPEED LIMITATIONS (Cont)

MINIMUM OPERATING SPEED

Intentional speed reduction below the onset of stall warning, as defined bystick shaker operation, is prohibited unless a lower speed is specifically autho-rized for flight test or training operations.

TIRE SPEED

Maximum tire speed (ground speed) ....................................................182 kts.

AIRSPEED/MACH LIMITATIONS(PRIMARY PITOT-STATIC SYSTEM)

Figure 02-03-01

SPDENV_BD100_10FEB04

100 125 150 175 200 225 250 275 300 325 350INDICATED AIRSPEED KNOTS

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NOTE:

1.0 lb = 0.4536 kg

REV 2


LIMITATIONS


9/12/06

OPERATIONAL LIMITATIONS

TAKEOFF AND LANDING

Maximum takeoff and landing pressure altitude..........................10 000 ftMaximum tailwind component .........................................................10 kts

Takeoffs and Landings are limited to paved runways.

The maximum runway slopes approved for takeoff and landing are +2% uphilland -2% downhill.

For aircraft on the State Aviation Administration of Ukraine (SAAU) registry:

MAXIMUM CROSSWIND COMPONENT - DRY RUNWAYS

The maximum crosswind component for takeoff is 28 knots (14 meters/sec).The maximum crosswind component for landing is 24 knots (12 meters/sec).

MAXIMUM CROSSWIND COMPONENT - WET RUNWAYS

The maximum crosswind component for takeoff and landing on a wet runwaywith water depth no more than 3.00 mm (0.125 inch) is defined in the follow-ing table for different values of the coefficient of friction:

1. Operation on runways with a coefficient of friction less than 0.3 isprohibited.

MAXIMUM CROSSWIND COMPONENT -CONTAMINATED RUNWAYS

1. The maximum crosswind component for takeoff and landing on acontaminated runway is 10 knots (5 meters/sec).


Reported RunwayCoefficient of Friction

Maximum CrosswindComponent

0.3 (poor braking) 10 knots (5 meters/sec)

0.4 (average braking) 15 knots (8 meters/sec)

0.5 (good braking, equivalent to dry) Takeoff - 28 knots (14 meters/sec)Landing - 24 knots (12 meters/sec)

EFFECTIVITY

REV 6


LIMITATIONS


9/12/06

OPERATIONAL LIMITATIONS (Cont)

TAKEOFF AND LANDING (Cont)

COLD WEATHER OPERATIONS

1. Takeoff is prohibited with frost, ice, snow, or slush adhering to anycritical surface (wings, horizontal stabilizer, vertical stabilizer, controlsurfaces, engine inlets, and upper surface of the fuselage).

WARNING: Even small amounts of frost, ice, snow or slush on the wingleading edges and forward upper wing surface may adverselychange the stall speeds, stall characteristics, and the protec-tion provided by the stall protection system, which may resultin loss of control on takeoff.

(Continued)

For aircraft on the Russian Federation (RF) and Commonwealth ofIndependent States (CIS) countries registry:

MAXIMUM CROSSWIND COMPONENT - DRY RUNWAYS

The maximum crosswind component for takeoff is 28 knots (14 meters/sec).The maximum crosswind component for landing is 24 knots (12 meters/sec).

MAXIMUM CROSSWIND COMPONENT - WET RUNWAYS

The maximum crosswind component for takeoff and landing on a wet run-way with water depth no more than 3.00 mm (0.125 inch) is defined in thefollowing table for different values of the coefficient of friction:


MAXIMUM CROSSWIND COMPONENT -CONTAMINATED RUNWAYS

1. The maximum crosswind component for takeoff and landing on acontaminated runway is 10 knots (5 meters/sec).


Reported RunwayCoefficient of Friction

Maximum CrosswindComponent

0.3 - 0.35 (Poor braking) 10 knots (5 meters/sec)0.35 - 0.5 (Medium braking) 15 knots (8 meters/sec)

0.5 - 0.6 (Good braking,equivalent to dry)

Takeoff - 28 knots (14 meters/sec)Landing - 24 knots (12 meters/sec)

EFFECTIVITY


LIMITATIONS


9/25/06

OPERATIONAL LIMITATIONS (Cont)COLD WEATHER OPERATIONS (Cont)

NOTE: - Comprehensive procedures for operating in cold weather areprovided in the Flight Crew Operating Manual, Supplement 1 -Cold Weather Operations.

- Takeoff is permitted with frost adhering to the underside of thewing that is caused by cold soaked fuel, in accordance with theinstructions provided in the Flight Crew Operating Manual,Supplement 1 - Cold Weather Operations.

EN ROUTEMaximum Pressure Altitude ........................................................45 000 ft

MANEUVERING LOAD FACTORSFlaps Up .............................................................................+2.6 g to -1.0 gFlaps Extended.................................................................. +2.0 g to 0.0 g

OPERATION WITH TYPE II, III & IV ANTI-ICING FLUIDSWhen Type II, III & IV anti-icing fluids have been applied:The wing anti-ice system must only be selected ON, if required, just prior tothrust increase for takeoff.

MANEUVERSAerobatic maneuvers and spins are prohibited.


LIMITATIONS


9/25/06

OPERATIONAL LIMITATIONS (Cont)ALTITUDE/TEMPERATURE LIMITATIONS

Figure 02-03-02

ALTENV_BD100_30OCT02

80 70 60 50 40 30 20 10 0 10 20 30 40 50 60TEMPERATURE oC

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For aircraft 20006 thru 20033 not incorporating Service BulletinSB100-52-05 (Replacement of Passenger Door Telescopic Struts forImproved Cold Weather Operation):

Operation is prohibited if the airplane, with engines shut down, is exposed toa ground ambient temperature of -20 C (-4 F) or below for a period of morethan 2 hours, unless an approved procedure is used to warm the airplanefollowing this exposure.

EFFECTIVITY


ACTION

Insert this temporary revision in front of page 020401 in the LIMITATIONSchapter of the Airplane Flight Manual.

INSTRUCTIONS: Replace AUTOFLIGHT with the following paragraph:

AUTOFLIGHT

Do not intentionally overpower the autopilot.

Autopilot Minimum Use Height:

Climb, En Route, or Descent ..................................................................... 700 feet AGL

Approach

Precision with glidepath angle of 3.5 degrees or less ............................80 feet AGL

Precision with glidepath angle between 3.5 and 4.5 degrees...............160 feet AGL

Visual and non-precision .....................................................................200 feet AGL

The maximum altitude with yaw damper off is 31 000 ft.

LIMITATIONS

TEMPORARY REVISION TR-47

To address glidepath limits, and provide data for approaches between 3.5 and4.5 degrees.

DOT Approved May 06/2008

TR47


CSP 1001

REASON FOR ISSUE

Temporary revision to advise the crew of the following:


LIMITATIONS


9/25/06

SYSTEMS LIMITATIONSAIR CONDITIONING AND PRESSURIZATIONAIR CONDITIONINGDo not select the AIR SOURCE switch to TRIM AIR ONLY while the aircraftis on the ground.The pack must be operating (APU or engine running and AIR SOURCEswitch NORM or PACK ONLY) when the aircraft electrical power ison (BATTs or EXT PWR On) for more than 30 minutes and the OAT isabove 40 C (104 F).

OXYGEN

The following aircraft certification requirements are in addition to the require-ments of applicable operating rules. The most restrictive requirements (certifi-cation or operating) must be observed.

Crew and passenger oxygen masks are not approved for use above 40 000 feetcabin altitude. Prolonged operation of passenger masks above 25 000 feetcabin altitude is not recommended.

PRESSURIZATIONThe maximum differential pressure on the ground (during taxi) must notexceed 0.1 psi.The maximum differential pressure during landing must not exceed 1.0 psi.The maximum positive differential pressure is 9.4 psi. The maximum negativedifferential pressure is -0.5 psi.

AUTOFLIGHTDo not intentionally overpower the autopilot.Operation with an ILS glidepath angle that exceeds 3.5 degrees is prohibited.Autopilot Minimum Use Height:Climb, En Route, or Descent..................................................... 700 feet AGL.Approach

Precision............................................................................... 80 feet AGL.Visual and non-precision.................................................... 200 feet AGL.

The maximum altitude with yaw damper off is 31 000 ft.

REV 4


LIMITATIONS


9/12/06

SYSTEMS LIMITATIONS (Cont)

AVIONICS

DATALINK (If installed)

The DATALINK is approved for the transmission and receipt of messages thatwill not create an unsafe condition if the message is improperly received. Anunsafe condition may exist if:

The message or part of the message is delayed or not received The message is delivered to the wrong recipient The message content is corrupted

(Continued)


NOTE: Referenced North American or European regulatory material isin compliance with its RF and CIS countries equivalent.

COMMUNICATIONS

Flight in polar regions outside VHF coverage shall be allowed providedforecast is favorable for HF radio waves propagation.

EFFECTIVITY

For aircraft not on the Russian Federation (RF) and Commonwealth ofIndependent States (CIS) countries registry:

Crew actions based on messages such as pre-departure clearance, oceanicclearance, digital automatic terminal information service, weight and bal-ance, take-off data (speeds, trim settings, runway distances) are prohibitedunless the approved operational procedures are used to verify that the mes-sage is received by the intended recipient, that the message is valid, and thatthe content is not corrupted.

For aircraft 20001 thru 20059 not incorporating Service BulletinSB100-34-18:

If the DATALINK system is used for clearances or other flight relatedinformation, the crew must either monitor the DATALINK CDU page orperiodically check the DATALINK CDU page until the reply is receivedand accepted. (Annunciation of incoming Datalink messages is providedonly by the ACTIVE ADVISORY prompt display on DATALINK CDUpages).

EFFECTIVITY

REV 6


LIMITATIONS


9/25/06

SYSTEMS LIMITATIONS (Cont)AVIONICS (Cont)DATALINK (If installed) (Cont)

FLIGHT MANAGEMENT SYSTEM (FMS)Use of the FMS V-speed data is prohibited for temperatures above ISA +33 C.

For aircraft on the Russian Federation (RF) and Commonwealth ofIndependent States (CIS) countries registry:NOTE: Use of DATALINK is not permitted for ATC purposes.

Crew actions based on messages such as digital automatic terminal informa-tion service, weight and balance, take-off data (speeds, trim settings, runwaydistances) are prohibited unless the approved operational procedures areused to verify that the message is received by the intended recipient, that themessage is valid, and that the content is not corrupted.

EFFECTIVITY

For aircraft not on the Russian Federation (RF) and Commonwealth ofIndependent States (CIS) countries registry:

Single FMS- The FMS V-speed data (if installed) is advisory only and must be

verified with AFM data.- V-speed database part number must be verified to be: 815-5961-

002.

Dual FMS (If installed)- The FMS V-speed data (if installed) does not need to be verified with

the AFM, provided two Flight Management Computers are avail-able.

- V-speed database part number must be verified to be: 815-5961-002.

EFFECTIVITY


- The FMS V-speed data (if installed) does not need to be verifiedwith the AFM, provided both Flight Management Computers areavailable.

- V-speed database part number must be verified to be: 815-5961-002.

EFFECTIVITY


LIMITATIONS


9/25/06

SYSTEMS LIMITATIONS (Cont)AVIONICS (Cont)FLIGHT MANAGEMENT SYSTEM (Cont)

The Collins FMS-5000 Flight Management System Operators Guide (Partnumber 523-0780848-00XXXX dated May 15/2004, or later applicableversion) must be immediately available to the flight crew whenever navigationis predicated on the use of the FMS.

The FMS is approved for use with software version [FMC SCID 832-4118-018, or later applicable revision]. The software status in the FMS OperatorsGuide must match that displayed on the equipment.

The performance database part number must be verified to be: 815-5959-002.

FMS range and fuel management information is advisory only.

When the batteries are removed, the FUEL USED on the FMS will indicate thevalue from the previous flight. After re-installing the batteries, the FUELUSED should be manually reset to zero.

To be used for navigation, the FMS must be receiving suitable navigationinformation from the following sources:

One VOR / DME, or Two DMEs, or GPS. If the GPS is the only available sensor, use of the FMS for

navigation is not approved unless the Collins prediction program[832-3443-007, or later applicable version] has been run.

IFR enroute and terminal navigation is prohibited unless the pilot verifies thecurrency of the database or verifies the waypoints for accuracy by reference tocurrent publications.Instrument approaches must be accomplished only in accordance with instru-ment approach procedures that are contained in the FMS database. The data-base must incorporate the current update cycle. The pilot must verify approachwaypoints for accuracy by reference to current publications.

Use of FMS instrument approaches is prohibited unless APPR is annunciatedon the PFD.

(Continued)

For aircraft 20002 thru 20050 not incorporating Service Bulletin 100-11-01(Replacement of Airspeed Limits Placard for MTOW Increase to 38 850 lb/17 622 kg):The performance database part number must be verified as: 815-5959-001.

EFFECTIVITY


LIMITATIONS


4/23/07

SYSTEMS LIMITATIONS (Cont)AVIONICS (Cont)FLIGHT MANAGEMENT SYSTEM (Cont)

Use of VNAV vertical guidance for V-MDA type approach between the finalapproach fix and the missed approach fix is prohibited.

The FMS with inputs from GPS may only be used for approach guidance if thereference co-ordinate data system for the instrument approach is WGS-84 orNAD-83.When the altimeter is adjusted to show the Height Above Ground (QFE) ratherthan sea level, VNAV must not be used.FMS range and fuel management information is advisory only.

CAUTION: - Errors to VNAV defined paths may occur because ofcoding errors in the navigation data base and because ofaltimetry errors. The actual VNAV path may deviate signif-icantly below the intended VNAV path in very coldtemperatures, unless an approved temperature compensa-tion function (if equipped) is used to correct for non-stan-dard temperatures.

- Database coding of VNAV altitudes for approachwaypoints may result in VNAV paths continuing belowMinimum Descent Altitude (MDA), Decision Altitude(DA), or Decision Height (DH), or ending at an altitude toohigh to continue a safe descent to landing. VNAV paths(often called pseudo-glide paths) are not equivalent to anILS glideslope.

- Position along an approach must be verified prior to com-mencement of VNAV descent as displayed by the FMS.The required visual reference must be obtained prior tocommencing descent below published MDAs, DAs, orDHs.

Approval Status:

Provided the FMS is receiving adequate usable signals, the FMS has beendemonstrated capable of and has been shown to meet the performance require-ments for the following operations:

Lateral Navigation VFR/IFR en

Challenger 300 Airplane Flight Manual (Imperial)

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