AFM M2K 005 AIRCRAFT FLIGHT MANUAL 319 112 2K
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- AFM - 12 DEC 17 - GLG - A319-112
- Front Matter
- Preliminary Pages
- APPROVAL DATA
- Preliminary Pages
- TEMPORARY REVISIONS
- ABN - ENG STALL
- Unreliable Airspeed
- (TR 4.02.00/41) - ENG Compressor vane/ENG STALL on ground
- (TR 2.05.00/47) - Non Precision Approaches withOEI
- (TR 2.05.00/67) - Ram Air Turbine (RAT) Flight Testing
- Autoland Databases with Honeywell ADIRU
- MCDL 54-05 Pylon Fairing Seal
- MCDL 78-01 Duct Opening Actuator for CFM Engine
- Abnormal V Alpha Prot
- EMER DESCENT
- Towbarless Operations
- MCDL 52-03 Access Door TO Potable Water Filling and Drainage
- GENERAL
- LIMITATIONS
- Preliminary Pages
- GENERAL
- WEIGHTS AND LOADING
- AIRSPEEDS
- OPERATIONAL PARAMETERS
- 09 TOWING AND TAXIING
- 21 AIR COND/PRESS/VENT
- 22 AUTO FLIGHT SYSTEM
- 24 ELECTRICAL POWER
- 28 FUEL
- 29 HYDRAULIC
- 32 LANDING GEAR
- 34 NAVIGATION
- 46 INFORMATION SYSTEMS
- 49 AUXILIARY POWER UNIT
- 70 POWER PLANT
- EMERGENCY PROCEDURES
- ABNORMAL PROCEDURES
- Preliminary Pages
- GENERAL
- ONE ENGINE INOPERATIVE
- 21 AIR COND/PRESS/VENT
- 22 AUTO FLIGHT SYSTEM
- AUTO FLIGHT SYSTEM
- 22-CATII FAILURES OR WARNINGS DURING A CAT II APPROACH WITH OR WITHOUT AUTOMATIC LANDING
- Multiple Failures or Warnings (CAT II)
- Altitude Loss with Autopilot Malfunction (CAT II)
- Failure Leading to Slats/Flaps less than FLAPS 3 (CAT II)
- Antiskid System and/or Nosewheel Steering Failure(CAT II)
- Alpha Floor Activation (CAT II)
- One Engine Failure (CAT II)
- Red "RA" Flag on two PFDs (CAT II)
- Amber "CHECK ATT" Flag on two PFDs (CAT II)
- Red "ATT" Flag on one PFD (CAT II)
- Diagonal Line or "INVALID DATA" on one PFD and one ND (CATII)
- Amber "CHECK HDG" Flag on two PFDs and on two NDs (CAT II)
- Red "HDG" Flag on one PFD and one ND (CAT II)
- Red "SPD" Flag on one PFD (CAT II)
- "AP OFF" Warning (CAT II)
- Loss of "CAT 2" Capability (CAT II)
- LOC or G/S Excessive Deviation on PFD (CAT II)
- "AUTOLAND" Light (CAT II)
- A/THR Fault (CAT II)
- No "LAND" at 350 ft (CAT II)
- Incorrect Selected Course at 350 ft > 5 deg (CAT II)
- No "FLARE" at 30 ft (CAT II)
- 22-CATIIIDH FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
- Multiples Failures or Warnings (CAT III with DH)
- Failure Leading to Slats/Flaps less than CONF 3 (CAT III withDH)
- Nosewheel Steering Failure (CAT III with DH)
- Antiskid Failure (CAT III with DH)
- Alpha Floor Activation (CAT III with DH)
- One Engine Failure (CAT III with DH)
- Auto Callout RA Failure (CAT III with DH)
- Red "RA" Flag on two PFDs (CAT III with DH)
- Amber "CHECK ATT" Flag on two PFDs (CAT III with DH)
- Red "ATT" Flag on one PFD (CAT III with DH)
- Amber "CHECK HDG" Flag on two PFDs and two NDs (CAT III withDH)
- Red "HDG" Flag on one PFD and one ND (CAT III with DH)
- Red "SPD" Flag on one PFD (CAT III with DH)
- "AP OFF" Warning (CAT III with DH)
- Capability Decrease (Except if due to A/THR Loss) (CAT IIIwith DH)
- Total Loss of A/THR ("CAT 3" Decreases to "CAT 2") (CAT IIIwith DH)
- LOC or G/S Excessive Deviation on PFD (CAT III with DH)
- "AUTOLAND" Light (CAT III with DH)
- No "LAND" at 350 ft (CAT III with DH)
- Incorrect Selected Course at 350 ft > 5 deg (CAT III withDH)
- No "FLARE" at 30 ft (CAT III with DH)
- 22-CATIIInoDH FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
- Multiple Failures or Warnings (CAT III no DH)
- Failure Leading to Slats/Flaps less than CONF 3 (CAT III noDH)
- Nosewheel Steering Failure (CAT III no DH)
- Antiskid Failure (CAT III no DH)
- Alpha Floor Activation (CAT III no DH)
- One Engine Failure (CAT III no DH)
- Auto Callout RA Failure (CAT III no DH)
- Red "RA" Flag on two PFDs (CAT III no DH)
- Amber "CHECK ATT" Flag on two PFDs (CAT III no DH)
- Red "ATT" Flag on one PFD (CAT III no DH)
- Amber "CHECK HDG" Flag on two PFDs and two NDs (CAT III noDH)
- Red "HDG" Flag on one PFD and one ND (CAT III no DH)
- Red "SPD" Flag on one PFD (CAT III no DH)
- "AP OFF" Warnings (CAT III no DH)
- Capability Decrease (Except if due to A/THR Loss)(CAT III no DH)
- Total Loss of A/THR ("CAT 3" Decreases to "CAT 2") (CAT IIIno DH)
- LOC or G/S Excessive Deviation on PFD (CAT III no DH)
- "AUTOLAND" Light (CAT III no DH)
- No "LAND" at 350 ft (CAT III no DH)
- Incorrect Selected Course at 350 ft > 5 deg (CAT III noDH)
- No "FLARE" at 30 ft (CAT III no DH)
- 24 ELECTRICAL POWER
- 27 FLIGHT CONTROLS
- F/CTL - FLAPS FAULT
- F/CTL - FLAPS LOCKED
- F/CTL - SLATS FAULT
- F/CTL - SLATS LOCKED
- APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATIONFACTOR
- PERFORMANCE LIMITATION FOR LANDING IN CLEAN CONFIGURATION
- F/CTL - SPLR FAULT
- F/CTL - GND SPLR FAULT
- F/CTL - SPD BRK DISAGREE
- F/CTL - SPD BRK FAULT
- F/CTL - RUDDER JAM
- F/CTL - STOP RUDDER INPUT
- F/CTL - L (R) ELEV FAULT
- F/CTL - ELAC 1(2) FAULT
- F/CTL - SEC FAULT
- F/CTL - FCDC 1 + 2 FAULT
- F/CTL - STABILIZER JAM
- F/CTL - ATLN LAW (PROT LOST)
- F/CTL - DIRECT LAW (PROT LOST)
- 28 FUEL
- 29 HYDRAULIC
- 30 ICE AND RAIN PROTECTION
- 31 INDICATING/RECORDING SYSTEM
- 32 LANDING GEAR
- 34 NAVIGATION
- 36 PNEUMATIC
- 52 DOORS
- 70 POWER PLANT
- 90 MISCELLANEOUS
- NORMAL PROCEDURES
- PERFORMANCE
- APPENDICES AND SUPPLEMENTS
- MASTER CONFIGURATION DEVIATION LIST
- Preliminary Pages
- GENERAL
- 21 AIR CONDITIONING
- 23 COMMUNICATION
- 27 FLIGHT CONTROL
- 27-01 Flap Track Fairing
- 27-03 Slat Track Closing Plate
- 27-05 Access Panel for Bearings at Elevator
- 27-06 Flap Track Fairing Rear Top Cover and Tail Cone
- 27-07 Rubber Seal under Slat
- 27-08 Seal Between Inboard and Outboard Flap
- 27-09 Inboard Aileron Edge to Wing Seal
- 27-10 Slat End Seal and Weather Seal
- 27-11 Slat Track Filler Block
- 27-12 Slat Track Sealing Packer
- 27-13 Inter-flap Cushion Seal
- 27-14 Flap Track Moveable Fairing Seal
- 27-15 Flap Track Fixed Fairing Seal
- 27-16 Flap Track Moveable Fairing Pivot Cover
- 28 FUEL
- 30 ICE AND RAIN PROTECTION
- 32 LANDING GEAR
- 33 LIGHTS
- 33-01 Wing/Engine Scan light Cover 3LX, 4LX
- 33-02 Taxi Light Lamp 8LR
- 33-03 Rear Navigation Light Lens 15LA
- 33-04 Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light Cover
- 33-05 Logo Light Lens (Cover) 3LY, 4LY
- 33-07 Landing Light Lens 7LB, 8LB
- 33-08 Turn OFF Light Lamp 3LC1, 3LC2
- 33-09 Takeoff Light Lamp 7LR
- 49 APU
- 51 STRUCTURE
- 52 DOORS
- 52-01 Toilet Servicing and Drainage Door
- 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB
- 52-03 Access Door to Potable Water Filling and Drainage
- 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB
- 52-05 Access Door to Air Conditioning Ground Supply 191 CB
- 52-07 External Power Ground Connection Access Door Assy 121 AL
- 52-08 Access Door of Cargo Opening System 134 AR - 154 AR
- 52-09 Nose Landing Gear Main Door (713, 714)
- 52-10 Nose Landing Gear Aft Door (715, 716)
- 52-11 Nose Landing Gear Leg Door (712)
- 52-12 Main Landing Gear Door (732, 742) (flight with gear up)
- 52-13 Main Landing Gear Door (733, 743) (flight with gear up)
- 52-14 Main Landing Gear Door (732, 742) (flight with gear down)
- 52-15 Main Landing Gear Door (733, 743) (Flight with gear down)
- 52-16 Main Landing Gear Door (734, 744) (Flight with gear down)
- 52-18 Main Landing Gear Door : Seal on Secondary Hinged Fairing
- 52-19 Pax Door Upper Cover Plate
- 52-20 Access Door to HP Air Ground Connector 191 DB
- 52-21 Blue Hydraulic Access Door 197 FB
- 52-22 Forward Cargo Door Access Cover Panel 825 AR
- 52-23 Aft Cargo Door Access Cover Panel 826 AR
- 53 FUSELAGE
- 54 NACELLE / PYLON
- 57 WINGS
- 71 POWER PLANT
- 78 EXHAUST
- SUPPLEMENTARY PERFORMANCE
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GLG A319-112 FLEET TRL P 1/2
AFM 12 DEC 17
Issue date: 12 DEC 17
This is the AIRPLANE FLIGHT MANUAL at issue date 12 DEC 17 for the A319-112 and replacing
last issue dated 14 NOV 17
A319
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TRANSMITTAL LETTER
Intentionally left blank
GLG A319-112 FLEET TRL P 2/2
AFM 12 DEC 17
A319
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FILING INSTRUCTIONS
GLG A319-112 FLEET FI P 1/2
AFM 12 DEC 17
Please incorporate this revision as follow:
InsertLocalization
Subsection Title Remove Rev. Date
PLP-LESS
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS ALL 12 DEC 17
PLP-LEDU
LIST OF EFFECTIVE DOCUMENTARY UNITS ALL 12 DEC 17
PLP-LAR
LIST OF APPROVAL REFERENCES ALL 12 DEC 17
APPRO-PLP-TOC
TABLE OF CONTENTS ALL 12 DEC 17
APPRO-PLP-SOH
SUMMARY OF HIGHLIGHTS ALL 12 DEC 17
PERF-PLP-TOC
TABLE OF CONTENTS ALL 12 DEC 17
PERF-PLP-SOH
SUMMARY OF HIGHLIGHTS ALL 12 DEC 17
PERF-OCTO
PERFORMANCE DATABASE ALL 12 DEC 17
MCDL-PLP-TOC
TABLE OF CONTENTS ALL 12 DEC 17
MCDL-PLP-SOH
SUMMARY OF HIGHLIGHTS ALL 12 DEC 17
MCDL-27-01
Flap Track Fairing ALL 12 DEC 17
MCDL-27-03
Slat Track Closing Plate ALL 12 DEC 17
MCDL-27-08
Seal Between Inboard and Outboard Flap ALL 12 DEC 17
MCDL-27-16
Flap Track Moveable Fairing Pivot Cover ALL 12 DEC 17
MCDL-28-01
Refuel/Defuel Coupling Cap 101 QM Or 41 QM ALL 12 DEC 17
MCDL-28-02
Refuel Panel Door 192MB ALL 12 DEC 17
MCDL-33-02
Taxi Light Lamp 8LR ALL 12 DEC 17
MCDL-33-07
Landing Light Lens 7LB, 8LB ALL 12 DEC 17
MCDL-52-05
Access Door to Air Conditioning Ground Supply 191 CB ALL 12 DEC 17
Continued on the following page
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FILING INSTRUCTIONS
GLG A319-112 FLEET FI P 2/2
AFM 12 DEC 17
Continued from the previous page
InsertLocalization
Subsection Title Remove Rev. Date
MCDL-52-21
Blue Hydraulic Access Door 197 FB ALL 12 DEC 17
MCDL-57-01
Wing Tip Fence ALL 12 DEC 17
MCDL-57-02
Belly Fairing Sliding Panel ALL 12 DEC 17
MCDL-57-06
Outer Flap Blade Seal ALL 12 DEC 17
SPERF-PLP-TOC
TABLE OF CONTENTS ALL 12 DEC 17
SPERF-CONT-PERF
PERFORMANCE ALL 12 DEC 17
PRELIMINARY PAGES
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PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET PLP-TOC P 1/2
AFM 07 MAR 17
PLP PRELIMINARY PAGES
TABLE OF CONTENTS
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
LIST OF EFFECTIVE DOCUMENTARY UNITS
LIST OF EFFECTIVE TEMPORARY REVISIONS
LIST OF APPROVAL REFERENCES
LIST OF MODIFICATIONS
APPRO APPROVAL DATA
GEN GENERAL
LIM LIMITATIONS
EMER EMERGENCY PROCEDURES
ABN ABNORMAL PROCEDURES
NORM NORMAL PROCEDURES
PERF PERFORMANCE
APP APPENDICES AND SUPPLEMENTS
MCDL MASTER CONFIGURATION DEVIATION LIST
SPERF SUPPLEMENTARY PERFORMANCE
A319
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TABLE OF CONTENTS
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GLG A319-112 FLEET PLP-TOC P 2/2
AFM 07 MAR 17
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LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
GLG A319-112 FLEET PLP-LESS P 1/6
AFM 12 DEC 17
M(1) Localization Subsection Title Rev. Date
APPRO-TR TEMPORARY REVISIONS 14 NOV 17
GEN-INTR INTRODUCTION 07 FEB 17
GEN-DESC AFM DESCRIPTION 07 FEB 17
GEN-DEF WORDING DEFINITIONS 16 MAR 15
GEN-ABB ABBREVIATIONS 16 MAR 15
GEN-UNIT UNITS 25 JAN 11
GEN-VIEW 3-VIEW DRAWING 08 APR 11
LIM-GEN GENERAL 14 DEC 13
LIM-WGHT WEIGHTS AND LOADING 25 JAN 11
LIM-SPD AIRSPEEDS 25 JAN 11
LIM-OPS OPERATIONAL PARAMETERS 25 JAN 11
LIM-09 TOWING AND TAXIING 30 JUL 15
LIM-21 AIR COND/PRESS/VENT 25 JAN 11
LIM-22-FMS Flight Management System 14 APR 17
LIM-22-FGS Flight Guidance System 10 OCT 17
LIM-24 ELECTRICAL POWER 25 JAN 11
LIM-28 FUEL 12 SEP 17
LIM-29 HYDRAULIC 25 JAN 11
LIM-32 LANDING GEAR 25 JAN 11
LIM-34 NAVIGATION 14 NOV 17
LIM-46 INFORMATION SYSTEMS 25 JAN 11
LIM-49 AUXILIARY POWER UNIT 25 JAN 11
LIM-70 POWER PLANT 13 JUN 17
EMER-GEN GENERAL 08 AUG 17
EMER-21 AIR COND/PRESS/VENT 14 DEC 13
EMER-24 ELECTRICAL POWER 14 DEC 13
EMER-26 FIRE/SMOKE 16 MAR 15
EMER-27 FLIGHT CONTROLS 14 DEC 13
EMER-29 HYDRAULIC 14 DEC 13
EMER-32 LANDING GEAR 25 AUG 15
EMER-34 NAVIGATION 06 JAN 15
EMER-70 POWER PLANT 25 JAN 11
EMER-90 MISCELLANEOUS 12 SEP 17
ABN-GEN GENERAL 08 AUG 17
ABN-OEI-TO TAKEOFF 16 MAR 15
ABN-OEI-LDG APPROACH AND LANDING 14 DEC 13
ABN-21 AIR COND/PRESS/VENT 05 DEC 11
ABN-22-AUTOFLT AUTO FLIGHT SYSTEM 13 JUN 17
ABN-22-CATII FAILURES OR WARNINGS DURING A CAT II APPROACH WITH
OR WITHOUT AUTOMATIC LANDING
25 JAN 11
Continued on the following page
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LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
GLG A319-112 FLEET PLP-LESS P 2/6
AFM 12 DEC 17
Continued from the previous page
M(1) Localization Subsection Title Rev. Date
ABN-22-CATIIIDH FAILURES OR WARNINGS DURING A CAT III APPROACH
WITH DH
25 JAN 11
ABN-22-CATIIInoDH FAILURES OR WARNINGS DURING A CAT III APPROACH
WITH NO DH
14 DEC 13
ABN-24 ELECTRICAL POWER 10 SEP 14
ABN-27 FLIGHT CONTROLS 08 AUG 17
ABN-28 FUEL 10 SEP 14
ABN-29 HYDRAULIC 14 DEC 13
ABN-30 ICE AND RAIN PROTECTION 16 MAR 15
ABN-31 INDICATING/RECORDING SYSTEM 14 DEC 13
ABN-32 LANDING GEAR 10 SEP 14
ABN-34 NAVIGATION 11 JUL 17
ABN-36 PNEUMATIC 10 SEP 14
ABN-52 DOORS 08 APR 11
ABN-70 POWER PLANT 22 SEP 15
ABN-90 MISCELLANEOUS 08 APR 11
NORM-GEN GENERAL 16 MAR 15
NORM-PFLT PREFLIGHT CHECKS 10 OCT 17
NORM-TO TAKEOFF 16 MAR 15
NORM-FLT FLIGHT 07 MAR 17
NORM-LDG APPROACH AND LANDING 25 JAN 11
NORM-22-CONF Demonstrated System Configuration 13 JUN 17
NORM-22-NPA Non Precision Approach 14 DEC 13
NORM-22-PA Precision Approach 16 MAR 15
NORM-28 FUEL 25 JAN 11
NORM-30 ICE AND RAIN PROTECTION 25 JAN 11
NORM-34 NAVIGATION 13 JUN 17
NORM-49 AUXILIARY POWER UNIT 25 JAN 11
PERF-GEN GENERAL 25 JAN 11
PERF-CAL-TO TAKEOFF 25 JAN 11
PERF-CAL-CRU CRUISE (Clean Configuration) 25 JAN 11
PERF-CAL-LDG LANDING 25 JAN 11
PERF-TO TAKEOFF PERFORMANCE 08 APR 11
PERF-FLT IN FLIGHT PERFORMANCE 08 APR 11
PERF-LDG LANDING PERFORMANCE 14 DEC 13
R PERF-OCTO PERFORMANCE DATABASE 12 DEC 17
PERF-ENG ENGINE MANAGEMENT 25 JAN 11
PERF-FLEX REDUCED THRUST TAKEOFF 25 JAN 11
APP-NOI EXTERNAL NOISE 25 JAN 11
Continued on the following page
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LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
GLG A319-112 FLEET PLP-LESS P 3/6
AFM 12 DEC 17
Continued from the previous page
M(1) Localization Subsection Title Rev. Date
APP-TCAS TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 12 JAN 17
APP-INOP DISPATCH WITH INOPERATIVE ITEMS 25 JAN 11
APP-LGDN-GEN GENERAL 25 JAN 11
APP-LGDN-LIM LIMITATIONS 25 JAN 11
APP-LGDN-EMER EMERGENCY PROCEDURES 25 JAN 11
APP-LGDN-ABN ABNORMAL PROCEDURES 25 JAN 11
APP-LGDN-NORM NORMAL PROCEDURES 25 JAN 11
APP-LGDN-PERF PERFORMANCE 25 JAN 11
APP-LGDN-APP APPENDICES AND SUPPLEMENTS 25 JAN 11
APP-INTX-GEN GENERAL 25 JAN 11
APP-INTX-LIM LIMITATIONS 25 JAN 11
APP-INTX-ABN ABNORMAL PROCEDURES 14 DEC 13
APP-INTX-NORM NORMAL PROCEDURES 25 JAN 11
APP-HAO-GEN GENERAL 22 SEP 15
APP-HAO-LIM LIMITATIONS 12 SEP 17
APP-HAO-NORM NORMAL PROCEDURES 22 SEP 15
APP-HAO-PERF PERFORMANCE 22 SEP 15
APP-TAWS TAWS-GPWS 16 MAR 15
APP-NRWY NARROW RUNWAY 08 AUG 17
APP-PFC OPERATIONS ON WET GROOVED/PFC RUNWAYS 25 JAN 11
MCDL-GEN-INTR Introduction 10 OCT 17
MCDL-GEN-LIM Limitations 25 JAN 11
MCDL-GEN-PERF Performance 16 MAR 15
MCDL-21-01 Ram Air Inlet Flap 25 JAN 11
MCDL-21-03 Ram Air Inlet Leading Edge 25 JAN 11
MCDL-23-01 Static Discharger 09 JUL 14
R MCDL-27-01 Flap Track Fairing 12 DEC 17
R MCDL-27-03 Slat Track Closing Plate 12 DEC 17
MCDL-27-05 Access Panel for Bearings at Elevator 25 JAN 11
MCDL-27-06 Flap Track Fairing Rear Top Cover and Tail Cone 14 DEC 13
MCDL-27-07 Rubber Seal under Slat 14 DEC 13
R MCDL-27-08 Seal Between Inboard and Outboard Flap 12 DEC 17
MCDL-27-09 Inboard Aileron Edge to Wing Seal 25 JAN 11
MCDL-27-10 Slat End Seal and Weather Seal 03 MAY 16
MCDL-27-11 Slat Track Filler Block 25 JAN 11
MCDL-27-12 Slat Track Sealing Packer 25 JAN 11
MCDL-27-13 Inter-flap Cushion Seal 25 JAN 11
MCDL-27-14 Flap Track Moveable Fairing Seal 14 DEC 13
MCDL-27-15 Flap Track Fixed Fairing Seal 14 DEC 13
Continued on the following page
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PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
GLG A319-112 FLEET PLP-LESS P 4/6
AFM 12 DEC 17
Continued from the previous page
M(1) Localization Subsection Title Rev. Date
R MCDL-27-16 Flap Track Moveable Fairing Pivot Cover 12 DEC 17
R MCDL-28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM 12 DEC 17
R MCDL-28-02 Refuel Panel Door 192MB 12 DEC 17
MCDL-30-01 Icing Indicator 25 JAN 11
MCDL-32-03 Nose Wheel Hubcap 14 DEC 13
MCDL-32-04 Nose Fitting Towing 14 DEC 13
MCDL-33-01 Wing/Engine Scan light Cover 3LX, 4LX 14 DEC 13
R MCDL-33-02 Taxi Light Lamp 8LR 12 DEC 17
MCDL-33-03 Rear Navigation Light Lens 15LA 14 DEC 13
MCDL-33-04 Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light Cover 14 DEC 13
MCDL-33-05 Logo Light Lens (Cover) 3LY, 4LY 14 DEC 13
R MCDL-33-07 Landing Light Lens 7LB, 8LB 12 DEC 17
MCDL-33-08 Turn OFF Light Lamp 3LC1, 3LC2 14 DEC 13
MCDL-33-09 Takeoff Light Lamp 7LR 14 DEC 13
MCDL-49-01 APU Overpressure Release Door 25 JAN 11
MCDL-51-02 Passenger Door Scuff Plate 25 JAN 11
MCDL-51-04 Fairing Aft Safety Stay Point 311 AL 25 JAN 11
MCDL-52-01 Toilet Servicing and Drainage Door 07 FEB 17
MCDL-52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB
11 JUL 17
MCDL-52-03 Access Door to Potable Water Filling and Drainage 30 JUL 15
MCDL-52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB
16 MAR 15
R MCDL-52-05 Access Door to Air Conditioning Ground Supply 191 CB 12 DEC 17
MCDL-52-07 External Power Ground Connection Access Door Assy 121 AL 10 OCT 17
MCDL-52-08 Access Door of Cargo Opening System 134 AR - 154 AR 25 JAN 11
MCDL-52-09 Nose Landing Gear Main Door (713, 714) 14 DEC 13
MCDL-52-10 Nose Landing Gear Aft Door (715, 716) 14 DEC 13
MCDL-52-11 Nose Landing Gear Leg Door (712) 14 DEC 13
MCDL-52-12 Main Landing Gear Door (732, 742) (flight with gear up) 14 DEC 13
MCDL-52-13 Main Landing Gear Door (733, 743) (flight with gear up) 14 DEC 13
MCDL-52-14 Main Landing Gear Door (732, 742) (flight with gear down) 14 DEC 13
MCDL-52-15 Main Landing Gear Door (733, 743) (Flight with gear down) 14 DEC 13
MCDL-52-16 Main Landing Gear Door (734, 744) (Flight with gear down) 14 DEC 13
MCDL-52-18 Main Landing Gear Door : Seal on Secondary Hinged Fairing 25 JAN 11
MCDL-52-19 Pax Door Upper Cover Plate 25 JAN 11
MCDL-52-20 Access Door to HP Air Ground Connector 191 DB 16 MAR 15
R MCDL-52-21 Blue Hydraulic Access Door 197 FB 12 DEC 17
MCDL-52-22 Forward Cargo Door Access Cover Panel 825 AR 14 DEC 13
Continued on the following page
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LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
GLG A319-112 FLEET PLP-LESS P 5/6
AFM 12 DEC 17
Continued from the previous page
M(1) Localization Subsection Title Rev. Date
MCDL-52-23 Aft Cargo Door Access Cover Panel 826 AR 01 SEP 16
MCDL-53-01 Belly Fairing Vent Louver Vane 16 MAR 15
MCDL-53-03 Root Fillet Fairing 14 DEC 13
MCDL-54-01 Nacelle Strake 16 MAR 15
MCDL-54-03 Pylon Pressure Relief Door 413(423) BL - 414(424) BR 14 DEC 13
MCDL-54-04 Pylon Access Door 415(425) AL - 415(425) AR 25 JAN 11
MCDL-54-05 Pylon Fairing Seal 19 NOV 14
MCDL-54-06 Aerodynamic Seal 14 DEC 13
R MCDL-57-01 Wing Tip Fence 12 DEC 17
R MCDL-57-02 Belly Fairing Sliding Panel 12 DEC 17
MCDL-57-03 Outboard Flaps Rubbing Strip 25 JAN 11
MCDL-57-04 Inboard Flap Rubbing Strip 14 DEC 13
R MCDL-57-06 Outer Flap Blade Seal 12 DEC 17
MCDL-71-01 Frangible Drain Mast 14 DEC 13
MCDL-71-09 Fan Cowl Hold Open Rod 01 DEC 16
MCDL-78-01 Duct Opening Actuator 14 APR 15
MCDL-78-09 Thrust Reverser 11 and 1 O'clock Struts 14 DEC 13
MCDL-78-11 Thrust Reverser Lockout Fairing 16 MAR 15
SPERF-CONT-GEN GENERAL 25 JAN 11
SPERF-CONT-LIM LIMITATIONS 08 APR 11
R SPERF-CONT-PERF PERFORMANCE 12 DEC 17
(1) Evolution code : N=New, R=Revised, E=Effectivity, M=Moved
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APPROVED
M(1) Localization T(2) DU Title DU identification DU date
R PLP-LEDU List of Effective Documentary Units 12 DEC 17
Approved by Airbus under the authority of DOA ref.
EASA. 21J.031
APPRO-HEAD Heading Approbation A319-112 00007334.0006001 09 APR 96
Approval reference: . Approved by
Criteria: 319-112
Applicable to: MSN 1882, 2078
APPRO-TR x ABN - ENG STALL 00016179.0001001 03 SEP 15
Approval reference: 10054650 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x Unreliable Airspeed 00009810.0003001 11 FEB 16
Approval reference: 10056693 Approved by EASA
Criteria: (A318 or 319-100 or 320-200 or 321-100 or 321-200)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x (TR 4.02.00/41) - ENG Compressor
vane/ENG STALL on ground
00009728.0001001 21 OCT 09
Approval reference: 10027686 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x (TR 2.05.00/47) - Non Precision
Approaches with OEI
00009667.0001001 23 NOV 09
Approval reference: 10027986 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x (TR 2.05.00/67) - Ram Air Turbine (RAT)
Flight Testing
00009670.0001001 23 NOV 09
Approval reference: 10027986 Approved by EASA
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x Autoland Databases with Honeywell
ADIRU
00014157.0003001 04 NOV 15
Approval reference: 10055306 Approved by EASA
Criteria: (SA and (30652 or 30941 or 30942 or 31105 or 31706))
Applicable to: MSN 1882, 2078
Impacted DU: NONE
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AFM 12 DEC 17
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APPRO-TR x MCDL 54-05 Pylon Fairing Seal 00015738.0001001 29 OCT 14
Approval reference: 10050974 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x MCDL 78-01 Duct Opening Actuator for
CFM Engine
00016021.0003001 20 MAR 15
Approval reference: 10052671 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x Abnormal V Alpha Prot 00016062.0001001 05 DEC 14
Approval reference: 10051494 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x EMER DESCENT 00016716.0001001 07 OCT 15
Approval reference: 10055034 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x Towbarless Operations 00016598.0001001 09 JUL 15
Approval reference: 10053997 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
APPRO-TR x MCDL 52-03 Access Door TO Potable
Water Filling and Drainage
00016654.0001001 06 JUL 15
Approval reference: 10053953 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
GEN-INTR Introduction 00007010.0001001 16 JAN 17
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Approved AFM Format 00015195.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
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M(1) Localization T(2) DU Title DU identification DU date
GEN-DESC Customized AFM 00007013.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Organization of the Manual 00007015.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Documentary Unit (DU) 00007016.0001001 16 JAN 17
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Identification Strip 00007017.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Approval Information 00020434.0001001 16 JAN 17
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC AFM Revision 00007366.0001001 16 JAN 17
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DESC Temporary Revision (TR) 00007018.0001001 16 JAN 17
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DEF Warning Definition 00007020.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DEF Caution Definition 00007021.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-DEF Note Definition 00006982.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
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APPROVED
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GEN-DEF LAND ASAP Definition 00007322.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-ABB Abbreviations 00006976.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-UNIT Correspondence Between Units 00006979.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
GEN-VIEW 3-View Drawing 00006880.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
LIM-GEN Introduction 00006957.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-GEN Kind of Operations 00006958.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-GEN Minimum Flight Crew 00006959.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-GEN Maximum Operating Altitude 00006960.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30748)
Applicable to: MSN 1882, 2078
LIM-GEN Maneuver Limit Load Factors 00006961.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-GEN Icing Conditions Definition 00009165.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
LIM-WGHT Weight Limitations 00006860.0014001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 and 25328)
Applicable to: MSN 1882, 2078
LIM-WGHT Center of Gravity Envelope 00006861.0131001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((319-111 or 319-112 or 319-113 or 319-114 or 319-131 or 319-132) and 25328)
Applicable to: MSN 1882, 2078
LIM-WGHT Performance Limitations 00006962.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-WGHT Loading 00006963.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-SPD VMO/MMO 00007065.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-SPD VA 00007319.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
LIM-SPD VFE 00006883.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (320-231 or 320-232 or 320-233 or A318 or A319)
Applicable to: MSN 1882, 2078
LIM-SPD VLO and VLE/MLE 00007317.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-OPS Environmental Envelope 00006919.0015001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or 321-200) and 30748)
Applicable to: MSN 1882, 2078
LIM-OPS Tailwind 00007309.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
LIM-OPS Runway Slope 00007310.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-09 Maneuvers on Ground 00007357.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-09 x Towbarless Operations 00016592.0001001 09 JUL 15
Approval reference: 10053997 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: 00007358 Towbarless Operations
LIM-09 Towbarless Operations 00007358.0001001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted by TDU: 00016592 Towbarless Operations
LIM-21 Cabin Pressurization 00007261.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-22-FMS General 00009567.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
Applicable to: MSN 1882, 2078
LIM-22-FMS Airworthiness Standards Compliance 00009568.0016001 13 MAR 17
Approval reference: 10061213 Approved by EASA
Criteria: ((A319 or A320 or A321) and ((31896 or 31897) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241
or 30631 or 30635)))
Applicable to: MSN 1882, 2078
LIM-22-FMS Navigation Performance 00009569.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and ((31896 or 31897 or 32475 or 32929) and (25205 or 26111 or 26485 or 26999
or 28382 or 30241 or 30631 or 30635)))
Applicable to: MSN 1882, 2078
LIM-22-FMS Use of NAV Mode 00009570.0003001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
LIM-22-FMS x Non Precision Approaches with OEI 00009620.0001001 23 NOV 09
Approval reference: 10027986 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
LIM-22-FMS Approaches 00009571.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and ((25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635)
and (31896 or 31897 or 32401 or 32402 or 32475 or 32929)))
Applicable to: MSN 1882, 2078
LIM-22-FGS Airworthiness Standards Compliance 00009235.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-22-FGS x Autoland Databases with Honeywell
ADIRU
00009711.0009001 04 NOV 15
Approval reference: 10055306 Approved by EASA
Criteria: (SA and (30652 or 30941 or 30942 or 31105 or 31706))
Applicable to: MSN 1882, 2078
Impacted DU: NONE
LIM-22-FGS Autoland 00009238.0003001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (((320-211 or 320-212 or 320-214) and 24617) or (319-111 or 319-112 or 319-113 or 319-114 or 319-115))
Applicable to: MSN 1882, 2078
LIM-22-FGS Minimum Height for Use of the Autopilot 00009242.0001001 28 MAR 17
Approval reference: SA22FM1701636 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
LIM-22-FGS CAT II / CAT III Operations 00009243.0013001 11 AUG 17
Approval reference: D01FM1703037 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: A319
Applicable to: MSN 1882, 2078
LIM-24 Electrical 00007263.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-28 Fuel and Additive Specifications 00007246.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
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GLG A319-112 FLEET PLP-LEDU P 8/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
LIM-28 Usable Fuel 00007248.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or 320-200)
Applicable to: MSN 1882, 2078
LIM-28 Fuel Imbalance 00007254.0015001 11 AUG 17
Approval reference: D01FM1703948 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
LIM-28 Fuel Temperature Limits 00007259.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((320-111 and 20024) or (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216))
Applicable to: MSN 1882, 2078
LIM-29 Hydraulics Fluid 00007262.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-29 x Ram Air Turbine (RAT) 00009631.0001001 23 NOV 09
Approval reference: 10027986 Approved by EASA
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Applicable to: MSN 1882, 2078
Impacted DU: NONE
LIM-32 Tire Speed 00011074.0001001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-34 Inertial Reference System (IRS) 00007264.0001001 10 NOV 17
Approval reference: SA03D17036154 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: ((A318 or A320) or ((A319 or A321) and (25204 or 30400 or 30941 or 31105 or 31706 or 33600 or 35793))
or ((A319 or A321) and (151772 or 24785 or 25294 or 26001)))
Applicable to: MSN 1882, 2078
LIM-34 Reduced Vertical Separation Minimum
(RVSM)
00007359.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (25861 or 25910 or 25952 or 31039 or 31528))
Applicable to: MSN 1882, 2078
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APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
LIM-46 Airline Operation Control Applications 00006965.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 27522)
Applicable to: MSN 1882, 2078
LIM-49 Auxiliary Power Unit (APU) 00007260.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (25888 or 37987))
Applicable to: MSN 1882, 2078
LIM-70 Main Engines 00007233.0021001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: 319-112
Applicable to: MSN 1882, 2078
LIM-70 Engine Parameters 00007235.0002001 11 MAY 17
Approval reference: 10061833 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
LIM-70 Reverse Thrust 00007236.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
LIM-70 Oil 00007232.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
LIM-70 Reduced Thrust Takeoff 00007239.0008001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 320-215) or ((319-111 or 319-112) and 32619) or (319-112 and 33239))
Applicable to: MSN 1882, 2078
LIM-70 Operations in Icing Conditions 00006881.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-GEN INTRODUCTION 00007037.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-GEN LANDING DISTANCE DETERMINATION
IN CASE OF IN-FLIGHT FAILURE
00015177.0001001 14 JUL 17
Approval reference: 10062618 Approved by EASA
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-21 CAB PR - EXCESS CAB ALT 00007053.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
EMER-21 CAB PR - EXCESS RESIDUAL PR 00009326.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and 35220)
Applicable to: MSN 1882, 2078
EMER-24 ELEC - EMER CONFIG (BOTH ENGINE
GENERATORS FAILED)
00006884.0003001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A320 and 28160) or (A318 or A319 or A321))
Applicable to: MSN 1882, 2078
EMER-26 GENERAL 00007038.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-26 ENG 1 (2) FIRE (In Flight) 00007041.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-26 ENG 1 (2) FIRE (On Ground) 00007042.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and ((20067 or 20069) and (36847 or 37871)))
Applicable to: MSN 1882, 2078
EMER-26 APU FIRE 00007043.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-26 SMOKE - FWD or AFT CARGO SMOKE 00009335.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (37871 and (20067 or 20069)))
Applicable to: MSN 1882, 2078
EMER-26 SMOKE/FUMES/AVNCS SMOKE 00007044.0006001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and (31276 and 37871))
Applicable to: MSN 1882, 2078
EMER-26 REMOVAL OF SMOKE/FUMES 00007045.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
EMER-27 F/CTL - L + R ELEV FAULT 00007051.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
EMER-27 F/CTL - FLAP LVR NOT ZERO 00009325.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (28479 or 28916))
Applicable to: MSN 1882, 2078
EMER-29 HYD - G + B SYS LO PR 00007048.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A320 and 35220) or A319)
Applicable to: MSN 1882, 2078
EMER-29 HYD - B + Y SYS LO PR 00007049.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
EMER-29 HYD - G + Y SYS LO PR 00007050.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
EMER-32 L/G - GEAR NOT DOWNLOCKED 00007052.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-32 LOSS OF BRAKING 00009809.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-34 x Abnormal V Alpha Prot 00016060.0001001 05 DEC 14
Approval reference: 10051494 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
EMER-70 DUAL ENG FAILURE (BOTH ENGINES
FLAME OUT)
00007039.0011001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112 or 319-115)
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
EMER-70 ENG - 1(2) OIL LO PR 00007040.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
EMER-90 STALL RECOVERY 00013505.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-90 x EMER DESCENT 00016883.0001001 07 OCT 15
Approval reference: 10055034 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: 00006626 EMER DESCENT
EMER-90 EMER DESCENT 00006626.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted by TDU: 00016883 EMER DESCENT
EMER-90 EMERGENCY EVACUATION 00006625.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
EMER-90 DITCHING 00006622.0002001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and 31276)
Applicable to: MSN 1882, 2078
EMER-90 FORCED LANDING 00006621.0002001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and 31276)
Applicable to: MSN 1882, 2078
EMER-90 Emergency Landing (All Engines
Failure)
00021836.0002001 11 AUG 17
Approval reference: D01FM1703948 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-GEN INTRODUCTION 00007087.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 13/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-GEN LANDING DISTANCE DETERMINATION
IN CASE OF IN-FLIGHT FAILURE
00015178.0001001 14 JUL 17
Approval reference: 10062618 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-TO ENGINE FAILURE BEFORE V1
(REJECTED TAKEOFF)
00007100.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-TO ENGINE FAILURE BETWEEN V1 AND V2 00007102.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-TO ENGINE FAILURE DURING INITIAL
CLIMB OUT
00007103.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-LDG APPROACH AND LANDING 00007104.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
ABN-OEI-LDG MISSED APPROACH (FROM
INTERMEDIATE APPROACH
CONFIGURATION)
00007105.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-LDG BALKED LANDING 00007106.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-21 AIR - PACK 1 + 2 FAULT 00007161.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-21 CAB PR - SYS 1 + 2 FAULT 00006672.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
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PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 14/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-21 CAB PR - SAFETY VALVE OPEN 00007162.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 35220)
Applicable to: MSN 1882, 2078
ABN-21 COND - HOT AIR FAULT 00007164.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-21 VENT - SKIN VALVE FAULT 00007165.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-AUTOFLT AUTO FLT - FCU 1(2) FAULT 00009309.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-AUTOFLT AUTO FLT - RUD TRV LIM SYS 00006936.0005001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: ((A318 or A319) and 37871)
Applicable to: MSN 1882, 2078
ABN-22-AUTOFLT AUTO FLT - FAC 1+2 FAULT 00009311.0002001 15 MAY 17
Approval reference: SA01D17016179 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: ((318-121 or 318-122) or ((318-111 or 318-112 or A319) and (36847 or 37871)))
Applicable to: MSN 1882, 2078
ABN-22-AUTOFLT AUTO FLT - YAW DAMPER SYS 00009310.0001001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Multiple Failures or Warnings (CAT II) 00009313.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Altitude Loss with Autopilot Malfunction
(CAT II)
00009795.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Failure Leading to Slats/Flaps less than
FLAPS 3 (CAT II)
00009315.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 15/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Antiskid System and/or Nosewheel
Steering Failure (CAT II)
00009338.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Alpha Floor Activation (CAT II) 00009342.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII One Engine Failure (CAT II) 00009343.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
ABN-22-CATII Red "RA" Flag on two PFDs (CAT II) 00009344.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Amber "CHECK ATT" Flag on two PFDs
(CAT II)
00009349.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Red "ATT" Flag on one PFD (CAT II) 00009350.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Diagonal Line or "INVALID DATA" on
one PFD and one ND (CAT II)
00009351.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Amber "CHECK HDG" Flag on two PFDs
and on two NDs (CAT II)
00009352.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Red "HDG" Flag on one PFD and one ND
(CAT II)
00009353.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 16/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Red "SPD" Flag on one PFD (CAT II) 00009354.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII "AP OFF" Warning (CAT II) 00009355.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Loss of "CAT 2" Capability (CAT II) 00009314.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII LOC or G/S Excessive Deviation on PFD
(CAT II)
00009356.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII "AUTOLAND" Light (CAT II) 00009357.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII A/THR Fault (CAT II) 00009358.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII No "LAND" at 350 ft (CAT II) 00009359.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII Incorrect Selected Course at 350 ft > 5
deg (CAT II)
00009360.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII No "FLARE" at 30 ft (CAT II) 00009361.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 17/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-22-CATIIIDH Multiples Failures or Warnings (CAT III
with DH)
00009366.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Failure Leading to Slats/Flaps less than
CONF 3 (CAT III with DH)
00009383.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Nosewheel Steering Failure (CAT III with
DH)
00009382.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Antiskid Failure (CAT III with DH) 00009381.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Alpha Floor Activation (CAT III with DH) 00009380.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH One Engine Failure (CAT III with DH) 00009379.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Auto Callout RA Failure (CAT III with DH) 00009378.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Red "RA" Flag on two PFDs (CAT III with
DH)
00009377.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Amber "CHECK ATT" Flag on two PFDs
(CAT III with DH)
00009386.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 18/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-22-CATIIIDH Red "ATT" Flag on one PFD (CAT III with
DH)
00009385.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Amber "CHECK HDG" Flag on two PFDs
and two NDs (CAT III with DH)
00009376.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Red "HDG" Flag on one PFD and one ND
(CAT III with DH)
00009375.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Red "SPD" Flag on one PFD (CAT III
with DH)
00009374.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH "AP OFF" Warning (CAT III with DH) 00009373.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Capability Decrease (Except if due to
A/THR Loss) (CAT III with DH)
00009372.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Total Loss of A/THR ("CAT 3" Decreases
to "CAT 2") (CAT III with DH)
00009384.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH LOC or G/S Excessive Deviation on PFD
(CAT III with DH)
00009371.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH "AUTOLAND" Light (CAT III with DH) 00009370.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 19/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH No "LAND" at 350 ft (CAT III with DH) 00009369.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH Incorrect Selected Course at 350 ft > 5
deg (CAT III with DH)
00009368.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH No "FLARE" at 30 ft (CAT III with DH) 00009367.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Multiple Failures or Warnings (CAT III no
DH)
00009393.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Failure Leading to Slats/Flaps less than
CONF 3 (CAT III no DH)
00009394.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Nosewheel Steering Failure (CAT III no
DH)
00009395.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Antiskid Failure (CAT III no DH) 00009396.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Alpha Floor Activation (CAT III no DH) 00009397.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH One Engine Failure (CAT III no DH) 00009413.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A321)
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 20/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Auto Callout RA Failure (CAT III no DH) 00009398.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Red "RA" Flag on two PFDs (CAT III no
DH)
00009399.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Amber "CHECK ATT" Flag on two PFDs
(CAT III no DH)
00009400.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Red "ATT" Flag on one PFD (CAT III no
DH)
00009401.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Amber "CHECK HDG" Flag on two PFDs
and two NDs (CAT III no DH)
00009402.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Red "HDG" Flag on one PFD and one ND
(CAT III no DH)
00009403.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Red "SPD" Flag on one PFD (CAT III no
DH)
00009404.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH "AP OFF" Warnings (CAT III no DH) 00009405.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 21/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-22-CATIIInoDH Capability Decrease (Except if due to
A/THR Loss) (CAT III no DH)
00009406.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Total Loss of A/THR ("CAT 3" Decreases
to "CAT 2") (CAT III no DH)
00009407.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH LOC or G/S Excessive Deviation on PFD
(CAT III no DH)
00009408.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH "AUTOLAND" Light (CAT III no DH) 00009409.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH No "LAND" at 350 ft (CAT III no DH) 00009410.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH Incorrect Selected Course at 350 ft > 5
deg (CAT III no DH)
00009411.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH No "FLARE" at 30 ft (CAT III no DH) 00009412.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-24 ELEC - AC ESS BUS FAULT 00007139.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-24 ELEC - AC BUS 1 FAULT 00007140.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 22/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-24 ELEC - AC BUS 2 FAULT 00007141.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC ESS BUS FAULT 00007143.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC BUS 1 FAULT 00007148.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 151269)
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC BUS 2 FAULT 00007150.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC EMER CONFIG 00007152.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC BUS 1 + 2 FAULT 00007154.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (((A320 or A321) and 21678) or A319)
Applicable to: MSN 1882, 2078
ABN-24 ELEC - DC ESS BUS SHED 00007159.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 151269)
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - FLAPS FAULT 00007108.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - FLAPS LOCKED 00006637.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - SLATS FAULT 00007109.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 23/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-27 F/CTL - SLATS LOCKED 00006638.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A318 or A319 or A320) and 20024)
Applicable to: MSN 1882, 2078
ABN-27 APPROACH SPEED INCREMENT AND
LANDING DISTANCE MULTIPLICATION
FACTOR
00006879.0005001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
ABN-27 PERFORMANCE LIMITATION FOR
LANDING IN CLEAN CONFIGURATION
00007110.0003001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - SPLR FAULT 00006639.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - GND SPLR FAULT 00007114.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - SPD BRK DISAGREE 00007117.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - SPD BRK FAULT 00007118.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - RUDDER JAM 00007119.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - STOP RUDDER INPUT 00015241.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 154473)
Applicable to: MSN 2078
ABN-27 F/CTL - L (R) ELEV FAULT 00007120.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: (A318 or A319)
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - ELAC 1(2) FAULT 00007121.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - SEC FAULT 00006640.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - FCDC 1 + 2 FAULT 00007131.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - STABILIZER JAM 00007132.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - ATLN LAW (PROT LOST) 00006618.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-27 F/CTL - DIRECT LAW (PROT LOST) 00006671.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-28 FUEL - L(R) TK PUMP 1+2 LO PR 00007194.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320) and 20024)
Applicable to: MSN 1882, 2078
ABN-28 FUEL - L(R) WING TK LO LVL 00007198.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320) and 20024)
Applicable to: MSN 1882, 2078
ABN-28 FUEL - L+R WING TK LO LVL 00007200.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 151269)
Applicable to: MSN 1882, 2078
ABN-28 FUEL - CTR TK PUMPS LO PR 00009364.0003001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A318 or A319 or A320) and 151269)
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
ABN-28 FUEL GRAVITY FEEDING 00006624.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-28 FUEL - L INNER (R INNER) (L OUTER) (R
OUTER) TK HI TEMP
00007201.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or A318)
Applicable to: MSN 1882, 2078
ABN-28 FUEL IMBALANCE 00007203.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or A318) and 20024)
Applicable to: MSN 1882, 2078
ABN-28 FUEL LEAK 00006692.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((320-111 or 320-211 or 320-212 or 320-214 or 320-231 or 320-232 or 320-233 or A318 or A319) and
20024)
Applicable to: MSN 1882, 2078
ABN-29 HYD - G SYS LO PR 00006656.0005001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-29 HYD - Y SYS LO PR 00006657.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-29 HYD - B SYS LO PR 00006658.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-29 HYD - RSVR LO AIR PR 00009203.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-29 HYD - RSVR OVHT 00009204.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-29 HYD - RSVR LO LVL 00009205.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-30 ANTI ICE - CAPT (F/O) PROBES HEAT
FAULT
00007178.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-30 DOUBLE AOA HEAT FAILURE 00007179.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 31283)
Applicable to: MSN 1882, 2078
ABN-30 WING A.ICE - SYS FAULT or OFF 00006619.0012001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-30 ANTI ICE - CAPT + F/O (CAPT + STBY)
(F/O + STBY) PITOT HEAT FAULT
00009388.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 35220)
Applicable to: MSN 1882, 2078
ABN-30 ANTI ICE - ALL PITOT HEAT FAULT 00009389.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 35220)
Applicable to: MSN 1882, 2078
ABN-31 FWS - FWC 1 + 2 FAULT 00007209.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-31 FWS - SDAC 1 + 2 FAULT 00007210.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-31 DISPLAY UNIT FAILURE 00007211.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-32 L/G GRAVITY EXTENSION 00006663.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 27/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
ABN-32 L/G - GEAR NOT UPLOCKED 00007168.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-32 L/G - GEAR UPLOCK FAULT 00007169.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-32 L/G - SHOCK ABSORBER FAULT 00007170.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-32 L/G - DOORS NOT CLOSED 00007171.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-32 BRAKES - A-SKID N-WS FAULT or OFF 00006623.0005001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-32 BRAKES - AUTO BRK FAULT 00007175.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
ABN-32 BRAKES - HOT 00007176.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 153741)
Applicable to: MSN 1882, 2078
ABN-32 AUTOBRAKE 00007177.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 NAV - RA 1+2 FAULT 00007212.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 NAV - IR 1+2 (1+3) (2+3) FAULT 00007213.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-34 NAV IR DISAGREE 00007214.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 NAV - ADR 1+2 FAULT 00007186.0001001 15 MAY 17
Approval reference: SA01D17016179 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 NAV - ADR 1+3 FAULT 00007187.0002001 15 MAY 17
Approval reference: SA01D17016179 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-34 NAV - ADR 2+3 FAULT 00009566.0002001 15 MAY 17
Approval reference: SA01D17016179 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-34 ADR 1+2+3 FAULT 00006691.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 NAV ADR DISAGREE 00007192.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34 x UNRELIABLE AIRSPEED INDICATION 00009811.0003001 11 FEB 16
Approval reference: 10056693 Approved by EASA
Criteria: (A318 or 319-100 or 320-200 or 321-100 or 321-200)
Applicable to: MSN 1882, 2078
Impacted DU: 00006690 UNRELIABLE AIRSPEED INDICATION
ABN-34 UNRELIABLE AIRSPEED INDICATION 00006690.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted by TDU: 00009811 UNRELIABLE AIRSPEED INDICATION
ABN-36 AIR - ENG 1(2) BLEED HI TEMP 00015197.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 151269)
Applicable to: MSN 1882, 2078
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 29/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
ABN-36 AIR - ENG 1(2) BLEED FAULT 00007180.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320) and 151269)
Applicable to: MSN 1882, 2078
ABN-36 AIR - ENG 1(2) BLEED ABNORM PR 00007181.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320) and 151269)
Applicable to: MSN 1882, 2078
ABN-36 AIR - X BLEED FAULT 00007184.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-36 AIR - L (R) WING LEAK 00007188.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-36 AIR - ENG 1(2) BLEED LEAK 00007190.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-36 AIR - ENG 1(2) BLEED LO TEMP 00009345.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A321 or ((A318 or A319 or A320) and 21566))
Applicable to: MSN 1882, 2078
ABN-36 AIR - ENG 1 + 2 BLEED LO TEMP 00009346.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A321 or ((A318 or A319 or A320) and 21566))
Applicable to: MSN 1882, 2078
ABN-52 DOOR - DOOR NOT CLOSED 00010780.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 x ENG - STALL 00016178.0001001 03 SEP 15
Approval reference: 10054650 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: NONE
ABN-70 x ENG COMPRESSOR VANE/ENG STALL
on ground
00009732.0001001 21 OCT 09
Approval reference: 10027686 Approved by EASA
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 30/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
ABN-70 ENG - FAIL 00006885.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 ENG - SHUTDOWN 00007091.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 ENG - REV PRESSURIZED 00007092.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 ENG - REVERSE UNLOCKED 00007093.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and 30660)
Applicable to: MSN 1882, 2078
ABN-70 ENG - REVERSER FAULT 00009156.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30660)
Applicable to: MSN 1882, 2078
ABN-70 ENG - THR LEVER FAULT 00009157.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30660)
Applicable to: MSN 1882, 2078
ABN-70 ENG - THR LEVER DISAGREE 00009158.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30660)
Applicable to: MSN 1882, 2078
ABN-70 ENG - OIL HI TEMP 00007095.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 ENG - FADEC FAULT 00007096.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213) and (36847 or
37871))
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 31/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
ABN-70 ENG - FADEC HI TEMP (FADEC OVHT) 00007097.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213) and (36847 or
37871))
Applicable to: MSN 1882, 2078
ABN-70 ENG - N1 (N2) (EGT) OVERLIMIT 00007098.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-70 ENG RELIGHT IN FLIGHT 00006620.0009001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
ABN-90 BOMB ON BOARD 00007024.0002001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and 31276)
Applicable to: MSN 1882, 2078
ABN-90 OVERWEIGHT LANDING 00007107.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-90 REJECTED TAKEOFF WITH ALL
ENGINES OPERATIVE
00007183.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-GEN Introduction 00009222.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-PFLT Electrical 00007056.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A321)
Applicable to: MSN 1882, 2078
NORM-PFLT Cockpit Door 00007057.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 32/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
NORM-PFLT Braking Efficiency Test 00007058.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-TO Takeoff Procedure 00007059.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213 or A318)
Applicable to: MSN 1882, 2078
NORM-FLT Buffet Onset 00007063.0003001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
NORM-FLT Flight in Severe Turbulence 00007066.0007001 14 FEB 17
Approval reference: FM1700589 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: A319
Applicable to: MSN 1882, 2078
NORM-LDG Normal Landing 00007067.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
NORM-LDG Balked Landing (All Engines Operating) 00007068.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-LDG Reverse Thrust 00007069.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-LDG Autobrake 00007070.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF AP/FD, Speed modes, Autothrust 00009463.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF Takeoff 00009464.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 33/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
NORM-22-CONF Climb, Cruise, Descent 00009465.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 24414)
Applicable to: MSN 1882, 2078
NORM-22-CONF Non Precision Approach 00009466.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF CAT I ILS Approach 00009467.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF CAT II ILS Approach 00009468.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF CAT II/III ILS Approach and Automatic
Approach
00009469.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF Go-around 00009470.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-CONF Altitude Loss after Automatic Go-around
Initiation
00009472.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115)
Applicable to: MSN 1882, 2078
NORM-22-NPA General 00009575.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-22-NPA Instrument Approach Using NAV Mode 00009576.0004001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((A319 or A320 or A321) and ((25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635)
and 150110))
Applicable to: MSN 1882, 2078
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 34/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
NORM-22-PA CAT II and CAT III Approach and/or
Automatic Landing
00009482.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A321)
Applicable to: MSN 1882, 2078
NORM-22-PA Required Equipment for CAT II and CAT
III Approach and Landing
00009476.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-28 Fuel System 00009172.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A320 and 20024) or (A318 or A319 or A321))
Applicable to: MSN 1882, 2078
NORM-30 Operations in Icing Conditions 00007071.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-30 Rain Repellent (If Activated) 00007080.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-34 Ground Proximity Warning System
(GPWS)
00007081.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-34 Inertial Reference System (IRS) 00009174.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
NORM-34 Reduced Vertical Separation Minimum
(RVSM)
00009175.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or ((A319 or A320 or A321) and (31039 or 31528)))
Applicable to: MSN 1882, 2078
NORM-34 Windshear Warning and Guidance
System
00009761.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 22249)
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
NORM-49 Auxiliary Power Unit (APU) 00006923.0009001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 25888)
Applicable to: MSN 1882, 2078
PERF-GEN Introduction 00006988.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-GEN Aircraft Configuration 00007266.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
PERF-GEN Maximum Demonstrated Crosswind at
Takeoff and Landing
00007267.0001001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
PERF-CAL-TO Speed Corrections in Ground Effect 00007268.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-CAL-TO Speed Corrections out of Ground Effect 00007269.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-CAL-TO Altitude Corrections 00007270.0004001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-CAL-CRU Speed and Mach Corrections 00007271.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (((A320 or A321) and (25490 or 25570)) or A319)
Applicable to: MSN 1882, 2078
PERF-CAL-CRU Altitude Corrections 00007272.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (((A320 or A321) and (25490 or 25570)) or A319)
Applicable to: MSN 1882, 2078
PERF-CAL-LDG Speed Corrections in Ground Effect 00007273.0003001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
PERF-CAL-LDG Speed Corrections Out of Ground Effect 00007274.0004001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-CAL-LDG Altitude Corrections 00007275.0004001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-TO Speeds Definitions 00006991.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-TO Distances Definitions 00006992.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-TO Takeoff Performance 00006904.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-TO Takeoff Flight Path 00006935.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-FLT In-Flight Performance 00006995.0006001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
PERF-LDG Approach Climb and Landing Climb 00006909.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
PERF-LDG Approach and Landing Speeds
Definition
00006996.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-LDG Landing Distance Definitions 00006997.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
PERF-LDG Landing Performance 00006910.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-LDG Autoland Landing Distance Increments 00006998.0007001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112 or 319-115)
Applicable to: MSN 1882, 2078
PERF-OCTO General 00021844.0001001 11 AUG 17
Approval reference: D01FM1703948 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (318-111 or 318-112 or 318-121 or 318-122 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or
319-131 or 319-132 or 319-133 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or 320-231 or 320-232 or
320-233 or 321-111 or 321-112 or 321-131 or 321-211 or 321-212 or 321-213 or 321-231 or 321-232)
Applicable to: MSN 1882, 2078
PERF-OCTO Performance Database 00006895.0028001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-112 and (32619 or 33239))
Applicable to: MSN 1882, 2078
N PERF-OCTO Complementary Performance Data File 00021722.0005001 07 NOV 17
Approval reference: 10063632 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
PERF-ENG Takeoff Thrust 00006989.0022001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: 319-112
Applicable to: MSN 1882, 2078
PERF-ENG Maximum Continuous Thrust 00007420.0015001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-111 or 319-112)
Applicable to: MSN 1882, 2078
PERF-ENG Go-Around Thrust 00007455.0012001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: 319-112
Applicable to: MSN 1882, 2078
PERF-FLEX Reduced Thrust Takeoff 00006990.0008001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-112 and (32619 or 33239))
Applicable to: MSN 1882, 2078
APP-NOI General 00007036.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 38/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Criteria: (321-111 or 321-112 or 321-131 or 321-231 or 321-232 or A318 or A319 or A320)
Applicable to: MSN 1882, 2078
APP-NOI External Noise 00006882.0045001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (319-112 and (25800 and 27772))
Applicable to: MSN 1882, 2078
APP-TCAS General 00007060.0005001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: ((SA and (150842 or 152353 or 153870 or 39146)) or (SA and 152830))
Applicable to: MSN 1882, 2078
APP-TCAS Procedures 00007062.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (26877 or 27698 or 27740 or 27753 or 28738 or 28739 or 30163))
Applicable to: MSN 1882, 2078
APP-INOP General 00006946.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
APP-INOP Performance 00007064.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 318-121 or 318-122 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or
320-111 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or
321-213)
Applicable to: MSN 1882, 2078
APP-LGDN-GEN General 00007074.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
APP-LGDN-LIM Limitations 00007075.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((A320 and 28160) or (A318 or A319 or A321))
Applicable to: MSN 1882, 2078
APP-LGDN-EMER ENG DUAL FAILURE 00007079.0006001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (((320-214 or 320-215 or 320-216) and 28160) or (319-111 or 319-112 or 319-115 or 321-111 or 321-112 or
321-211 or 321-212 or 321-213))
Applicable to: MSN 1882, 2078
APP-LGDN-ABN F/CTL FLIGHT CONTROLS FAILURE 00007078.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
APP-LGDN-NORM Preflight Check 00007076.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
APP-LGDN-PERF Performance 00007354.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
APP-LGDN-APP Appendices and Supplements 00009236.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
APP-INTX-GEN General 00007085.0007001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
APP-INTX-LIM Limitations 00009744.0006001 03 AUG 10
Approval reference: 10060714 Approved by EASA
Criteria: 319-112
Applicable to: MSN 1882, 2078
APP-INTX-ABN ENG RELIGHT IN FLIGHT in case of
SAC/DAC intermix
00007089.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (319-112 or 320-214 or 321-111 or 321-211 or 321-212)
Applicable to: MSN 1882, 2078
APP-INTX-ABN ENG RELIGHT IN FLIGHT in case of
SAC-TI intermix
00009652.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
APP-INTX-NORM Takeoff Procedure 00007088.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
APP-HAO-GEN General 00007111.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or
320-232 or 320-233 or 321-200) and (25615 or 34540))
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 40/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
APP-HAO-LIM Environmental Envelope 00007112.0093001 11 AUG 17
Approval reference: D01FM1703037 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: ((319-111 or 319-112) and (25615 and 30748))
Applicable to: MSN 1882, 2078
APP-HAO-NORM Normal Procedures 00007122.0006001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or
320-215 or 320-216 or 320-232 or 320-233 or 321-200) and 25615)
Applicable to: MSN 1882, 2078
APP-HAO-PERF Performance 00007129.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or
320-215 or 320-216 or 320-232 or 320-233 or 321-200) and 25615)
Applicable to: MSN 1882, 2078
APP-TAWS General 00007228.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (26526 or 28244 or 34637 or 39146))
Applicable to: MSN 1882, 2078
APP-TAWS Limitations 00007229.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and (26526 or 28244))
Applicable to: MSN 1882, 2078
APP-TAWS Normal Procedures 00007231.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 28244)
Applicable to: MSN 1882, 2078
APP-NRWY General 00006985.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30397)
Applicable to: MSN 1882, 2078
APP-NRWY Limitations 00006987.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30397)
Applicable to: MSN 1882, 2078
APP-NRWY Procedures 00007014.0001001 03 AUG 17
Approval reference: 10062810 Approved by EASA
Criteria: ((A319 or A320 or A321) and 30397)
Applicable to: MSN 1882, 2078
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 41/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
APP-NRWY Performance 00006986.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and 30397)
Applicable to: MSN 1882, 2078
APP-PFC General 00007028.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
APP-PFC Performance 00007029.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-GEN-INTR Introduction 00006202.0001001 02 OCT 17
Approval reference: SA03D17033085 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-GEN-LIM Limitations 00006203.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-GEN-PERF Performance Determination Method 00006204.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-GEN-PERF Performance Penalties published in the
Airplane Flight Manual MCDL Chapter
00006205.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-GEN-PERF Performance Penalties calculated with
AFM_OCTO Software
00006206.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-21-01 Ram Air Inlet Flap 00006207.0002001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (SA and ((26363 and A319) or (26363 and A320) or (26363 and A321) or A318))
Applicable to: MSN 1882, 2078
MCDL-21-01 Illustration Ram Air Inlet Flap 00006213.0001001 23 NOV 09
Criteria: SA
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
MCDL-21-03 Ram Air Inlet Leading Edge 00006216.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-21-03 Illustration Ram Air Inlet Leading Edge 00006219.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-23-01 Static Discharger 00006220.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-23-01 Illustration Static Discharger 00006221.0001001 12 JUN 14
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-27-01 Flap Track Fairing 00006235.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-27-01 Illustration Flap track fairing 00006236.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-27-03 Slat Track Closing Plate 00006239.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-03 Illustration Slat track closing plate 00006240.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-05 Access Panel for Bearings at Elevator 00006243.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-05 Illustration Access panel for bearings at
elevator
00006244.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-06 Flap Track Fairing Rear Top Cover and
Tail Cone
00006245.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 43/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
MCDL-27-06 Illustration Flap track fairing rear top
cover and tail cone
00006246.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-07 Rubber Seal under Slat 00006247.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-07 Illustration Rubber seal under slat 00006248.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-27-08 Seal Between Inboard and Outboard
Flap
00006250.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
MCDL-27-08 Illustration Seal Between Inboard and
Outboard Flap
00006251.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-09 Inboard Aileron Edge to Wing Seal 00006252.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-09 Illustration Inboard Aileron to Wing Seal 00006253.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-10 Slat End Seal and Weather Seal 00006254.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-10 Illustration Slat End Seal and Weather
Seal
00006255.0001001 24 NOV 15
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-11 Slat Track Filler Block 00006256.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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GLG A319-112 FLEET PLP-LEDU P 44/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-27-11 Illustration Slat track filler block 00006257.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-12 Slat Track Sealing Packer 00006258.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-12 Illustration Slat track sealing packer 00006259.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-13 Inter-flap Cushion Seal 00006249.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-13 Illustration Inter-flap cushion seal 00006260.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-14 Flap Track Moveable Fairing Seal 00006261.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-14 Illustration Moveable flap track fairing
seal
00006262.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-15 Flap Track Fixed Fairing seal 00006263.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-27-15 Illustration Fixed flap track fairing seal 00006264.0001001 23 NOV 09
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
R MCDL-27-16 Flap Track Moveable Fairing Pivot Cover 00006265.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-16 Illustration Flap Track Moveable Fairing
Pivot Cover
00006266.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
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AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
R MCDL-28-01 Refuel/Defuel Coupling Cap 101 QM Or
41 QM
00006282.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-28-01 Illustration Refuel/Defuel Coupling Cap
101 QM or 41 QM
00006283.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-28-02 Refuel Panel Door 00006285.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-28-02 Illustration Refuel Panel Door 192MB 00006286.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-30-01 Icing Indicator 00006287.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-30-01 Illustration Icing Indicator 00006288.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-32-03 Nose Wheel Hubcap 00006297.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-32-03 Illustration Nose Wheel Hubcap 00006298.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-32-04 Nose Fitting Towing 00006299.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-32-04 Illustration Nose Fitting Towing 00006300.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-01 Wing/Engine Scan Light Cover 3LX, 4LX 00006301.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 46/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-33-01 Illustration Wing/Engine Scan light
Cover 3LX, 4LX
00006302.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-33-02 Taxi Light Lamp 8LR 00006303.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-02 Illustration Taxi Light Lamp 8LR 00006304.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-03 Rear Navigation Light Lens 15LA 00006305.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-03 Illustration Rear Navigation Light Lens
15LA
00006306.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-04 Upper 7LV and Lower 6LV Anti-collision
(Beacon) Light Cover
00006307.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-04 Illustration Upper and Lower
Anti-Collision ( Beacon) Light Cover
00006308.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-05 Logo Light Lens (Cover) 3LY, 4LY 00006309.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-05 Illustration Logo Light Lens (Cover) 3LY,
4LY
00006310.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-33-07 Landing Light Lens 7LB, 8LB 00006321.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 47/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-33-07 Illustration Landing Light Lens 7LB, 8LB 00006322.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-08 Turn OFF Light Lamp 3LC1, 3LC2 00006324.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-08 Illustration Turn OFF Light Lamp 3LC1,
3LC2
00006325.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-09 Takeoff light lamp 7LR 00006327.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-09 Illustration Takeoff Light Lamp 7LR 00006328.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-49-01 APU Overpressure Release Door 00006329.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-49-01 Illustration APU Overpressure Release
Door
00006330.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-51-02 Passenger Door Scuff Plate 00006333.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-51-02 Illustration Passenger Door Scuff Plate 00006334.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-51-04 Fairing Aft Safety Stay Point 311 AL 00006338.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-51-04 Illustration Fairing Aft Safety Stay Point
311AL
00006339.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 48/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-52-01 Toilet Servicing and Drainage Door 172
AR
00006441.0003001 23 JAN 17
Approval reference: SA52D17001991 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: ((A319 or A320 or A321) and 20109)
Applicable to: MSN 1882, 2078
MCDL-52-01 Illustration Toilet Servicing and
Drainage Door
00006442.0002001 23 NOV 09
Criteria: (SA and 20109)
Applicable to: MSN 1882, 2078
MCDL-52-02 Access Door To Hydraulic Ground
Connectors 197 CB - 197 EB - 198 CB
00006447.0001001 16 JUN 17
Approval reference: SA52FM1703062 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
MCDL-52-02 Illustration Access Door to Hydraulic
Ground Connectors 197 CB - 197 EB -
198 CB
00006449.0001001 24 NOV 15
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-03 x Access Door To Potable Water Filling
And Drainage 133 AL - 171 AL
00016655.0001001 06 JUL 15
Approval reference: 10053953 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
Impacted DU: 00006452 Access Door to Potable Water Filling and Drainage
MCDL-52-03 Access Door To Potable Water Filling
And Drainage 133 AL - 171 AL - 192 NB
00006452.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
Impacted by TDU: 00016655 Access Door to Potable Water Filling and Drainage
MCDL-52-03 x Illustration Access Door to Potable
Water Filling and Drainage
00016656.0001001 06 JUL 15
Approval reference: 10053953 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
Impacted DU: 00006453 Illustration Access Door to Potable Water Filling and Drainage
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 49/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-52-03 Illustration Access Door to Potable
Water Filling and Drainage
00006453.0001001 23 NOV 09
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
Impacted by TDU: 00016656 Illustration Access Door to Potable Water Filling and Drainage
MCDL-52-04 Access Door To Opening Control Of
Landing Gear Doors On Ground 195 BB
- 196 BB
00006455.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
MCDL-52-04 Illustration Access door to opening
control of landing gear doors on ground
195 BB - 196 BB
00006456.0001001 03 AUG 10
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-52-05 Access Door To Air Conditioning
Ground Supply 191 CB
00006457.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-05 Illustration Access door to air
conditionning ground supply 191 CB
00006458.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-07 External Power Ground Connection
Access Door Assy 121 AL
00006461.0001001 02 OCT 17
Approval reference: SA03D17033085 Approved by Airbus under the authority of DOA ref.
EASA.21J.031
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-07 Illustration External Power Ground
Connection Access Door Assy 121 AL
00006462.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-08 Access Door Of Cargo Opening System
134 AR - 154 AR
00006463.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 50/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-52-08 Illustration Access Door of Cargo
Opening System 134 AR - 154 AR
00006464.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-09 Nose Landing Gear Main Door (713, 714) 00006465.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-52-09 Illustration Nose Landing Gear Main
Door (713, 714)
00006466.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-10 Nose Landing Gear Aft Door (715, 716) 00006467.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-10 Illustration Nose Landing Gear Aft Door
(715, 716)
00006468.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-11 Nose Landing Gear Leg Door (712) 00006471.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-11 Illustration Nose Landing Gear Leg Door
(712)
00006472.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-12 Main Landing Gear Door (732, 742)
(flight with gear up)
00006473.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-52-12 Illustration Main Landing Gear Door
(732, 742)
00006474.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-13 Main Landing Gear Door (733, 743)
(flight with gear up)
00006487.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 51/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
MCDL-52-13 Illustration Main Landing Gear Door
(733, 743)
00006488.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-14 Main Landing Gear Door (732, 742)
(Flight with gear down)
00006475.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-52-14 Illustration Main Landing Gear Door
(732, 742)
00006476.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-15 Main Landing Gear Door (733, 743)
(Flight with gear down)
00006489.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A319 or A320 or A321)
Applicable to: MSN 1882, 2078
MCDL-52-15 Illustration Main Landing Gear Door
(733, 743)
00006490.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-16 Main Landing Gear Door (734, 744)
(Flight with gear down)
00006491.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-52-16 Illustration Main Landing Gear Door
(734, 744)
00006492.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-18 Main Landing Gear Door : Seal On
Secondary Hinged Fairing
00006479.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-18 Illustration Main Landing Gear Door :
Seal on Secondary Hinged Fairing
00006480.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 52/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-52-19 Pax Door Upper Cover Plate 00006481.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-52-19 Illustration Pax Door Upper Cover Plate 00006482.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-20 Access Door To HP Air Ground
Connector 191 DB
00006483.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-20 Illustration Access Door to HP Air
Ground Connector 191 DB
00006484.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-52-21 Blue Hydraulic Access Door 197 FB 00007449.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-21 Illustration Blue Hydraulic Access Door
197 FB
00007450.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-22 Forward Cargo Door Access Cover
Panel 825 AR
00007451.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-22 Illustration Forward Cargo Door Access
Cover Panel 825 AR
00007452.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-23 Aft Cargo Door Access Cover Panel 826
AR
00007453.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-23 Illustration Aft Cargo Door Access
Cover Panel 826 AR
00007454.0002001 17 AUG 16
Criteria: A319
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 53/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
Applicable to: MSN 1882, 2078
MCDL-53-01 Belly Fairing Vent Louver Vane 00006512.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-53-01 Illustration Belly Fairing Vent Louver
Vane
00006513.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-53-03 Root Fillet Fairing 00011063.0005001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
MCDL-53-03 Illustration Root Fillet Fairing 00011064.0001001 03 AUG 10
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-01 Nacelle Strake 00006516.0005001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
MCDL-54-01 Illustration Nacelle Strake 00006517.0002001 23 NOV 09
Criteria: (A318 or A319 or A321)
Applicable to: MSN 1882, 2078
MCDL-54-03 Pylon Pressure Relief Door 413(423) BL
- 414(424) BR
00006540.0003001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
MCDL-54-03 Illustration Pylon Pressure Relief Door
413(423) BL - 414(424) BR
00006541.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-04 Pylon Access Door 415(425) AL -
415(425) AR
00006543.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-04 Illustration Pylon Access Door 415(425)
AL - 415(425) AR
00006544.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
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PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 54/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-54-05 x Pylon Fairing Seal 00015527.0001001 29 OCT 14
Approval reference: 10050974 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: 00006545 Pylon Fairing Seal
MCDL-54-05 Pylon Fairing seal 00006545.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted by TDU: 00015527 Pylon Fairing Seal
MCDL-54-05 x Illustration Pylon Fairing Seal 00015528.0001001 29 OCT 14
Approval reference: 10050974 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted DU: 00006546 Illustration Pylon Fairing Seal
MCDL-54-05 Illustration Pylon Fairing Seal 00006546.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
Impacted by TDU: 00015528 Illustration Pylon Fairing Seal
MCDL-54-06 Aerodynamic Seal 00006547.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-06 Illustration Aerodynamic Seal 00006548.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-57-01 Wing Tip Fence 00006549.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
MCDL-57-01 Illustration Wing Tip Fence 00006550.0001001 23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
R MCDL-57-02 Belly Fairing Sliding Panel 00006551.0002001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: (SA and 26495)
Applicable to: MSN 1882, 2078
MCDL-57-02 Illustration Belly Fairing Sliding Panel 00006552.0002001 23 NOV 09
Criteria: (SA and 26495)
Applicable to: MSN 1882, 2078
Continued on the following page
A319
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PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 55/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-57-03 Outboard Flap Rubbing Strip Items 10,
15, 20, 40
00006564.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-57-03 Illustration Outboard Flap Rubbing Strip 00006565.0001001 23 NOV 09
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-57-04 Inboard Flap Rubbing Strip items 1, 5,
10, 30
00006567.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-57-04 Illustration Inboard Flap Rubbing Strip 00006568.0001001 02 DEC 13
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
R MCDL-57-06 Outer Flap Blade Seal 00021897.0001001 29 NOV 17
Approval reference: 10063916 Approved by EASA
Criteria: (A318 or A319 or A320 or A321)
Applicable to: MSN 1882, 2078
MCDL-57-06 Illustration Outer Flap Blade Seal 00021942.0001001 07 SEP 17
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-71-01 Frangible Drain Mast 00006569.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-111 or 320-214 or 320-215 or 320-216 or
321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-71-01 Illustration Frangible Drain Mast 00006570.0001001 23 NOV 09
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-71-09 Fan Cowl Hold Open Rod 00006587.0002001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-71-09 Illustration Fan Cowl Hold Open Rod 00006588.0003001 09 NOV 16
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Continued on the following page
A319
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PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 56/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
MCDL-78-01 x Duct Opening Actuator 00016031.0001001 20 MAR 15
Approval reference: 10052671 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
MCDL-78-01 x Illustration Duct Opening Actuator 00016033.0001001 20 MAR 15
Approval reference: 10052671 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
Impacted DU: NONE
MCDL-78-09 Thrust Reverser 11 and 1 O'clock Struts 00006596.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-78-09 Illustration Thrust Reverser 11 and 1
O'clock Struts
00006597.0001001 02 DEC 13
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-78-11 Thrust Reverser Lockout Fairing 00014886.0001001 14 JAN 15
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
MCDL-78-11 Illustration of the Thrust Reverser
Lockout Fairing
00014887.0001001 02 DEC 13
Approval reference: 10060714 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
SPERF-CONT-GEN General 00009415.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
SPERF-CONT-LIM Limitations 00009416.0001001 04 APR 11
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
GLG A319-112 FLEET PLP-LEDU P 57/58
AFM 12 DEC 17
APPROVED
Continued from the previous page
M(1) Localization T(2) DU Title DU identification DU date
SPERF-CONT-PERF Introduction 00009417.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
R SPERF-CONT-PERF Aircraft Configuration 00009441.0001001 07 NOV 17
Approval reference: 10063632 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
SPERF-CONT-PERF Takeoff and Landing Performance 00009429.0001001 23 NOV 09
Approval reference: 10060714 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
(1) Evolution code : N=New, R=Revised, E=Effectivity
(2) Temporary information
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
Intentionally left blank
GLG A319-112 FLEET PLP-LEDU P 58/58
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE TEMPORARY REVISIONS
GLG A319-112 FLEET PLP-LETR P 1/2
AFM 14 NOV 17
APPROVED
M(1) TR identification TR approval
date
TR Title Deleted by
TR1 issue 1 23 NOV 09 (TR 2.05.00/47) - Non Precision Approaches
with OEI
Mod 37665 for A318/A320
or Mod 153286 for A321
Approval reference: 10027986 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
TR6 issue 1 23 NOV 09 (TR 2.05.00/67) - Ram Air Turbine (RAT) Flight
Testing
Mod 28413 or Mod
34978 or Mod 35511
Approval reference: 10027986 Approved by EASA
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Applicable to: MSN 1882, 2078
TR34 issue 1 21 OCT 09 (TR 4.02.00/41) - ENG Compressor vane/ENG
STALL on ground
Approval reference: 10027686 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or
321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
TR188 issue 2 04 NOV 15 Autoland Databases with Honeywell ADIRU MOD 38480 or 154407
or 37784 or 35793
or 37806 or 37785
or 156889 or 156844
Approval reference: 10055306 Approved by EASA
Criteria: (SA and (30652 or 30941 or 30942 or 31105 or 31706))
Applicable to: MSN 1882, 2078
TR423 issue 1 29 OCT 14 MCDL 54-05 Pylon Fairing Seal
Approval reference: 10050974 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
TR499 issue 1 20 MAR 15 MCDL 78-01 Duct Opening Actuator for CFM
Engine
Approval reference: 10052671 Approved by EASA
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or
320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Applicable to: MSN 1882, 2078
TR500 issue 1 03 SEP 15 ABN - ENG STALL
Approval reference: 10054650 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
TR502 issue 1 05 DEC 14 Abnormal V Alpha Prot
Approval reference: 10051494 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF EFFECTIVE TEMPORARY REVISIONS
GLG A319-112 FLEET PLP-LETR P 2/2
AFM 14 NOV 17
APPROVED
Continued from the previous page
M(1) TR identification TR approval
date
TR Title Deleted by
TR556 issue 1 09 JUL 15 Towbarless Operations
Approval reference: 10053997 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
TR562 issue 1 11 FEB 16 Unreliable Airspeed
Approval reference: 10056693 Approved by EASA
Criteria: (A318 or 319-100 or 320-200 or 321-100 or 321-200)
Applicable to: MSN 1882, 2078
TR564 issue 1 06 JUL 15 MCDL 52-03 Access Door TO Potable Water
Filling and Drainage
Approval reference: 10053953 Approved by EASA
Criteria: (A319 or A321)
Applicable to: MSN 1882, 2078
TR566 issue 1 07 OCT 15 EMER DESCENT
Approval reference: 10055034 Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
(1) Evolution code : N=New, R=Revised, E=Effectivity
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF APPROVAL REFERENCES
GLG A319-112 FLEET PLP-LAR P 1/2
AFM 12 DEC 17
Approval Date Approval Reference Approved By
29 NOV 17 10063916 EASA
10 NOV 17 SA03D17036154 Airbus under the authority
of DOA ref. EASA.21J.031
07 NOV 17 10063632 EASA
02 OCT 17 SA03D17033085 Airbus under the authority
of DOA ref. EASA.21J.031
07 SEP 17 D03D17028536 Airbus under the authority
of DOA ref. EASA.21J.031
11 AUG 17 D01FM1703037 Airbus under the authority
of DOA ref. EASA.21J.031
11 AUG 17 D01FM1703948 Airbus under the authority
of DOA ref. EASA.21J.031
03 AUG 17 10062810 EASA
14 JUL 17 10062618 EASA
16 JUN 17 SA52FM1703062 Airbus under the authority
of DOA ref. EASA.21J.031
15 MAY 17 SA01D17016179 Airbus under the authority
of DOA ref. EASA.21J.031
11 MAY 17 10061833 EASA
28 MAR 17 SA22FM1701636 Airbus under the authority
of DOA ref. EASA.21J.031
13 MAR 17 10061213 EASA
14 FEB 17 FM1700589 Airbus under the authority
of DOA ref. EASA.21J.031
23 JAN 17 SA52D17001991 Airbus under the authority
of DOA ref. EASA.21J.031
16 JAN 17 10060714 EASA
16 JAN 17 10060714 EASA
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF APPROVAL REFERENCES
Intentionally left blank
GLG A319-112 FLEET PLP-LAR P 2/2
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF MODIFICATIONS
GLG A319-112 FLEET PLP-LOM P 1/4
AFM 08 AUG 17
M(1) CRITERION Linked SB Incorp. Date Title
20024 14 DEC 10 FUEL- INSTALL A CENTRE TANK SYSTEM-
Applicable to: MSN 1882, 2078
20067 14 DEC 10 FIRE PROTECTION - FWD CARGO COMPARTMENT -
INSTALL SMOKE DETECTION SYSTEM -
Applicable to: MSN 1882, 2078
20069 14 DEC 10 FIRE PROTECTION - AFT CARGO COMPARTMENT -
INSTALL SMOKE DETECTION SYSTEM -
Applicable to: MSN 1882, 2078
20109 14 DEC 10 WATER/WASTE- INSTALL VACUUM TOILET SYSTEM
-
Applicable to: MSN 1882, 2078
21566 14 DEC 10 ICE AND RAIN PROTECTION - MODIFY AIR BLEED
SYSTEM TO PROVIDE LOW TEMPERATURE
WARNING-
Applicable to: MSN 1882, 2078
22249 14 DEC 10 AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION
Applicable to: MSN 1882, 2078
22803 14 DEC 10 HYDRAULIC POWER - AUXILIARY HYDRAULIC
POWER - INTRODUCE A321 RAM AIR TURBINE
Applicable to: MSN 1882, 2078
24414 14 DEC 10 AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU)
DELETE "EXPEDITE" FUNCTION FROM FCU
Applicable to: MSN 1882, 2078
25294 14 DEC 10 NAVIGATION - ADIRS - INSTALL HONEYWELL ADIRS
CAPABLE OF A319 A/C
Applicable to: MSN 1882, 2078
25328 14 DEC 10 GENERAL - DESIGN WEIGHTS - INCREASED
MAXIMUM TAKE-OFF WEIGHT (MTOW) TO 70.0 T
Applicable to: MSN 1882, 2078
25615 22 SEP 15 CERTIFICATION - GENERAL - CERTIFICATION FOR
HIGH ALTITUDE AIRPORT OPERATION
Applicable to: MSN 1882, 2078
25800 14 DEC 10 POWER PLANT-GENERAL-INTRODUCE CFM56-5B/P
Applicable to: MSN 1882, 2078
25861 14 DEC 10 NAVIGATION-REDUCED VERTICAL SEPARATION
MINIMUM (RVSM) (CERTIFICATION APPLICABLE ON
A319/A320 ONLY)
Applicable to: MSN 1882, 2078
25888 14 DEC 10 A.P.U.-POWER PLANT-INTRODUCE ALLIED SIGNAL
APU 131-9(A)
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF MODIFICATIONS
GLG A319-112 FLEET PLP-LOM P 2/4
AFM 08 AUG 17
Continued from the previous page
M(1) CRITERION Linked SB Incorp. Date Title
26001 14 DEC 10 NAVIGATION-ADIRS-INTRODUCE HONEYWELL 4
MCU P/N AC09
Applicable to: MSN 1882, 2078
26363 14 DEC 10 AIR CONDITIONING-AIR COOLING SYSTEM-
INTRODUCE MODIFIED RAM AIR OUTLET
Applicable to: MSN 1882, 2078
26495 14 DEC 10 WINGS-INBOARD FLAP-MODIFY SLIDING PANEL
DRIVING MECHANISM
Applicable to: MSN 1882, 2078
26526 14 DEC 10 NAVIGATION - GPWS - ACTIVATE ENHANCED
FUNCTIONS OF THE EGPWS
Applicable to: MSN 1882, 2078
26999 14 DEC 10 NAVIGATION - MMR - INSTALL COLLINS MMR
PROVIDING ILS AND GPS FUNCTION
Applicable to: MSN 1882, 2078
27522 14 DEC 10 INFORMATION SYSTEM - AIR TRAFFIC AND
INFORMATION SYSTEM (ATIMS) - INSTALL ATSU
COMPUTER FOR ACARS
Applicable to: MSN 1882, 2078
27753 14 DEC 10 NAVIGATION - TCAS - INSTALL COLLINS TCAS
TTR921 WITH COLLINS ATC TPR901
Applicable to: MSN 1882, 2078
27772 14 DEC 10 ENGINES-CFM56-5B-FAN FRAME ASSY- INTRODUCE
QC1 PANEL KIT (ACOUSTIC TREATMENT)
Applicable to: MSN 1882, 2078
28244 14 DEC 10 NAVIGATION-GPWS-INTRODUCE EGPWS P/N
206-206 AND INHIBIT AUTOMATIC DEACTIVATION
ENHANCED FUNCTIONS
Applicable to: MSN 1882, 2078
28479 14 DEC 10 INDICATING RECORDING SYSTEM-FWC-
INTRODUCE FWC STANDARD H2/E3P
Applicable to: MSN 1882, 2078
28916 14 DEC 10 INDICATING RECORDING SYSTEM-FWS INTRODUCE
FWC STANDARD H1PE3P
Applicable to: MSN 1882, 2078
30397 21 MAR 12 CERTIFICATION DOCUMENTS - GENERAL - CERTIFY
AIRCRAFT FOR OPERATION ON RUNWAYS LESS
THAN 45M WIDTH
Applicable to: MSN 1882, 2078
30660 14 DEC 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
FWC STANDARD H2E4
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF MODIFICATIONS
GLG A319-112 FLEET PLP-LOM P 3/4
AFM 08 AUG 17
Continued from the previous page
M(1) CRITERION Linked SB Incorp. Date Title
30748 14 DEC 10 GENERAL-FLIGHT ENVIRONMENTAL ENVELOPE-
EXTENSION TO 12100 M (39800 FT)
Applicable to: MSN 1882, 2078
30941 14 DEC 10 NAVIGATION-ADIRU-INSTALL HONEYWELL ADIR U 4
MCU AD11 (NEW HARD)
Applicable to: MSN 1882, 2078
31276 14 DEC 10 ELECTRICAL POWER - GENERAL - INSTALL A
COMMERCIAL SHEDDING PUSH-BUTTON SWITCH IN
COCKPIT
Applicable to: MSN 1882, 2078
31283 14 DEC 10 INDICATING RECORDING SYSTEM-FWC-
INTRODUCE FWC STANDARD H2 F1
Applicable to: MSN 1882, 2078
31528 14 DEC 10 NAVIGATION-ADIRU-RESTORE RVSM 3 CIRCUIT
CAPABILITIES (SERIAL SOLUTION)
Applicable to: MSN 1882, 2078
31896 14 DEC 10 AUTOFLIGHT-FMGC-INSTALL FMGC CFM
C13042AA01 (EQUIPPED WITH FMS2) HONEYWELL
Applicable to: MSN 1882, 2078
32619 14 DEC 10 ENGINE FUEL AND CONTROL - FADEC SYSTEM
INTRODUCE NEW FADEC SOFTWARE "5BK" ON SAC
CFM56-5B ENGINES
Applicable to: MSN 1882, 2078
33239 14 DEC 10 ENGINE FUEL AND CONTROL - FADEC SYSTEM -
INSTALL "5BL" STANDARD ECU SOFTWARE FOR
CFM56-5B ENGINES (A318 CAPABLE)
Applicable to: MSN 1882, 2078
35220 05 DEC 11 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2F3
Applicable to: MSN 1882, 2078
37871 05 DEC 11 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F5
Applicable to: MSN 1882, 2078
150110 05 DEC 11 AUTO FLIGHT- FLIGHT MANAGEMENT SYSTEM-
ACTIVATE BARO RADIO SETTING FUNCTION
Applicable to: MSN 1882, 2078
151269 11 APR 14 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F6
Applicable to: MSN 1882, 2078
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PRELIMINARY PAGES
LIST OF MODIFICATIONS
GLG A319-112 FLEET PLP-LOM P 4/4
AFM 08 AUG 17
Continued from the previous page
M(1) CRITERION Linked SB Incorp. Date Title
152830 03 NOV 16 NAVIGATION-TRAFFIC COLLISION AVOIDANCE
SYSTEM (TCAS) - INSTALL TCAS COLLINS TTR-921
CHANGE 7.1
Applicable to: MSN 1882, 2078
153741 11 APR 14 INDICATING RECORDING SYSTEMS-FWC-
INTRODUCE FWC STANDARD H2-F7
Applicable to: MSN 1882, 2078
154473 08 AUG 17 AUTO FLIGHT-FLIGHT AUGMENTATION (FAC)
DEFINE STOP RUDDER INPUT WARNING FUNCTION
ON AIRCRAFT
Applicable to: MSN 2078
(1) Evolution code : N=New, R=Revised, E=Effectivity
APPROVAL DATA
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET APPRO-PLP-TOC P 1/2
AFM 12 DEC 17
APPRO-TR TEMPORARY REVISIONS
ABN - ENG STALL..................................................................................................................................................A
Unreliable Airspeed..................................................................................................................................................B
(TR 4.02.00/41) - ENG Compressor vane/ENG STALL on ground........................................................................ C
(TR 2.05.00/47) - Non Precision Approaches with OEI..........................................................................................D
(TR 2.05.00/67) - Ram Air Turbine (RAT) Flight Testing........................................................................................E
Autoland Databases with Honeywell ADIRU...........................................................................................................F
MCDL 54-05 Pylon Fairing Seal............................................................................................................................. G
MCDL 78-01 Duct Opening Actuator for CFM Engine............................................................................................H
Abnormal V Alpha Prot.............................................................................................................................................I
EMER DESCENT.....................................................................................................................................................J
Towbarless Operations............................................................................................................................................K
MCDL 52-03 Access Door TO Potable Water Filling and Drainage........................................................................L
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
PRELIMINARY PAGES
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET APPRO-PLP-TOC P 2/2
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 1/12
AFM A 14 NOV 17
TR500 Issue 1
ABN - ENG STALL
Ident.: TDU / APPRO-TR-00016179.0001001 / 03 SEP 15 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 03 SEP 15
Approval reference: 10054650
Do not remove this Tempory Revision until instructed to do so.
Reason for issue: This Temporary Revision is issued to provide the ENG STALL Abnormal
procedure.
Applicable to: All A318/A319/A320/A321 aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016179.0001001/03 SEP 15 ABN-70-00016178.0001001/03 SEP 15
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 2/12
AFM B 14 NOV 17
TR562 Issue 1
UNRELIABLE AIRSPEED
Ident.: TDU / APPRO-TR-00009810.0003001 / 11 FEB 16 APPROVED
Criteria: (A318 or 319-100 or 320-200 or 321-100 or 321-200)
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 11 FEB 16
Approval reference: 10056693
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This Temporary Revision (TR) provides the updated unreliable airspeed
procedure.
Applicable to: A318 or A319CEO or A320CEO or A321CEO aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00009810.0003001/11 FEB 16 ABN-34-00009811.0003001/11 FEB 16
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 3/12
AFM C 14 NOV 17
TR34 Issue 1
(TR 4.02.00/41) - ENG COMPRESSOR VANE/ENG STALL ON GROUND
Ident.: TDU / APPRO-TR-00009728.0001001 / 21 OCT 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 21 OCT 09
Approval reference: 10027686
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This TR is issued in digital format to provide the content of TR 4.02.00/41
and in order to be approved further by the EASA. .
This Temporary Revision requests the flight crew to monitor the potential
occurrence of symptoms in order to prevent stalls during takeoff and climb.
Applicable to: A318 or A319 or A320 or A321 aircraft fitted with CFM 56-5B engines.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00009728.0001001/21 OCT 09 ABN-70-00009732.0001001/21 OCT 09
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 4/12
AFM D 14 NOV 17
TR1 Issue 1
(TR 2.05.00/47) - NON PRECISION APPROACHES WITH OEI
Ident.: TDU / APPRO-TR-00009667.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 23 NOV 09
Approval reference: 10027986
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This TR is issued in digital format to provide the content of TR 2.05.00/47
approved by the DGAC on June 21st, 2001.
Applicable to: SA.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00009667.0001001/23 NOV 09 LIM-22-FMS-00009620.0001001/23 NOV 09
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 5/12
AFM E 14 NOV 17
TR6 Issue 1
(TR 2.05.00/67) - RAM AIR TURBINE (RAT) FLIGHT TESTING
Ident.: TDU / APPRO-TR-00009670.0001001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 23 NOV 09
Approval reference: 10027986
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This TR is issued in digital format to provide the content of TR 2.05.00/67
approved by the EASA under reference EASA.A.A.01088 on November
25th, 2005.
Applicable to: A318-111/-112 or A319 or A320 or A321 aircraft
with Mod 22803 or Mod 27189 Ram Air Turbine (RAT) standards.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00009670.0001001/23 NOV 09 LIM-29-00009631.0001001/23 NOV 09
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 6/12
AFM F 14 NOV 17
TR188 Issue 2
AUTOLAND DATABASES WITH HONEYWELL ADIRU
Ident.: TDU / APPRO-TR-00014157.0003001 / 04 NOV 15 APPROVED
Criteria: (SA and (30652 or 30941 or 30942 or 31105 or 31706))
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 04 NOV 15
Approval reference: 10055306
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This TR is issued because some Honeywell ADIRU magnetic variation
databases are obsolete since 2005. The guaranteed value for the magnetic
heading accuracy is no longer respected in some areas of the world. Some
operational limitations have been assessed when the error between the
magnetic heading and the QFU is greater than 3 °.
Applicable to: SA aircraft with Honeywell ADIRUs.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00014157.0003001/04 NOV 15 LIM-22-FGS-00009711.0009001/04 NOV 15
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 7/12
AFM G 14 NOV 17
TR423 Issue 1
MCDL 54-05 PYLON FAIRING SEAL
Ident.: TDU / APPRO-TR-00015738.0001001 / 29 OCT 14 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 29 OCT 14
Approval reference: 10050974
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This TR provides an update of MCDL item 54-05 in order to change the
quantity of fairing seals installed from 4 to 6 (3 on each pylon).
Applicable to: All A318/A319/A320/A321 aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00015738.0001001/29 OCT 14 MCDL-54-05-00015528.0001001/29 OCT 14
MCDL-54-05-00015527.0001001/29 OCT 14
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 8/12
AFM H 14 NOV 17
TR499 Issue 1
MCDL 78-01 DUCT OPENING ACTUATOR FOR CFM ENGINE
Ident.: TDU / APPRO-TR-00016021.0003001 / 20 MAR 15 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 20 MAR 15
Approval reference: 10052671
Reason for issue: This TR introduces the new MCDL item 78-01 Duct Opening Actuator for
CFM engine.
Applicable to: All A319/A320/A321 aircraft with CFM engine.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016021.0003001/20 MAR 15 MCDL-78-01-00016033.0001001/20 MAR 15
MCDL-78-01-00016031.0001001/20 MAR 15
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 9/12
AFM I 14 NOV 17
TR502 Issue 1
ABNORMAL V ALPHA PROT
Ident.: TDU / APPRO-TR-00016062.0001001 / 05 DEC 14 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 05 DEC 14
Approval reference: 10051494
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This Temporary Revision is issued to provide the Abnormal V Alpha Prot
procedure.
Applicable to: All A318/A319/A320/A321 aircraft
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016062.0001001/05 DEC 14 EMER-34-00016060.0001001/05 DEC 14
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 10/12
AFM J 14 NOV 17
TR566 Issue 1
EMER DESCENT
Ident.: TDU / APPRO-TR-00016716.0001001 / 07 OCT 15 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 07 OCT 15
Approval reference: 10055034
Do not remove this Tempory Revision until instructed to do so.
Reason for issue: This Temporary Revision is issued to cover the update of the EMER
DESCENT procedure: the notification of the emergency descent to the cabin
is postponed after ATC notification.
Applicable to: All A318/A319/A320/A321 aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016716.0001001/07 OCT 15 EMER-90-00016883.0001001/07 OCT 15
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 11/12
AFM K 14 NOV 17
TR556 Issue 1
TOWBARLESS OPERATIONS
Ident.: TDU / APPRO-TR-00016598.0001001 / 09 JUL 15 APPROVED
Criteria: SA
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 09 JUL 15
Approval reference: 10053997
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This Temporary Revision is issued to cover the new ISI reference.
Applicable to: All A318/A319/A320/A321 aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016598.0001001/09 JUL 15 LIM-09-00016592.0001001/09 JUL 15
A319
AIRPLANE FLIGHT MANUAL
APPROVAL DATA
TEMPORARY REVISIONS
GLG A319-112 FLEET APPRO-TR P 12/12
AFM L 14 NOV 17
TR564 Issue 1
MCDL 52-03 ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Ident.: TDU / APPRO-TR-00016654.0001001 / 06 JUL 15 APPROVED
Criteria: (A319 or A321)
Impacted DU: NONE
APPROVAL REFERENCE
APPROVED BY: EASA
Approval date: 06 JUL 15
Approval reference: 10053953
Do not remove this Temporary Revision until instructed to do so.
Reason for issue: This Temporary Revision is issued to update the MCDL item 52-03 ‘Access
Door to Potable Water Filling and Drainage’. The access door 192NB is not
installed on A319 and A321. Therefore, the quantity installed is updated.
Applicable to: A319 and A321 aircraft.
This Temporary Revision is made up of the following Temporary Documentary Units:
APPRO-TR-00016654.0001001/06 JUL 15 MCDL-52-03-00016656.0001001/06 JUL 15
MCDL-52-03-00016655.0001001/06 JUL 15
GENERAL
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
GENERAL
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET GEN-PLP-TOC P 1/2
AFM 07 FEB 17
GEN-INTR INTRODUCTION
Introduction...............................................................................................................................................................A
GEN-DESC AFM DESCRIPTION
Approved AFM Format............................................................................................................................................ A
Customized AFM..................................................................................................................................................... B
Organization of the Manual.....................................................................................................................................C
Documentary Unit (DU)...........................................................................................................................................D
Identification Strip.................................................................................................................................................... E
Approval Information................................................................................................................................................F
AFM Revision.......................................................................................................................................................... G
Temporary Revision (TR)........................................................................................................................................H
GEN-DEF WORDING DEFINITIONS
Warning Definition....................................................................................................................................................A
Caution Definition.....................................................................................................................................................B
Note Definition......................................................................................................................................................... C
LAND ASAP Definition............................................................................................................................................ D
GEN-ABB ABBREVIATIONS
Abbreviations............................................................................................................................................................A
GEN-UNIT UNITS
Correspondence Between Units..............................................................................................................................A
GEN-VIEW 3-VIEW DRAWING
3-View Drawing........................................................................................................................................................A
A319
AIRPLANE FLIGHT MANUAL
GENERAL
PRELIMINARY PAGES
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET GEN-PLP-TOC P 2/2
AFM 07 FEB 17
A319
AIRPLANE FLIGHT MANUAL
GENERAL
INTRODUCTION
GLG A319-112 FLEET GEN-INTR P 1/2
AFM A 07 FEB 17
INTRODUCTION
Ident.: GEN-INTR-00007010.0001001 / 16 JAN 17 APPROVED
Criteria: SA
This Airplane Flight Manual (AFM) is a reference document published in English. It is not established
as an operational document to be used directly by the crew in flight.
Flight crew documents available in flight must include an Operational Manual, with appropriate
contents and language as required by the National Regulations.
Note: Any Flight Crew Operating Manual (FCOM) reference within the AFM must be considered
as advisory information, the FCOM being a non approved document.
This AFM is specific to a given certified aircraft model, which is specified in the Heading Approbation
Documentary Unit (Refer to APPRO-HEAD Heading Approbation).
It was approved by the Direction Générale de l'Aviation Civile (DGAC) prior to 28 September 2003
and is since approved by the European Aviation Safety Agency (EASA), or by Airbus under Design
Organisation Approval (DOA) reference EASA.21J.031 for AFM minor changes. When applicable, it
is approved by the EASA on behalf and according to the requirements of the importing Authority, e.g.
the US Federal Aviation Administration (FAA) for US registered aircraft.
A319
AIRPLANE FLIGHT MANUAL
GENERAL
INTRODUCTION
Intentionally left blank
GLG A319-112 FLEET GEN-INTR P 2/2
AFM 07 FEB 17
A319
AIRPLANE FLIGHT MANUAL
GENERAL
AFM DESCRIPTION
GLG A319-112 FLEET GEN-DESC P 1/4
AFM A to C → 07 FEB 17
APPROVED AFM FORMAT
Ident.: GEN-DESC-00015195.0001001 / 02 DEC 13 APPROVED
Criteria: SA
The AFM is approved in both PDF and Ops Library Browser (OLB) formats.
Note: OLB version 5.1 or higher must be used to consult the AFM in OLB format.
CUSTOMIZED AFM
Ident.: GEN-DESC-00007013.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The customized airline AFM:
‐ Is extracted from a non customized aircraft model envelope AFM
‐ Is an approved document related to an operator's/owner's fleet
‐ Takes into account the specific configuration of each aircraft of the concerned fleet.
Airbus will provide a manual which reflects the aircraft configuration at delivery, and the necessary
revisions to reflect configuration changes due to Airbus approved modifications.
The operator/owner must inform Airbus without delay of the effective changes to the aircraft
delivery configuration made through Airbus Service Bulletin (SB). This allows Airbus to provide AFM
revisions/updates to the operator/owner.
Airbus will not provide revisions, and thus will not assume the responsibility of any effect on the AFM:
‐ Due to modifications installed by third parties without an Airbus SB, and/or
‐ Due to modifications installed through an Airbus SB, if Airbus is not informed of the SB
embodiment.
ORGANIZATION OF THE MANUAL
Ident.: GEN-DESC-00007015.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The AFM is divided into 11 chapters:
‐ Approval data
‐ General
‐ Limitations
‐ Emergency procedures
‐ Abnormal procedures
‐ Normal procedures
‐ Performance (dry and wet runway)
‐ Appendices and supplements
‐ Master Configuration Deviation List (MCDL)
A319
AIRPLANE FLIGHT MANUAL
GENERAL
AFM DESCRIPTION
GLG A319-112 FLEET GEN-DESC P 2/4
AFM ← C to E 07 FEB 17
‐ Supplementary performance (contaminated runway)
‐ Regulatory differences (when applicable).
DOCUMENTARY UNIT (DU)
Ident.: GEN-DESC-00007016.0001001 / 16 JAN 17 APPROVED
Criteria: SA
The AFM is made of Documentary Units (DU). The DU is the smallest part of information with a
technical content.
The DUs are listed on a separate "List of Effective Documentary Unit" (LEDU).
The LEDU is produced and approved by Airbus under the authority of DOA reference EASA.21J.031.
IDENTIFICATION STRIP
Ident.: GEN-DESC-00007017.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Below the title of the DU, an identification strip is provided with each DU and consists of:
‐ Ident.: Each DU is identified by its own unique identification number
‐ The approval date of the DU
‐ The approval marking
Note: For non approved DU, this field is replaced by the label: FOR INFORMATION ONLY.
‐ Criteria: This field provides the type of aircraft and associated configuration for which the DU is
applicable
Note: SA stands for Single Aisle meaning that this DU is applicable to all
A318/A319/A320/A321 family.
‐ Specific: When necessary, this field provides the code of the specific regulation applicable to the
DU
‐ Impacted by TDU: When applicable, this field provides the identification number and the title of the
Temporary Documentary Unit (TDU) impacting the DU
‐ Belonging to: When applicable, this field provides the number of TR to which the TDU belongs
‐ Impacted DU: When applicable, this field provides the identification number and the title of the DU
impacted by the TDU.
A319
AIRPLANE FLIGHT MANUAL
GENERAL
AFM DESCRIPTION
GLG A319-112 FLEET GEN-DESC P 3/4
AFM F to H → 07 FEB 17
APPROVAL INFORMATION
Ident.: GEN-DESC-00020434.0001001 / 16 JAN 17 APPROVED
Criteria: SA
For each DU, the following information is provided in the LEDU:
‐ The approval reference of the DU
‐ The authority/organization that approved the DU
‐ The approval date of the DU.
AFM REVISION
Ident.: GEN-DESC-00007366.0001001 / 16 JAN 17 APPROVED
Criteria: SA
For each revision, a new LEDU is issued.
The LEDU contains:
‐ The DU identification and title
‐ The approval information (Refer to GEN-DESC Approval Information)
‐ The "M" field that may provide the following Evolution Code:
• The "R" letter indicates a revised DU: The content of the DU is updated by the revision. A
vertical line in the margin of the DU locates the modified part
• The "N" letter indicates a new DU introduced by the revision
• The "E" letter indicates an aircraft validity change for the DU: The list of MSNs for which the DU
is effective has been changed compared to the previous LEDU, by addition or deletion of one or
several MSN.
‐ The "T" field (Temporary Information) that contains a cross if the associated DU is a TDU
‐ Other fields that contain the list of MSNs to which the DU applies.
The holder of the AFM must check that the manual is in accordance with the LEDU of the latest
approved revision.
The aircraft model envelope AFM is continuously updated with new or revised technical information.
A revision of the operator/owner AFM is issued based on the latest approved aircraft model envelope
AFM.
In addition, an operator/owner AFM revision may be issued following a fleet modification or an SB
embodiment.
TEMPORARY REVISION (TR)
Ident.: GEN-DESC-00007018.0001001 / 16 JAN 17 APPROVED
Criteria: SA
A Temporary Revision (TR) is related to amendments to be quickly approved and introduced in the
AFM. A TR is made of Temporary Documentary Units (TDU).
A319
AIRPLANE FLIGHT MANUAL
GENERAL
AFM DESCRIPTION
GLG A319-112 FLEET GEN-DESC P 4/4
AFM ← H 07 FEB 17
The TRs are indicated with a dedicated layout and are listed on a separate "List of Effective
Temporary Revisions" (LETR).
A TR always has priority over the AFM content modified by the TR (a TDU always has priority over
the content of the impacted DU).
A319
AIRPLANE FLIGHT MANUAL
GENERAL
WORDING DEFINITIONS
GLG A319-112 FLEET GEN-DEF P 1/2
AFM A to D 16 MAR 15
WARNING DEFINITION
Ident.: GEN-DEF-00007020.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The following is the official definition of a WARNING, taken directly from the CS-25 (Chapter AMC
25.1581, paragraph 3-e) and applicable to Airbus flight operational documentation:
WARNING An operating procedure, technique, etc... which may result in personal injury or loss
of life if not carefully followed.
CAUTION DEFINITION
Ident.: GEN-DEF-00007021.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The following is the official definition of a CAUTION, taken directly from the CS-25 (Chapter AMC
25.1581, paragraph 3-e) and applicable to Airbus flight operational documentation:
CAUTION An operating procedure, technique, etc... which may result in damage to equipment
if not carefully followed.
NOTE DEFINITION
Ident.: GEN-DEF-00006982.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The following is the official definition of a NOTE, taken directly from the CS-25 (Chapter AMC
25.1581, paragraph 3-e) and applicable to Airbus flight operational documentation:
Note: An operating procedure, technique etc... considered essential to emphasize. Information
contained in notes may also be safety related.
LAND ASAP DEFINITION
Ident.: GEN-DEF-00007322.0001001 / 14 JAN 15 APPROVED
Criteria: SA
LAND ASAP (red)
Land as soon as possible at the nearest airport at which a safe landing can be made.
Note: LAND ASAP (red) information is applicable to a time-critical situation.
LAND ASAP (amber)
Consider landing at the nearest suitable airport.
Note: The suitability criteria should be defined in accordance with the Operator's policy.
A319
AIRPLANE FLIGHT MANUAL
GENERAL
WORDING DEFINITIONS
Intentionally left blank
GLG A319-112 FLEET GEN-DEF P 2/2
AFM 16 MAR 15
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 1/10
AFM A → 16 MAR 15
ABBREVIATIONS
Ident.: GEN-ABB-00006976.0001001 / 14 JAN 15 APPROVED
Criteria: SA
A
Abbreviation Term
A/C Aircraft
Advisory Circular
AC Alternative Current
ACD Airworthiness Compliance Document
ACJ Advisory Circular-Joint
ACL ATC Clearance
ACM ATC Communication Management
ACT Additional Center Tank
ADIRU Air Data Inertial Reference Unit
ADR Air Data Reference
ADS-B Automatic Dependent Surveillance-Broadcast
ADS-C Automatic Dependent Surveillance-Contract
AEO All Engines Operative
AFM Airplane Flight Manual
AGL Above Ground Level
AIME Autonomous Integrity Monitoring Extrapolation
ALD Actual Landing Distance
ATC Microphone Check
AMC Acceptable Means of Compliance
AMJ Advisory Material-Joint
AMM Aircraft Maintenance Manual
AOA Angle of Attack
AOC Airlines Operational Control
AP Autopilot
APU Auxiliary Power Unit
AR Authorization Required
ARINC Aeronautical Radio INC
ASD Accelerate Stop Distance
ASDA Accelerate Stop Distance Available
ASI Air Speed Indicator
ATA Air Transport Association
ATC Air Traffic Control
ATS Air Traffic Service
ATSA-AIRB Air Traffic Situational Awareness - Airborne
ATSA-ITP Air Traffic Situational Awareness - In Trail Procedures
ATSA-VSA Air Traffic Situational Awareness - Visual Separation on Approach
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 2/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
ATSAW Airborne Traffic Situational Awareness
ATSU Air Traffic Service Unit
AWO All Weather Operations
B
Abbreviation Term
BC Back Course
BSCU Braking and Steering Control Unit
C
Abbreviation Term
C/B Circuit Breaker
CAA Civil Aviation Authority
CAP Civil Aviation Publication
CAS Calibrated Airspeed
CCOM Cabin Crew Operating Manual
CDL Configuration Deviation List
CDLS Cockpit Door Locking System
CFR Code of Federal Regulations
CG Center of Gravity
CIS Commonwealth of Independent States
CJ Corporate Jet
CLD Certified Landing Distance
CM Context Management
CML Consumable Material List
CMP Configuration, Maintenance and Procedures
CONF Configuration
CPDLC Controller Pilot Datalink Communication
CS Certification Specifications
CSMG Constant Speed Motor Generator
CVR Cockpit Voice Recorder
CWY Clearway
D
Abbreviation Term
DA Decision Altitude
DAC Dual Annular Combustor
D-ATIS Digital Automatic Terminal Information Service
DC Direct Current
DCL Departure Clearance
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 3/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
DGAC Direction Générale de l'Aviation Civile
DH Decision Height
DLIC Data Link Initiation Capability
DMC Display Management Computer
DME Distance Measuring Equipment
DNA Dirección National de Aeronavegabilidad
DO Document Order (RTCA)
Display Unit
DU Documentary Unit
E
Abbreviation Term
EASA European Aviation Safety Agency
ECAM Electronic Centralized Aircraft Monitoring Computer
ED EUROCAE Document
EDTO Extended Diversion Time Operations
EFB Electronic Flight Bag
EFIS Electronic Flight Instrument System
EGPWS Enhanced Ground Proximity Warning System
EGT Exhaust Gas Temperature
EHS Enhanced Surveillance
EIS Electronic Instrument System
ELAC Elevator Aileron Computer
ELT Electronic Locator Transmitter
EMER Emergency
ENG Engine
EPR Engine Pressure Ratio
ESS Essential
Extended range operations for two engine aeroplanes (EASA)
ETOPS Extended operations (FAA)
EWD Engine Warning Display
F
Abbreviation Term
F Fuel
F/CTL Flight Controls
F-PLN Flight Plan
FAA Federal Aviation Administration
FAC Flight Augmentation Computer
FADEC Full Authority Digital Engine Control System
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 4/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
FAF Final Approach Fix
FANS Future Air Navigation System
FAP Final Approach Point
FAR Federal Aviation Regulations
FCDC Flight Control Data Concentrator
FCOM Flight Crew Operating Manual
FCU Flight Control Unit
FD Flight Director
FI Filling Instructions
FLS FMS Landing System
FLX Flex
FM Flight Management
FMA Flight Mode Annunciator
FMGC Flight Management and Guidance Computer
FMGS Flight Management and Guidance System
FMS Flight Management System
FOB Fuel on Board
FPA Flight Path Angle
FPV Flight Path Vector
FQI Fuel Quantity Indication
FU Fuel Used
FWC Flight Warning Computer
G
Abbreviation Term
G/S Glideslope
GBAS Ground-Based Augmentation System
GEN Generator
GLS GPS Landing System
GNSS Global Navigation Satellite System
GPS Global Positioning System
GPWS Ground Proximity Warning System
GSM Global System for Mobile Communication
H
Abbreviation Term
HF High Frequency
HKCAD Hong Kong Civil Aviation Department
HPC High Pressure Compressor
HUD Head Up Display
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 5/10
AFM ← A → 16 MAR 15
I
Abbreviation Term
IAC Instrução de Aviação Civil (Civil Aviation Instruction)
IAC AR Interstate Aviation Committee Aviation Register
IAS Indicated Airspeed
ICAO International Civil Aviation Organization
IDG Integrated Drive Generator
IFR Instrument Flight Rules
IGN Ignition
IL Information Leaflet
ILS Instrument Landing System
IR Inertial Reference
IRS Inertial Reference System
ISA International Standard Atmosphere
ISIS Integrated Standby Instrument System
ISPSS In-Seat Power Supply System
J
Abbreviation Term
JAA Joint Aviation Authorities
JAR Joint Aviation Regulation
JCAB Japan Civil Aviation Bureau
K
Abbreviation Term
KOZ Keep Out Zone
L
Abbreviation Term
L/G Landing Gear
LD Landing Distance
Localizer Directional Aid
LDA Landing Distances Available
LDG Landing
LEDU List of Effective Documentary Unit
LETR List of Effective Temporary Revision
LGCIU Landing Gear Control and Interface Unit
LH Left Hand
LIP Lift Improvement Package
LNAV Lateral Navigation
LOC Localizer
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 6/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
LOC-BC Localizer Back Course
LPV Localizer Performance with Vertical Guidance
LRBL Least Risk Bomb Location
LS Landing System
M
Abbreviation Term
MAC Mean Aerodynamic Chord
MAP Missed Approach Point
MAPSC Maximum Approved Passenger Seating Configuration
MCDL Master Configuration Deviation List
MCDU Multipurpose Control & Display Unit
MCPSC Maximum Certificated Passenger Seating Capacity
MCT Maximum Continuous Thrust
MDA Minimum Descent Altitude
MDH Minimum Descent Height
MEA Minimum En route Altitude
MLE Maximum Landing Gear Extended Mach
MLS Microwave Landing Distance
MLW Maximum Landing Weight
MMEL Master Minimum Equipment List
MMO Maximum Operating Mach
MMR Multi-Mode Receiver
MOPS Minimum Operational Performance Standards
MORA Minimum Off Route Altitude
MSN Manufacturer Serial Number
MTOW Maximum Takeoff Weight
MZFW Maximum Zero Fuel Weight
N
Abbreviation Term
N1 Low Pressure Rotor Speed
N2 High Pressure Rotor Speed
NAI Nose Air Intake
NDB Non-Directional Beacon
NAV Navigation
ND Navigation Display
NPA Non Precision Approach
NSA Norme Sud Aviation
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 7/10
AFM ← A → 16 MAR 15
O
Abbreviation Term
OANS On-board Airport Navigation System
OAT Outside Air Temperature
OCL Oceanic Clearance
OEI One Engine Inoperative
OEW Operational Empty Weight
OLB Ops Library Browser
OLD Operational Landing Distance
OVHT Overheat
OW Operational Weight
P
Abbreviation Term
P/B Pushbutton
PAPI Precision Approach Path Indicator
PAR Precision Approach Radar
PC Personal Computer
PED Portable Electronic Devices
PF Pilot Flying
PFC Porous Friction Course
PFD Primary Flight Display
PM Pilot Monitoring
PTU Power Transfer Unit
PVI Paravisual Indicator
Q
Abbreviation Term
QFE Field Elevation Atmosphere Pressure
QFU Runway Heading
QNH Sea Level Atmosphere Pressure
R
Abbreviation Term
Radio Altimeter
RA Resolution Advisory
RAT Ram Air Turbine
RBS Radio Beacon System
RF Radius to Fix
RH Right Hand
RLD Required Landing Distance
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 8/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
RNAV Area Navigation
RNP Required Navigation Performance
ROP Runway Overrun Protection
ROPS Runway Overrun Prevention System
ROW Runway Overrun Warning
RVR Runway Visual Range
RVSM Reduced Vertical Separation Minima
S
Abbreviation Term
SA Single Aisle
SAAAR Special Aircrew and Aircraft Authorization Required
SAC Single Annular Combustor
SAC-TI Single Annular Combustor- Tech Insertion
SAL Steep Approach Landing
SAT Static Air Temperature
SATCOM Satellite Communication
SB Service Bulletin
SD System Display
SDF Simplified Directional Facility
SEC Spoiler Elevator Computer
SES Single European Sky
SFCC Slat Flap Control Computer
SIL Service Information Letter
SRS Speed Reference System
STAT INV Static Inverter
SWY Stopway
T
Abbreviation Term
TA Traffic Advisory
TAB Tabulation and Interpolation Program
TAT Total Air Temperature
TAWS Terrain Awareness and Warning System
TCAS Traffic Alert and Collision Avoidance System
TDU Temporary Documentary Unit
TGL Temporary Guidance Leaflet
TI Tech Insertion
TO Takeoff
TOD Takeoff Distance
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 9/10
AFM ← A → 16 MAR 15
Continued from the previous page
Abbreviation Term
TODA Takeoff Distance Available
TOGA Takeoff - Go-Around
TOR Takeoff Run
TORA Takeoff Run Available
TR Temporary Revision
TRU Transformer Rectifer Unit
V
Abbreviation Term
V1 Takeoff Decision Speed
V2 Takeoff Safety Speed
VA Maximum Design Maneuvering Speed
VALPHAMAX Speed at Alpha-Max
VAPP Final Approach Speed
VC Design Cruise Speed
V/DEV Vertical Deviation
VDL VHF Data Link
VFE Maximum Flap Extended Speed
VFR Visual Flight Rules
VHF Very High Frequency
VLE Max L/G Extended Speed
VLO Max L/G Operating Speed
VLOF Lift-Off Speed
VLS Lowest Selectable Speed
VMC Visual Meteorological Conditions
VMCA Minimum Control Airspeed
VMCG Minimum Control Speed Ground
VMIN Minimum Operating Speed
VMIN 1G Minimum Operating Speed under 1g Load Factor
VMO Maximum Operating Speed
VNAV Vertical Navigation
VOR VHF Omnidirectional Range
VR Rotation Speed
VREF Landing Reference Speed
VS1G Stall Speed under 1g Load Factor
VSW Stall Warning Speed
A319
AIRPLANE FLIGHT MANUAL
GENERAL
ABBREVIATIONS
GLG A319-112 FLEET GEN-ABB P 10/10
AFM ← A 16 MAR 15
W
Abbreviation Term
WBM Weight and Balance Manual
WV Weight Variant
WX Weather mode (ND)
Z
Abbreviation Term
ZFCG Zero Fuel Center of Gravity
Zp Pressure Altitude
A319
AIRPLANE FLIGHT MANUAL
GENERAL
UNITS
GLG A319-112 FLEET GEN-UNIT P 1/2
AFM A → 25 JAN 11
CORRESPONDENCE BETWEEN UNITS
Ident.: GEN-UNIT-00006979.0001001 / 23 NOV 09 APPROVED
Criteria: SA
METRIC TO US
METRIC US
1 mm 0.0394 in
1 m 3.281 ft
1 m 1.094 yd
LENGTH
1 km 0.540 NM
1 m/s 3.281 ft/s
SPEED 1 km/h 0.540 kt
1 g 0.0353 oz
1 kg 2.204623 lb
WEIGHT
1 t 2 204.623 lb
1 N 0.2248 lb
FORCE 1 daN 2.248 lb
1 bar 14.505 PSI
PRESSURE 1 mbar 0.0145 PSI
1 l 0.2642 US Gal
VOLUME 1 m³ 264.2 US Gal
MOMENTUM 1 daN.m 88.50 lb.in
TEMPERATURE
US TO METRIC
US METRIC
1 in 25.4 mm
1 ft 0.3048 m
1 yd 0.914 m
LENGTH
1 NM 1.852 km
1 ft/s 0.3048 m/s
SPEED 1 kt 1.852 km/h
1 oz 28.35 g
1 lb 0.45359 kg
WEIGHT
1 lb 0.0004536 t
1 lb 4.448 N
FORCE 1 lb 0.4448 daN
1 PSI 0.0689 bar
PRESSURE 1 PSI 68.947 mbar
1 US Gal 3.785 l
VOLUME 1 US Gal 0.003785 m³
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
GENERAL
UNITS
GLG A319-112 FLEET GEN-UNIT P 2/2
AFM ← A 25 JAN 11
Continued from the previous page
US METRIC
MOMENTUM 1 lb.in 0.0113 daN.m
TEMPERATURE
A319
AIRPLANE FLIGHT MANUAL
GENERAL
3-VIEW DRAWING
GLG A319-112 FLEET GEN-VIEW P 1/4
AFM A → 08 APR 11
3-VIEW DRAWING
Ident.: GEN-VIEW-00006880.0004001 / 23 NOV 09 APPROVED
Criteria: A319
Front View
A319
AIRPLANE FLIGHT MANUAL
GENERAL
3-VIEW DRAWING
GLG A319-112 FLEET GEN-VIEW P 2/4
AFM ← A → 08 APR 11
Top View
Side View
WING
Reference area 122.4 m² 1 317 ft² 72 in²
Root chord 6.074 m 19 ft 11 in
MAC (LA) 4.194 m 13 ft 9 in
Aspect ratio 9.396
A319
AIRPLANE FLIGHT MANUAL
GENERAL
3-VIEW DRAWING
GLG A319-112 FLEET GEN-VIEW P 3/4
AFM ← A 08 APR 11
HORIZONTAL TAIL PLANE
Reference area 31 m² 333 ft² 98 in²
MAC (LH) 2.701 m 8 ft 10 in
Aspect ratio 5.00
Distance from 25 % LA to
25 % LH
15.454 m 50 ft 9 in
VERTICAL TAIL PLANE
Reference area 21.51 m² 231 ft² 77 in²
MAC (LV) 3.948 m 12 ft 11 in
Aspect ratio 1.6
Distance from 25 % LA to
25 % LV
14.589 m 47 ft 11 in
A319
AIRPLANE FLIGHT MANUAL
GENERAL
3-VIEW DRAWING
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GLG A319-112 FLEET GEN-VIEW P 4/4
AFM 08 APR 11
LIMITATIONS
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A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET LIM-PLP-TOC P 1/4
AFM 14 NOV 17
LIM-GEN GENERAL
Introduction...............................................................................................................................................................A
Kind of Operations...................................................................................................................................................B
Minimum Flight Crew...............................................................................................................................................C
Maximum Operating Altitude................................................................................................................................... D
Maneuver Limit Load Factors..................................................................................................................................E
Icing Conditions Definition....................................................................................................................................... F
LIM-WGHT WEIGHTS AND LOADING
Weight Limitations....................................................................................................................................................A
Center of Gravity Envelope..................................................................................................................................... B
Performance Limitations..........................................................................................................................................C
Loading.................................................................................................................................................................... D
LIM-SPD AIRSPEEDS
VMO/MMO............................................................................................................................................................... A
VA.............................................................................................................................................................................B
VFE.......................................................................................................................................................................... C
VLO and VLE/MLE..................................................................................................................................................D
LIM-OPS OPERATIONAL PARAMETERS
Environmental Envelope..........................................................................................................................................A
Tailwind.................................................................................................................................................................... B
Runway Slope..........................................................................................................................................................C
LIM-09 TOWING AND TAXIING
Maneuvers on Ground.............................................................................................................................................A
Towbarless Operations............................................................................................................................................B
Towbarless Operations............................................................................................................................................C
LIM-21 AIR COND/PRESS/VENT
Cabin Pressurization................................................................................................................................................A
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET LIM-PLP-TOC P 2/4
AFM 14 NOV 17
Continued from the previous page
LIM-22 AUTO FLIGHT SYSTEM
LIM-22-FMS Flight Management System
General.....................................................................................................................................................................A
Airworthiness Standards Compliance......................................................................................................................B
Navigation Performance.......................................................................................................................................... C
Use of NAV Mode................................................................................................................................................... D
Non Precision Approaches with OEI.......................................................................................................................E
Approaches.............................................................................................................................................................. F
LIM-22-FGS Flight Guidance System
Airworthiness Standards Compliance......................................................................................................................A
Autoland Databases with Honeywell ADIRU...........................................................................................................B
Autoland...................................................................................................................................................................C
Minimum Height for Use of the Autopilot................................................................................................................D
CAT II / CAT III Operations.....................................................................................................................................E
LIM-24 ELECTRICAL POWER
Electrical...................................................................................................................................................................A
LIM-28 FUEL
Fuel and Additive Specifications............................................................................................................................. A
Usable Fuel..............................................................................................................................................................B
Fuel Imbalance........................................................................................................................................................ C
Fuel Temperature Limits......................................................................................................................................... D
LIM-29 HYDRAULIC
Hydraulics Fluid....................................................................................................................................................... A
Ram Air Turbine (RAT)........................................................................................................................................... B
LIM-32 LANDING GEAR
Tire Speed............................................................................................................................................................... A
LIM-34 NAVIGATION
Inertial Reference System (IRS)..............................................................................................................................A
Reduced Vertical Separation Minimum (RVSM)..................................................................................................... B
LIM-46 INFORMATION SYSTEMS
Airline Operation Control Applications.....................................................................................................................A
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET LIM-PLP-TOC P 3/4
AFM 14 NOV 17
Continued from the previous page
LIM-49 AUXILIARY POWER UNIT
Auxiliary Power Unit (APU)..................................................................................................................................... A
LIM-70 POWER PLANT
Main Engines........................................................................................................................................................... A
Engine Parameters.................................................................................................................................................. B
Reverse Thrust........................................................................................................................................................ C
Oil.............................................................................................................................................................................D
Reduced Thrust Takeoff..........................................................................................................................................E
Operations in Icing Conditions.................................................................................................................................F
A319
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LIMITATIONS
PRELIMINARY PAGES
TABLE OF CONTENTS
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GLG A319-112 FLEET LIM-PLP-TOC P 4/4
AFM 14 NOV 17
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
GENERAL
GLG A319-112 FLEET LIM-GEN P 1/2
AFM A to E 14 DEC 13
INTRODUCTION
Ident.: LIM-GEN-00006957.0001001 / 23 NOV 09 APPROVED
Criteria: SA
This aircraft must be operated in compliance with the limitations given in this chapter. When
operating in accordance with an approved appendix or supplement to this AFM, these limitations
apply, unless amended by such appendix or supplement.
KIND OF OPERATIONS
Ident.: LIM-GEN-00006958.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The aircraft is certified in the public transport category (passengers and freight) for day and night
operations, in the following conditions, when the appropriate equipment and instruments required by
the airworthiness and operating regulations are approved, installed and in an operable condition:
‐ VFR and IFR
‐ Extended overwater flight
‐ Flight in icing conditions.
MINIMUM FLIGHT CREW
Ident.: LIM-GEN-00006959.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Minimum flight crew: 2 pilots.
MAXIMUM OPERATING ALTITUDE
Ident.: LIM-GEN-00006960.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 30748)
Slats and flaps retracted: 39 800 ft.
This is the maximum altitude at which it is possible to maintain cabin pressure altitude below 8 000 ft.
Slats and/or flaps extended: 20 000 ft.
MANEUVER LIMIT LOAD FACTORS
Ident.: LIM-GEN-00006961.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Slats and flaps retracted: -1 to +2.5 g.
Slats and/or flaps extended: 0 to +2.0 g.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
GENERAL
GLG A319-112 FLEET LIM-GEN P 2/2
AFM F 14 DEC 13
ICING CONDITIONS DEFINITION
Ident.: LIM-GEN-00009165.0001001 / 23 NOV 09 APPROVED
Criteria: SA
lcing conditions exist when the OAT on the ground and for takeoff, or when TAT in flight, is 10 °C or
below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or
less, rain, snow, sleet and ice crystals).
Icing conditions also exist on the ground and for takeoff when the OAT is 10 °C or below when
operating on ramps, taxiways, or runways where surface snow, standing water, or slush may be
ingested by the engines or freeze on engines, nacelles, or engine sensor probes.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
WEIGHTS AND LOADING
GLG A319-112 FLEET LIM-WGHT P 1/4
AFM A to B → 25 JAN 11
WEIGHT LIMITATIONS
Ident.: LIM-WGHT-00006860.0014001 / 23 NOV 09 APPROVED
Criteria: (A319 and 25328)
Weight Variant : WV 01
Maximum Taxi Weight 70 400 kg 155 205 lb
Maximum Takeoff Weight (MTOW) 70 000 kg 154 323 lb
Maximum Landing Weight (MLW) 61 000 kg 134 481 lb
Maximum Zero Fuel Weight (MZFW) 57 000 kg 125 663 lb
Minimum Weight 35 400 kg 78 044 lb
Note: 1. Refer to LIM-WGHT Center of Gravity Envelope.
2. The maximum weight limits also depend on the center of gravity and may be lower than
the values given in the above table.
CENTER OF GRAVITY ENVELOPE
Ident.: LIM-WGHT-00006861.0131001 / 23 NOV 09 APPROVED
Criteria: ((319-111 or 319-112 or 319-113 or 319-114 or 319-131 or 319-132) and 25328)
For Mean Aerodynamic Chord (MAC) and datum, see 3 - View Drawing. Refer to GEN-VIEW 3-View
Drawing.
Takeoff and landing CG limits are given for landing gear down configuration.
Flight CG limits are given for landing gear up configuration.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
WEIGHTS AND LOADING
GLG A319-112 FLEET LIM-WGHT P 2/4
AFM ← B to C → 25 JAN 11
CG Envelope WV 01
PERFORMANCE LIMITATIONS
Ident.: LIM-WGHT-00006962.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum Takeoff Weight (MTOW) and Maximum Landing Weight (MLW) may be reduced by
performance requirements of PERFORMANCE and or SUPPLEMENTARY PERFORMANCE
chapters of this AFM related to :
‐ Climb performance (first and second segment, final takeoff, en route, approach and landing)
‐ Available runway length (takeoff and landing)
‐ Obstacle clearance (takeoff and en route)
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
WEIGHTS AND LOADING
GLG A319-112 FLEET LIM-WGHT P 3/4
AFM ← C to D 25 JAN 11
‐ Brake energy limit (observe brake temperature warning (300 °C))
‐ Tire speed.
LOADING
Ident.: LIM-WGHT-00006963.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The aircraft must be loaded in accordance with the loading instructions given in the Weight and
Balance Manual (WBM) chapter 1-10.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
WEIGHTS AND LOADING
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GLG A319-112 FLEET LIM-WGHT P 4/4
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AIRSPEEDS
GLG A319-112 FLEET LIM-SPD P 1/2
AFM A to B → 25 JAN 11
VMO/MMO
Ident.: LIM-SPD-00007065.0001001 / 23 NOV 09 APPROVED
Criteria: SA
MAXIMUM OPERATING LIMIT SPEED (VMO/MMO)
VMO = 350 kt IAS
MMO = M 0.82
This limit must not be intentionally exceeded in any flight regime.
VA
Ident.: LIM-SPD-00007319.0004001 / 23 NOV 09 APPROVED
Criteria: A319
MAXIMUM DESIGN MANEUVERING SPEED (VA)
Note: This limitation only applies in alternate or direct flight control laws.
VA
If alternate or direct law is active:
‐ Full ailerons and rudder application should be confined to speeds below VA
‐ Manoeuvres involving angle of attack near stall should be confined to speeds below VA.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AIRSPEEDS
GLG A319-112 FLEET LIM-SPD P 2/2
AFM ← B to D 25 JAN 11
CAUTION Rapid and large alternating control inputs, especially in combination with large
changes in pitch, roll or yaw (e.g. large sideslip angles) may result in structural
failures at any speed, even below VA.
VFE
Ident.: LIM-SPD-00006883.0004001 / 23 NOV 09 APPROVED
Criteria: (320-231 or 320-232 or 320-233 or A318 or A319)
MAXIMUM SLATS/FLAPS EXTENDED SPEEDS OR OPERATING SPEEDS (VFE)
Flight Phase Slats Position Flaps Position Flaps Lever Position VFE
Intermediate approach 18 ° 0 ° 1 230 kt IAS
Takeoff 1+F 18 ° 10 ° 1 215 kt IAS
Approach and takeoff 22 ° 15 ° 2 200 kt IAS
Approach, takeoff
and landing 22 ° 20 ° 3 185 kt IAS
Landing 27 ° 40 ° FULL 177 kt IAS
VLO AND VLE/MLE
Ident.: LIM-SPD-00007317.0001001 / 23 NOV 09 APPROVED
Criteria: SA
MAXIMUM SPEED DURING LANDING GEAR EXTENSION
VLO = 250 kt IAS
MAXIMUM SPEED DURING LANDING GEAR RETRACTION
VLO = 220 kt IAS
MAXIMUM SPEED WITH LANDING GEAR LOCKED DOWN
VLE/MLE = 280 kt IAS / M 0.67
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
OPERATIONAL PARAMETERS
GLG A319-112 FLEET LIM-OPS P 1/2
AFM A to B 25 JAN 11
ENVIRONMENTAL ENVELOPE
Ident.: LIM-OPS-00006919.0015001 / 23 NOV 09 APPROVED
Criteria: ((A319 or 321-200) and 30748)
TAILWIND
Ident.: LIM-OPS-00007309.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum tailwind for takeoff and landing: 10 kt
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
OPERATIONAL PARAMETERS
GLG A319-112 FLEET LIM-OPS P 2/2
AFM C 25 JAN 11
RUNWAY SLOPE
Ident.: LIM-OPS-00007310.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum mean runway slope: ± 2 %
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
TOWING AND TAXIING
GLG A319-112 FLEET LIM-09 P 1/2
AFM A to C 30 JUL 15
MANEUVERS ON GROUND
Ident.: LIM-09-00007357.0001001 / 23 NOV 09 APPROVED
Criteria: SA
During towing, ±85 ° of nosewheel travel must not be exceeded.
Note: Mechanical stop is designed at ±95 ° of nosewheel travel.
TOWBARLESS OPERATIONS
Ident.: TDU / LIM-09-00016592.0001001 / 09 JUL 15 APPROVED
Criteria: SA
Impacted DU: 00007358 Towbarless Operations
Belongs to TR556 Issue 1
Towbarless operations on nose landing gear (towing and pushback) are approved provided
the towbarless towing operations are performed in compliance with appropriate operational
requirements, using towbarless towing vehicles that are qualified and operated to preclude damage
to the aircraft nosewheel steering system, or which provide a reliable and unmistakable warning
when damage to the steering system may have occurred. Towbarless towing vehicles that are
specifically accepted for the Airbus A318/A319/A320/A321 aircraft are listed in Airbus WISE
In-Service Information ISI 09.11.00001.
TOWBARLESS OPERATIONS
Ident.: LIM-09-00007358.0001001 / 03 AUG 10 APPROVED
Criteria: SA
Impacted by TDU: 00016592 Towbarless Operations
Towbarless operations on nose landing gear (towing and pushback) are approved provided
the towbarless towing operations are performed in compliance with appropriate operational
requirements, using towbarless towing vehicles that are qualified and operated to preclude damage
to the aircraft nosewheel steering system, or which provide a reliable and unmistakable warning
when damage to the steering system may have occurred. Towbarless towing vehicles that are
specifically accepted for the Airbus A318/A319/A320/A321 aircraft are listed in Airbus Service
Information Letter SIL 09-002.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
TOWING AND TAXIING
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GLG A319-112 FLEET LIM-09 P 2/2
AFM 30 JUL 15
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AIR COND/PRESS/VENT
GLG A319-112 FLEET LIM-21 P 1/2
AFM A 25 JAN 11
CABIN PRESSURIZATION
Ident.: LIM-21-00007261.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum safety relief differential pressure: 8.6 PSI (600 hPa).
Maximum negative differential pressure: -1 PSI ( -70 hPa).
Note: The ram air inlet must only be opened when the cabin differential pressure is less than
+1 PSI (70 hPa).
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AIR COND/PRESS/VENT
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GLG A319-112 FLEET LIM-21 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT MANAGEMENT SYSTEM
GLG A319-112 FLEET LIM-22-FMS P 1/4
AFM A to B → 14 APR 17
GENERAL
Ident.: LIM-22-FMS-00009567.0002001 / 23 NOV 09 APPROVED
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
The FMGS lateral and vertical navigation has been certified for after takeoff, en route and terminal
area operations, and for instrument approach procedures (except ILS, LOC, LOC-BC, LDA, SDF,
GLS and MLS) and missed approach procedures.
Approval of the FMGS is based on the assumption that the navigation database has been
validated for intended use. The airworthiness approval does not account for database accuracy or
compatibility.
Obstacle clearance and adherence to airspace constraints remains a flight crew responsibility.
Fuel, time predictions/performance information is provided for advisory purpose only.
For instrument procedures not coded in the WGS-84 coordinate system, the GPS must be
deselected, unless the shift between the local coordinate system and the WGS-84 is found
acceptable for the intended operation.
Note: 1. The assessment of this shift can be done:
‐ In flight, monitoring the navaid raw data in non RNAV procedures
‐ On ground, performing a GPS survey of the procedure waypoints.
2. RNAV (GPS) and RNP RNAV approach procedures require WGS-84 coordinates and
GPS PRIMARY.
AIRWORTHINESS STANDARDS COMPLIANCE
Ident.: LIM-22-FMS-00009568.0016001 / 13 MAR 17 APPROVED
Criteria: ((A319 or A320 or A321) and ((31896 or 31897) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635)))
The FMGS has been demonstrated to comply with applicable airworthiness requirements, including
FAA AC 20-130A, for a navigation system integrating multiple navigation sensors, when operating
with aircraft position based on:
‐ IRS position and GPS update, or
‐ IRS position and radio navaid update, or
‐ IRS position only.
The FMGS also complies with the airworthiness part of:
‐ EASA AMC 20-4 (or JAA TGL 2 Rev 1) for Basic RNAV
‐ EASA AMC 20-27 for RNP APPROACH (RNP APCH) Operations with or without APV
BARO-VNAV Operations
‐ FAA Advisory Circular 90-105A for RNP2 operations in domestic, oceanic and remote continental
area
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT MANAGEMENT SYSTEM
GLG A319-112 FLEET LIM-22-FMS P 2/4
AFM ← B to C → 14 APR 17
‐ FAA AC 90-105 for:
• RNP1 operations in Terminal area with or without RF leg
• RNP APCH operations with or without APV BARO-VNAV Operations in final approach segment
• RNP APCH operations with or without RF leg capability in the initial, the intermediate and the
missed approach segments.
Note: 1. RNP APCH without APV BARO-VNAV operation corresponds to RNAV(GNSS)
approach with LNAV Minimum.
2. RNP APCH with APV BARO-VNAV operation corresponds to RNAV(GNSS) approach
with LNAV/VNAV Minimum.
‐ JAA TGL 10 for Precision RNAV (compliance with paragraph 8.2 has not been demonstrated)
‐ FAA Advisory Circular 20-129 for baro VNAV
‐ FAA Advisory Circular 90-100A for terminal and en route RNAV operations
‐ FAA Order 8400.33 for RNP 4 in oceanic and remote area
‐ FAA Order 8400.12A for RNP 10 in oceanic and remote area.
RNP 10 oceanic/remote area operations are approved:
• With GPS PRIMARY
• Without GPS PRIMARY (GPS deselected or inoperative), provided time limitations in IRS only
navigation, acceptable to the operational authorities, are established.
Note: Compliance with the applicable airworthiness requirements does not constitute an
operational approval. Such authorization must be obtained by the operator from the
appropriate authorities.
NAVIGATION PERFORMANCE
Ident.: LIM-22-FMS-00009569.0003001 / 23 NOV 09 APPROVED
Criteria: ((A319 or A320 or A321) and ((31896 or 31897 or 32475 or 32929) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or
30631 or 30635)))
With GPS PRIMARY:
The FMGS is certified in accordance with the performance requirements of MASPS
ED-75/DO-236 for RNP RNAV operations.
The RNP accuracy with GPS PRIMARY has been demonstrated to be :
With AP ON in NAV With AP OFF and
FD ON in NAV
With AP OFF
and FD OFF
En Route 1 NM 1 NM 1.1 NM
In Terminal Area 0.5 NM 0.51 NM 0.51 NM
In Approach 0.3 NM 0.3 NM Not authorized
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT MANAGEMENT SYSTEM
GLG A319-112 FLEET LIM-22-FMS P 3/4
AFM ← C to E 14 APR 17
Without GPS PRIMARY:
The FMGS is certified in accordance with the accuracy requirements and assumptions of
MASPS ED-75/DO-236 for RNP RNAV operations provided the appropriate RNP value is
checked or entered on the MCDU and HIGH accuracy is displayed.
Without GPS PRIMARY (GPS deselected or inoperative) the navigation accuracy is a function of
ground radio navaid infrastructure or elapsed time since last radio update.
USE OF NAV MODE
Ident.: LIM-22-FMS-00009570.0003001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
NAV mode may be used:
‐ After takeoff provided:
• GPS PRIMARY is available, or
• FMGS takeoff updating has been checked.
‐ In terminal area provided:
• GPS PRIMARY is available, or
• HIGH accuracy is displayed and the appropriate RNP is checked or entered on the MCDU, or
• FMS navigation is cross-checked with Navaid raw data.
NAV, or NAV and APP NAV and FINAL APP mode may be used for VOR, VOR/DME, NDB,
NDB/DME or RNAV(GNSS) approach but not for ILS, LOC, LOC-BC, LDA, SDF, GLS or MLS final
approach.
NON PRECISION APPROACHES WITH OEI
Ident.: TDU / LIM-22-FMS-00009620.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Impacted DU: NONE
Belongs to TR1 Issue 1
In the case of One Engine Inoperative, the use of autopilot is not allowed to perform Non Precision
Approaches in the following flight modes:
‐ FINAL APP
‐ NAV/VS
‐ NAV/FPA.
Note: The use of FD in NAV mode remains authorized.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT MANAGEMENT SYSTEM
GLG A319-112 FLEET LIM-22-FMS P 4/4
AFM F 14 APR 17
APPROACHES
Ident.: LIM-22-FMS-00009571.0002001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320 or A321) and ((25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635) and (31896 or 31897 or
32401 or 32402 or 32475 or 32929)))
VOR, VOR/DME, NDB or NDB/DME approach procedures may be performed, in NAV, or NAV and
APP NAV and FINAL APP mode, provided AP or FD is used and:
‐ GPS PRIMARY is available. In this case, the reference navaid may be unserviceable, or the
airborne radio equipment may be inoperative, or not installed, provided an operational approval is
obtained.
‐ GPS PRIMARY is not available. In this case, the reference navaid and the corresponding airborne
equipment are serviceable, tuned and monitored during the approach.
RNAV(GNSS) approaches may be performed, in NAV, or NAV and APP NAV and FINAL APP mode
provided GPS PRIMARY is available and with AP or FD engaged.
RNAV(GNSS) approaches with LNAV/VNAV Minimum must be performed in FINAL APP mode.
Note: The RNAV(GNSS) approach limitations and procedures must be used to fly a RNAV
approach where the GPS is not required.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT GUIDANCE SYSTEM
GLG A319-112 FLEET LIM-22-FGS P 1/4
AFM A to B → 10 OCT 17
AIRWORTHINESS STANDARDS COMPLIANCE
Ident.: LIM-22-FGS-00009235.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The Flight Management and Guidance System (FMGS) with the associated equipment has been
found to meet the airworthiness requirements and performance criteria of:
‐ JAR 25
‐ ACJ 25.1329 for automatic flight system
‐ JAR AWO Subpart 1 - Automatic landing systems
‐ JAR AWO Subpart 2 - Category 2 operations
‐ JAR AWO Subpart 3 - Category 3 operations.
Note: Compliance with the standards noted above does not constitute an approval to conduct
category II or III operations. Such authorization must be obtained by the operator from the
appropriate authorities.
AUTOLAND DATABASES WITH HONEYWELL ADIRU
Ident.: TDU / LIM-22-FGS-00009711.0009001 / 04 NOV 15 APPROVED
Criteria: (SA and (30652 or 30941 or 30942 or 31105 or 31706))
Impacted DU: NONE
Belongs to TR188 Issue 2
The below table provides for each concerned airport, the dates when the following limitations begin:
‐ AUTOLAND is not allowed
‐ ROLLOUT is not allowed.
CAT II approaches without AUTOLAND are still allowed.
Airport Code Airport location Month/year
FAEL
EAST LONDON BEN SCHOEMAN SOUTH AFR
REP
August 2018
PAFA FAIRBANKS INTL AK USA January 2015
PANC ANCHORAGE INTL AK USA October 2015
BIKF KEFLAVIK ICELAND January 2015
EGAA BELFAST ALDERGROVE UNITED KINGDOM September 2020
EGPF GLASGOW UNITED KINGDOM July 2020
EGPH EDINBURGH UNITED KINGDOM September 2020
EFRO ROVANIEMI FINLAND September 2019
EFOU OULU FINLAND August 2020
Note: This TR is applicable until end of 2020. From 2021, without a revision of this TR,
AUTOLAND and ROLLOUT will not be allowed on any airport.
The above limitations do not apply if three new ADIRU with updated magnetic variation tables are
installed and Operators ensure previous standards are not installed.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT GUIDANCE SYSTEM
GLG A319-112 FLEET LIM-22-FGS P 2/4
AFM ← B to D 10 OCT 17
The following Honeywell ADIRU standards will cancel the limitations of this Temporary Revision:
‐ ADIRU 4 MCU P/N HG2030BE03 installed by modification 38480
‐ ADIRU 4 MCU P/N HG2030BE04 installed by modification 154407
‐ ADIRU 4 MCU P/N HG2030AC08 installed by modification 37784
‐ ADIRU 4 MCU P/N HG2030AE23 installed by modification 35793
‐ ADIRU 4 MCU P/N HG2030AC13 installed by modification 37806
‐ ADIRU 4 MCU P/N HG2030AD13 installed by modification 37785
‐ ADIRU 4 MCU P/N HG2030AE43 installed by modification 156889
‐ ADIRU 4 MCU P/N HG2030AD33 installed by modification 156844
‐ Or any later approved standards.
AUTOLAND
Ident.: LIM-22-FGS-00009238.0003001 / 02 DEC 13 APPROVED
Criteria: (((320-211 or 320-212 or 320-214) and 24617) or (319-111 or 319-112 or 319-113 or 319-114 or 319-115))
Autoland has been demonstrated:
‐ With CAT II and CAT III ILS beam, with ILS slope angle inside a range of -2.5 ° and -3.15 °
‐ For an airport that has an elevation between -1 000 ft and 9 200 ft.
Performance of ROLL OUT mode has been demonstrated on dry and wet runways.
One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3
DUAL capability must be displayed on FMA.
MINIMUM HEIGHT FOR USE OF THE AUTOPILOT
Ident.: LIM-22-FGS-00009242.0001001 / 28 MAR 17 APPROVED
Criteria: (A318 or A319 or A320)
At takeoff : 100 ft AGL and at least 5 seconds after liftoff.
In approach using FINAL APP, NAV
FPA, NAV V/S, TRK FPA, HDG V/S
: 250 ft AGL.
In circling approach : 500 ft AGL.
In ILS approach if CAT 2 or CAT 3
capability is not displayed on FMA
: 160 ft AGL.
In ILS approach when CAT 2 or CAT 3
capability is displayed on FMA
:Refer to LIM-22-FGS CAT II / CAT III Operations.
After a manual go-around : 100 ft AGL.
In all other flight phases : 500 ft AGL.
The use of AP and FD in OPEN DES and DES mode is not permitted if FCU altitude set below
MDA/MDH or 500 ft AGL whichever is higher.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT GUIDANCE SYSTEM
GLG A319-112 FLEET LIM-22-FGS P 3/4
AFM E → 10 OCT 17
CAT II / CAT III OPERATIONS
Ident.: LIM-22-FGS-00009243.0013001 / 11 AUG 17 APPROVED
Criteria: A319
CATEGORY II AUTOMATIC APPROACH WITHOUT AUTOMATIC LANDING
Minimum decision height: 100 ft
One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3
DUAL capability must be displayed on FMA.
Minimum height for AP disconnection: 80 ft
CATEGORY II AUTOMATIC APPROACH WITH AUTOMATIC LANDING
Minimum decision height: 100 ft
One autopilot at least must be engaged in APPR mode and CAT 2 or CAT 3 SINGLE or CAT 3
DUAL capability must be displayed on FMA.
CATEGORY III FAIL PASSIVE (SINGLE) AUTOMATIC APPROACH AND AUTOMATIC LANDING
Minimum decision height: 50 ft
One autopilot at least must be engaged in APPR mode and CAT 3 SINGLE or CAT 3 DUAL
capability must be displayed on FMA.
CATEGORY III FAIL OPERATIONAL (DUAL) AUTOMATIC APPROACH AND AUTOMATIC
LANDING
Alert height: 100 ft
CAT III with DH:
Two autopilots must be engaged in APPR mode and CAT 3 DUAL capability must be
displayed on FMA.
CAT III without DH:
Two autopilots must be engaged in APPR mode and CAT 3 DUAL capability must be
displayed on FMA.
Minimum Runway Visual Range (RVR): 75 m
MAXIMUM WIND CONDITIONS FOR CAT II OR CAT III AUTOMATIC APPROACH OR
AUTOMATIC LANDING AND AUTOMATIC ROLLOUT
With all engines operative (AEO):
CONF FULL with airport elevation at or below 5 750 ft
Headwind: 20 kt
Tailwind: 10 kt
Crosswind: 20 kt
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUTO FLIGHT SYSTEM
FLIGHT GUIDANCE SYSTEM
GLG A319-112 FLEET LIM-22-FGS P 4/4
AFM ← E 10 OCT 17
CONF FULL with airport elevation above 5 750 ft or CONF 3:
Headwind: 20 kt
Tailwind: 5 kt
Crosswind: 20 kt
With one engine inoperative (OEI):
CONF FULL with airport elevation at or below 5 750 ft
Headwind: 15 kt
Tailwind: 10 kt
Crosswind: 10 kt
CONF FULL with airport elevation above 5 750 ft or CONF 3:
Headwind: 15 kt
Tailwind: 5 kt
Crosswind: 10 kt
AUTOMATIC ROLLOUT LIMITATION: USE OF REVERSE
With one engine inoperative or one thrust reverser inoperative, the use of the remaining thrust
reverser is permitted provided no more than idle reverser thrust is used.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
ELECTRICAL POWER
GLG A319-112 FLEET LIM-24 P 1/2
AFM A 25 JAN 11
ELECTRICAL
Ident.: LIM-24-00007263.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum continuous load per generator (100 %): 90 KVA
Maximum continuous load per TRU: 200 A
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
ELECTRICAL POWER
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GLG A319-112 FLEET LIM-24 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
FUEL
GLG A319-112 FLEET LIM-28 P 1/4
AFM A to B 12 SEP 17
FUEL AND ADDITIVE SPECIFICATIONS
Ident.: LIM-28-00007246.0001001 / 02 DEC 13 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
The fuel system has been certified with: JET A1, JET B, JP4, JET A, JP5, JP8, RT, TS-1 and N° 3
JET.
Note: 1. See engine model specification.
2. See Airbus Consumable Material List (CML) Part 1 / S01-Fuels at the latest issue for
approved fuel specifications.
USABLE FUEL
Ident.: LIM-28-00007248.0003001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or 320-200)
Fuel loading varies with specific fuel gravity without any fuel weight limitation.
Tanks Fuel Quantity
2 Wing Tanks 15 609 l 4 123 US Gal
1 Center Tank 8 250 l 2 179 US Gal
Total 23 859 l 6 303 US Gal
Fuel Specific Gravity
0.80 kg/l 6.676 lb/US GalTanks
Fuel Weight
2 Wing Tanks 12 487 kg 27 525 lb
1 Center Tank 6 600 kg 14 547 lb
Total 19 087 kg 42 078 lb
Note: When the quantity indications reach "zero" the remaining fuel cannot safely be used.
WARNING Takeoff on center tank feeding is prohibited.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
FUEL
GLG A319-112 FLEET LIM-28 P 2/4
AFM C 12 SEP 17
FUEL IMBALANCE
Ident.: LIM-28-00007254.0015001 / 11 AUG 17 APPROVED
Criteria: (A319 or A320)
FUEL IMBALANCE AT TAKEOFF
INNER TANKS (OUTER BALANCED)
Tank Fuel Quantity
(Heavier Tank) Maximum Asymmetry
Full 500 kg (1 102 lb)
3 000 kg (6 613 lb) 1 050 kg (2 314 lb)
1 450 kg (3 196 lb) 1 450 kg (3 196 lb)
With linear interpolation between these values.
OUTER TANKS (INNER BALANCED)
Maximum Asymmetry 370 kg (815 lb)
FUEL IMBALANCE IN FLIGHT AND AT LANDING
INNER TANKS (OUTER BALANCED)
Tank Fuel Quantity
(Heavier Tank) Maximum Asymmetry
Full 1 500 kg (3 306 lb)
4 300 kg (9 479 lb) 1 600 kg (3 527 lb)
2 250 kg (4 960 lb) 2 250 kg (4 960 lb)
With linear interpolation between these values (No limitation below 2 250 kg / 4 960 lb).
OUTER TANKS (INNER BALANCED)
Maximum Asymmetry 690 kg (1 521 lb)
Higher outer wing tank asymmetry (up to the max outer tank quantity: one full/one empty) is
allowed provided:
‐ Fuel content of one side (outer + inner) is equal to the fuel content of the other side (outer +
inner), or
‐ Inner tank fuel quantity on the empty outer tank side is equal or higher, up to 3 t higher, than
the opposite inner tank.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
FUEL
GLG A319-112 FLEET LIM-28 P 3/4
AFM D 12 SEP 17
FUEL TEMPERATURE LIMITS
Ident.: LIM-28-00007259.0002001 / 23 NOV 09 APPROVED
Criteria: ((320-111 and 20024) or (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216))
MINIMUM:
Fuel temperature must not be less than:
JET A: -36 °C
JP5: -42 °C
JET A1, JP8, N° 3 JET: -43 °C
JET B: -46 °C
JP4: -54 °C
RT, TS-1: -45 °C
When using JET A:
If TAT reaches -34 °C, call ECAM fuel page and monitor that fuel temperature remains higher
than -36 °C.
MAXIMUM:
JET A1, JET A, JP5, JP8, RT, TS-1, N° 3 JET: +54 °C
JET B or JP4: +49 °C
When using JP4 or JET B :
Fuel in center tank is to be regarded as unusable if the wing fuel temperature exceeds the
following values before engine start and if the given flight level is exceeded before the center
tank fuel has been used :
+30 °C not above FL 350
+40 °C not above FL 300
+49 °C not above FL 250
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AIRPLANE FLIGHT MANUAL
LIMITATIONS
FUEL
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GLG A319-112 FLEET LIM-28 P 4/4
AFM 12 SEP 17
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
HYDRAULIC
GLG A319-112 FLEET LIM-29 P 1/2
AFM A to B 25 JAN 11
HYDRAULICS FLUID
Ident.: LIM-29-00007262.0001001 / 23 NOV 09 APPROVED
Criteria: SA
FLUID SPECIFICATIONS :
Refer to NSA 307-110
MAX OPERATING PRESSURE (AT ZERO DELIVERY) :
3 000 PSI ± 200 PSI (207 bar ± 14 bar)
RAM AIR TURBINE (RAT)
Ident.: TDU / LIM-29-00009631.0001001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Impacted DU: NONE
Belongs to TR6 Issue 1
In the case of RAT deployment flight testing, limit the speed to 250 kt from RAT deployment to
landing.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
HYDRAULIC
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GLG A319-112 FLEET LIM-29 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
LANDING GEAR
GLG A319-112 FLEET LIM-32 P 1/2
AFM A 25 JAN 11
TIRE SPEED
Ident.: LIM-32-00011074.0001001 / 03 AUG 10 APPROVED
Criteria: SA
Maximum tire speed: 195 kt (ground speed).
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
LANDING GEAR
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GLG A319-112 FLEET LIM-32 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
NAVIGATION
GLG A319-112 FLEET LIM-34 P 1/2
AFM A to B 14 NOV 17
INERTIAL REFERENCE SYSTEM (IRS)
Ident.: LIM-34-00007264.0001001 / 10 NOV 17 APPROVED
Criteria: ((A318 or A320) or ((A319 or A321) and (25204 or 30400 or 30941 or 31105 or 31706 or 33600 or 35793)) or ((A319 or A321) and
(151772 or 24785 or 25294 or 26001)))
The IRS are compliant with the position accuracy criteria of AC 25.4 and FAR 121 appendix G for a
flight time up to 16 h (i.e. in excess of the aircraft range).
The ground alignment of the IRS has been demonstrated to be acceptable between 73 ° North and
73 ° South.
If all ADIRUs have the same magnetic variation table:
Flights using the NAV mode are prohibited:
‐ North of 73 ° North, and
‐ South of 60 ° South.
If one ADIRU has a different magnetic variation table:
Flights using the NAV mode are prohibited:
‐ North of 60 ° North, between 30 ° West and 160 ° West, and
‐ North of 73 ° North, and
‐ South of 55 ° South.
REDUCED VERTICAL SEPARATION MINIMUM (RVSM)
Ident.: LIM-34-00007359.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and (25861 or 25910 or 25952 or 31039 or 31528))
Aircraft have been certified capable to participate in RVSM operations according to JAA TGL 6 and
FAA 91-RVSM requirements.
Note: Compliance with the standard noted above does not constitute an operational approval.
Such authorization must be obtained by the operator from the appropriate authorities.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
NAVIGATION
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GLG A319-112 FLEET LIM-34 P 2/2
AFM 14 NOV 17
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
INFORMATION SYSTEMS
GLG A319-112 FLEET LIM-46 P 1/2
AFM A 25 JAN 11
AIRLINE OPERATION CONTROL APPLICATIONS
Ident.: LIM-46-00006965.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 27522)
The Air Traffic Service Unit (ATSU) equipment has been approved for the provision of Airlines
Operational Control (AOC) applications.
The definition of the AOC application and obtaining its subsequent approval, is the responsibility of
the operator.
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
INFORMATION SYSTEMS
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GLG A319-112 FLEET LIM-46 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
AUXILIARY POWER UNIT
GLG A319-112 FLEET LIM-49 P 1/2
AFM A 25 JAN 11
AUXILIARY POWER UNIT (APU)
Ident.: LIM-49-00007260.0003001 / 23 NOV 09 APPROVED
Criteria: (SA and (25888 or 37987))
One Allied Signal APU 131-9[A].
APU PARAMETERS:
Maximum EGT: 675 °C
Maximum for start:
• 1 090 °C at altitudes below 35 000 ft
• 1 120 °C at altitudes at or above 35 000 ft
Maximum rotor speed: 107 %
OIL SPECIFICATIONS:
Model Specification 31-12048A-3A.
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LIMITATIONS
AUXILIARY POWER UNIT
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GLG A319-112 FLEET LIM-49 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
POWER PLANT
GLG A319-112 FLEET LIM-70 P 1/2
AFM A to D → 13 JUN 17
MAIN ENGINES
Ident.: LIM-70-00007233.0021001 / 03 AUG 10 APPROVED
Criteria: 319-112
Two CFM 56-5B6/P or two CFM 56-5B6/3 or two CFM 56-5B6/P with "TI HPC Kit".
ENGINE PARAMETERS
Ident.: LIM-70-00007235.0002001 / 11 MAY 17 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
Maximum Rotor Speed
Operating Condition Time Limit ENG Indicated
EGT Limit N1 N2
Starting (1) 725 °C ---- ----
Maximum Continuous CONT. 915 °C ---- ----
Normal 5 min 950 °C 104 % 105 %
Takeoff and
Go-around One ENG OUT 10 min 950 °C 104 % 105 %
(1) For ground starts (automatic or manual), a 20 s pause is required between successive cycles. A
15 min cooling period is required, subsequent to four failed cycles.
Note: The N1 value is dependent upon ambient conditions and engine air bleed configuration,
these may limit the N1 to a value lower than that given in this table (see performance
chapter of this AFM).
REVERSE THRUST
Ident.: LIM-70-00007236.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The selection of the thrust reversers in flight or their preselection before touchdown is prohibited.
On ground, backing the aircraft with use of reverse thrust is not permitted.
OIL
Ident.: LIM-70-00007232.0002001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
SPECIFICATION:
Service Bulletin CFMI 56-5B N° 79-001.
MINIMUM PRESSURE:
13 PSI
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
POWER PLANT
GLG A319-112 FLEET LIM-70 P 2/2
AFM ← D to F 13 JUN 17
MAXIMUM TEMPERATURE:
• 140 °C for continuous operation
• 155 °C for transient operation (limited to 15 min).
REDUCED THRUST TAKEOFF
Ident.: LIM-70-00007239.0008001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 320-215) or ((319-111 or 319-112) and 32619) or (319-112 and 33239))
Takeoff at reduced thrust is allowed only if the aircraft meets all performance requirements at the
takeoff weight, with the operating engines at the thrust available for the flex temperature.
Takeoff at reduced thrust is allowed with any inoperative item affecting the performance only if the
associated performance shortfall has been applied to meet above requirements.
Note: Allowed inoperative items may be identified through DISPATCH WITH INOPERATIVE
ITEMS chapter of this AFM (Refer to APP-INOP General) or through MMEL.
Takeoff at reduced thrust is not allowed on contaminated runways.
The flex temperature must not be:
‐ Higher than ISA + 60 (in order that the amount of thrust reduction does not exceed 25 % of the full
rated takeoff thrust)
‐ Lower than the flat rating temperature or actual OAT.
Takeoff at reduced thrust is not allowed unless the operator establishes a means to verify the
availability of takeoff thrust, to ensure that engine deterioration does not exceed authorized limits.
OPERATIONS IN ICING CONDITIONS
Ident.: LIM-70-00006881.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The engine anti-ice must be ON during all ground and flight operations when icing conditions exist or
are anticipated, except during climb and cruise when the temperature is below -40 °C SAT.
The engine anti-ice must be ON prior to and during descent in icing conditions, including
temperatures below -40 °C SAT.
Note: Do not rely on airframe visual icing cues to turn engine anti-ice on. Use the temperature
and visual moisture criteria specified the icing conditions definition (Refer to LIM-GEN Icing
Conditions Definition).
Delaying the use of engine anti-ice until buildup is visible from the cockpit may result in
severe engine damage and/or flameout.
EMERGENCY PROCEDURES
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A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET EMER-PLP-TOC P 1/2
AFM 12 SEP 17
EMER-GEN GENERAL
INTRODUCTION......................................................................................................................................................A
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE...................................................... B
EMER-21 AIR COND/PRESS/VENT
CAB PR - EXCESS CAB ALT................................................................................................................................ A
CAB PR - EXCESS RESIDUAL PR........................................................................................................................B
EMER-24 ELECTRICAL POWER
ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED)...................................................................... A
EMER-26 FIRE/SMOKE
GENERAL................................................................................................................................................................ A
ENG 1 (2) FIRE (In Flight)......................................................................................................................................B
ENG 1 (2) FIRE (On Ground).................................................................................................................................C
APU FIRE................................................................................................................................................................ D
SMOKE - FWD or AFT CARGO SMOKE............................................................................................................... E
SMOKE/FUMES/AVNCS SMOKE........................................................................................................................... F
REMOVAL OF SMOKE/FUMES............................................................................................................................. G
EMER-27 FLIGHT CONTROLS
F/CTL - L + R ELEV FAULT...................................................................................................................................A
F/CTL - FLAP LVR NOT ZERO..............................................................................................................................B
EMER-29 HYDRAULIC
HYD - G + B SYS LO PR.......................................................................................................................................A
HYD - B + Y SYS LO PR....................................................................................................................................... B
HYD - G + Y SYS LO PR.......................................................................................................................................C
EMER-32 LANDING GEAR
L/G - GEAR NOT DOWNLOCKED.........................................................................................................................A
LOSS OF BRAKING................................................................................................................................................B
EMER-34 NAVIGATION
Abnormal V Alpha Prot............................................................................................................................................A
EMER-70 POWER PLANT
DUAL ENG FAILURE (BOTH ENGINES FLAME OUT)......................................................................................... A
ENG - 1(2) OIL LO PR........................................................................................................................................... B
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET EMER-PLP-TOC P 2/2
AFM 12 SEP 17
Continued from the previous page
EMER-90 MISCELLANEOUS
STALL RECOVERY.................................................................................................................................................A
EMER DESCENT.................................................................................................................................................... B
EMER DESCENT.................................................................................................................................................... C
EMERGENCY EVACUATION................................................................................................................................. D
DITCHING................................................................................................................................................................E
FORCED LANDING.................................................................................................................................................F
Emergency Landing (All Engines Failure).............................................................................................................. G
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
GENERAL
GLG A319-112 FLEET EMER-GEN P 1/2
AFM A to B → 08 AUG 17
INTRODUCTION
Ident.: EMER-GEN-00007037.0001001 / 14 JAN 15 APPROVED
Criteria: SA
The procedures contained in this chapter have been established and are recommended by the
aircraft manufacturer for application in the event of a serious failure.
The following important remarks apply:
1. It is assumed that, in general, all failures are indicated by the operation of specific system
warnings and/or by direct observation.
2. The actions recommended may result in the loss of certain systems not associated with the failure.
3. For a definition of LAND ASAP, Refer to GEN-DEF LAND ASAP Definition.
When actions depend on a condition, a dot (•) or a square (■) identifies this condition. The square is
used when there is a choice between one or more conditions and only one is applicable.
These procedures are approved by the Airworthiness Authorities as acceptable procedures, for
operation of the aircraft. This approval does not prevent the operator from developing equivalent
procedures provided these procedures are approved by appropriate Operational Authorities.
In case of discrepancy between procedures displayed on the ECAM and procedures stated in the
AFM, the AFM procedures always have precedence.
Unless otherwise specified in the procedures, the minimum speed to be used for approach and
landing is the VLS corresponding to the configuration requested by the procedure.
Note: VLS, when mentioned in a procedure, is the one corresponding to the configuration
requested by the procedure (e.g. if the procedure requests to use FLAPS 2, take VLS of
CONF 2).
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE
Ident.: EMER-GEN-00015177.0001001 / 14 JUL 17 APPROVED
Criteria: SA
RUNWAY CONDITION DETERMINATION
The flight crew shall obtain the runway condition and/or the depth and type of runway contaminant
to make the basic assessment of actual condition. Estimated Surface Friction (Mu) or Pilot Reports
of Braking Action (PiRep) or similar qualitative information may be used in addition.
Landing distance determination must not consider a better Braking Action than the one related to
the runway condition.
Runway Condition Max Reported Braking Action
Dry 6 - DRY
Wet 5 - GOOD
Compacted Snow 4 - GOOD to MEDIUM
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
GENERAL
GLG A319-112 FLEET EMER-GEN P 2/2
AFM ← B 08 AUG 17
Continued from the previous page
Runway Condition Max Reported Braking Action
More than 3 mm of Dry or Wet Snow 3 - MEDIUM
More than 3 mm of Standing Water or Slush 2 - MEDIUM to POOR
Ice (Cold and Dry) 1 - POOR
LANDING DISTANCE DETERMINATION
The landing distance to be applied in the case of failure is the Operational Landing Distance
(OLD).
The OLD can be determined by selecting the failure case in the IN-FLIGHT FAILURE field of
the AFM_OCTO interface, using the database given in the PERFORMANCE chapter of this
manual (Refer to PERF-OCTO Performance Database), combined with LSAE05.fail file using the
AFM_OCTO approved FM module at revision 32 or higher.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
AIR COND/PRESS/VENT
GLG A319-112 FLEET EMER-21 P 1/2
AFM A to B 14 DEC 13
CAB PR - EXCESS CAB ALT
Ident.: EMER-21-00007053.0004001 / 02 DEC 13 APPROVED
Criteria: (SA and 37871)
If above FL 100:
Use crew oxygen masks.
If below FL 160:
Initiate descent to the higher one of: FL 100 or MEA.
If above FL 160:
Turn on cabin signs.
Initiate emergency descent to the higher one of: FL 100 or MEA. Refer to EMER-90 EMER
DESCENT
If cabin altitude above 14 000 ft:
Manually confirm passengers oxygen masks on.
CAB PR - EXCESS RESIDUAL PR
Ident.: EMER-21-00009326.0001001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and 35220)
Turn off both packs.
Alert cabin crew.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
AIR COND/PRESS/VENT
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GLG A319-112 FLEET EMER-21 P 2/2
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
ELECTRICAL POWER
GLG A319-112 FLEET EMER-24 P 1/2
AFM A 14 DEC 13
ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED)
Ident.: EMER-24-00006884.0003001 / 02 DEC 13 APPROVED
Criteria: ((A320 and 28160) or (A318 or A319 or A321))
LAND ASAP
Minimum RAT speed: 140 kt
Turn off then on all generators one after the other.
If no generator reset successful:
Set BUS TIE to OFF.
Attempt a further all generators reset.
If any generator reset is successful:
Turn off then on both FACs one after the other.
If generator reset still unsuccessful:
Note: 1. For communications, only VHF 1 and ATC 1 are available.
2. Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT
LOST).
3. Engines are fed by gravity. Refer to ABN-28 FUEL GRAVITY FEEDING.
4. The Cockpit Door Locking System (CDLS) is inoperative (if installed).
Manually confirm emergency electrical power on.
Set ENG MODE selector to IGN START.
Turn off then on FAC 1.
Set BUS TIE to AUTO.
Start APU if available.
Set ventilation blower and extract to OVRD.
For approach and landing:
Note: Slats and flaps extend slowly.
Apply necessary landing performance corrections.
Note: 1. Antiskid is inoperative. Refer to ABN-32 BRAKES - A-SKID N-WS FAULT or OFF.
2. Half spoilers are inoperative.
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EMERGENCY PROCEDURES
ELECTRICAL POWER
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GLG A319-112 FLEET EMER-24 P 2/2
AFM 14 DEC 13
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AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 1/8
AFM A to B 16 MAR 15
GENERAL
Ident.: EMER-26-00007038.0001001 / 14 JAN 15 APPROVED
Criteria: SA
Whenever fire is encountered on the aircraft, landing at the nearest airport is recommended.
After conducting any fire suppression/smoke evacuation procedure, even though smoke has
dissipated, if it has not or cannot be visibly verified that the fire has been put out, immediately land at
the nearest airport.
The flight crew should always go to 100 % oxygen whenever a hand held fire extinguisher is to be
discharged in the cockpit or when required because of smoke accumulation.
ENG 1 (2) FIRE (IN FLIGHT)
Ident.: EMER-26-00007041.0001001 / 23 NOV 09 APPROVED
Criteria: SA
LAND ASAP
Shut down affected engine and push relevant FIRE pushbutton.
Discharge AGENT 1 after 10 s.
Notify ATC.
If fire not extinguished after 30 s:
Discharge AGENT 2.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 2/8
AFM C to D 16 MAR 15
ENG 1 (2) FIRE (ON GROUND)
Ident.: EMER-26-00007042.0002001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and ((20067 or 20069) and (36847 or 37871)))
Set all thrust levers to idle.
Note: Full thrust reversers may be used to stop the aircraft.
When aircraft stopped:
Set parking brake to ON.
Notify ATC.
Alert cabin crew.
Shut down affected engine and push relevant FIRE pushbutton.
Discharge all fire agents of affected engine.
Shut down other engine.
If evacuation required:
Initiate evacuation.
Shut down APU.
APU FIRE
Ident.: EMER-26-00007043.0001001 / 23 NOV 09 APPROVED
Criteria: SA
LAND ASAP
Push APU FIRE pushbutton.
Discharge agent after 10 s.
Shut down APU.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 3/8
AFM E 16 MAR 15
SMOKE - FWD OR AFT CARGO SMOKE
Ident.: EMER-26-00009335.0004001 / 23 NOV 09 APPROVED
Criteria: (SA and (37871 and (20067 or 20069)))
LAND ASAP
Turn off affected cargo compartment isolation valves (as installed).
Turn off cabin fans (if installed).
Discharge affected cargo compartment agent (as installed).
After landing:
When aircraft stopped:
Disembark passengers before opening cargo doors.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 4/8
AFM F → 16 MAR 15
SMOKE/FUMES/AVNCS SMOKE
Ident.: EMER-26-00007044.0006001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320 or A321) and (31276 and 37871))
If perceptible smoke is confirmed:
LAND ASAP
Use crew oxygen masks, if required.
Set ventilation blower and extract to OVRD.
Turn off cabin fans and galleys.
Turn on cabin signs.
Establish communication between cockpit and cabin.
Try to identify and isolate faulty equipment.
If smoke source not immediately isolated:
Initiate a diversion.
Initiate a descent to the higher one of: FL 100 or MEA-MORA.
At any time of the procedure, if smoke/fumes becomes the greatest threat:
Consider applying the removal of smoke/fumes procedure and setting Elec Emer Config.
Refer to EMER-26 REMOVAL OF SMOKE/FUMES.
Note: To set Elec Emer Config, turn off EMER ELEC GEN 1 LINE and set EMER ELEC
PWR to MAN ON then, when EMER GEN is available, turn off GEN 2 and APU
GEN.
Apply the Elec Emer Config procedure without performing generator reset. Refer
to EMER-24 ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED).
Before landing gear extension, restore normal electrical supply for landing: turn on
GEN 2 and EMER ELEC GEN 1 LINE.
At any time of the procedure, if the situation becomes unmanageable:
Consider landing immediately.
If air conditioning smoke suspected:
Turn off APU bleed.
Set ventilation blower and extract to AUTO.
Close all cargo isolation valves.
Turn off pack 1.
If smoke continues:
Turn on pack 1.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 5/8
AFM ← F 16 MAR 15
Continued from the previous page SMOKE/FUMES/AVNCS SMOKE
Turn off pack 2.
If smoke still continues:
Turn on pack 2.
Set ventilation blower and extract to OVRD.
Consider removal of smoke/fumes procedure. Refer to EMER-26 REMOVAL OF
SMOKE/FUMES.
If cabin equipment smoke suspected:
If smoke continues:
Turn on emergency exit lights.
Turn off COMMERCIAL.
Check smoke dissipation and try to identify and isolate faulty equipment.
If smoke still continues or when faulty equipment confirmed isolated:
Turn on COMMERCIAL.
Consider removal of smoke/fumes procedure. Refer to EMER-26 REMOVAL OF
SMOKE/FUMES.
If smoke source cannot be determined and still continues or avionics/electrical
smoke suspected:
Consider setting Elec Emer Config.
Note: To set Elec Emer Config, turn off EMER ELEC GEN 1 LINE and set EMER ELEC
PWR to MAN ON then, when EMER GEN is available, turn off GEN 2 and APU
GEN.
Apply the Elec Emer Config procedure without performing generator reset. Refer
to EMER-24 ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED).
3 min before landing or 2 000 ft above airport altitude, restore normal electrical
supply for landing: turn on GEN 2 and EMER ELEC GEN 1 LINE.
If smoke disappears within 5 min:
Restore normal ventilation.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 6/8
AFM G → 16 MAR 15
REMOVAL OF SMOKE/FUMES
Ident.: EMER-26-00007045.0001001 / 14 JAN 15 APPROVED
Criteria: (A319 or A320)
Turn on emergency exit lights.
If fuel vapors:
Turn on CAB FANS.
Turn off both packs.
If no fuel vapors:
Turn off CAB FANS.
Set PACK FLOW to HI.
Set landing elevation to the higher one of: 10 000 ft or MEA-MORA.
Descend to the higher one of: FL 100 or MEA-MORA.
Notify ATC.
While descending, continue applying the appropriate steps of the smoke/fumes/avncs smoke
procedure.
When at FL 100 or MEA-MORA:
If electrical emergency configuration:
Set APU master switch to ON.
Turn off both packs.
Use manual pressurization mode.
Maintain the cabin vertical speed switch in the UP position.
Turn on RAM AIR when cabin differential pressure below 1 PSI.
Set APU master switch to OFF.
If smoke persists and PM cockpit window opening required:
Maximum speed: 200 kt
Open cockpit door.
Put headsets on.
Open PM cockpit window.
When window open:
Turn on non affected pack(s) and continue applying the appropriate steps of the
smoke/fumes/avncs smoke procedure.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
GLG A319-112 FLEET EMER-26 P 7/8
AFM ← G 16 MAR 15
Continued from the previous page REMOVAL OF SMOKE/FUMES
CAUTION Due to the increased noise level pay particular attention to visual warnings.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FIRE/SMOKE
Intentionally left blank
GLG A319-112 FLEET EMER-26 P 8/8
AFM 16 MAR 15
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET EMER-27 P 1/2
AFM A to B 14 DEC 13
F/CTL - L + R ELEV FAULT
Ident.: EMER-27-00007051.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
Note: 1. Pitch mechanical back up.
2. Roll is in direct law.
Use manual pitch trim.
Do not use speed brakes.
Maximum speed: 320 kt/M 0.77
Use FLAPS 3 for landing.
Set GPWS LDG FLAP 3 to ON.
Approach speed = VREF + 10 kt
Apply necessary landing performance corrections.
F/CTL - FLAP LVR NOT ZERO
Ident.: EMER-27-00009325.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and (28479 or 28916))
Set flaps lever to 0.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
FLIGHT CONTROLS
Intentionally left blank
GLG A319-112 FLEET EMER-27 P 2/2
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
HYDRAULIC
GLG A319-112 FLEET EMER-29 P 1/4
AFM A 14 DEC 13
HYD - G + B SYS LO PR
Ident.: EMER-29-00007048.0001001 / 02 DEC 13 APPROVED
Criteria: ((A320 and 35220) or A319)
LAND ASAP
Note: 1. Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
2. Ailerons and left elevator are inoperative.
Maneuver with care.
If blue system has been lost by ELEC PUMP LO PR:
Manually confirm RAT on.
Minimum RAT speed: 140 kt
Turn off associated pumps.
Do not use speed brakes.
For approach and landing:
Note: Flaps extend slowly.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
Note: If slats retracted, extend landing gear only below 200 kt.
Approach speed = VREF + 25 kt
Apply necessary landing performance corrections.
Note: 1. Slats are inoperative.
2. Spoilers are partially inoperative.
3. Nosewheel steering is inoperative.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
HYDRAULIC
GLG A319-112 FLEET EMER-29 P 2/4
AFM B 14 DEC 13
HYD - B + Y SYS LO PR
Ident.: EMER-29-00007049.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320)
LAND ASAP
Note: 1. Flight controls are in normal law.
2. Right elevator is inoperative.
Maneuver with care.
If yellow system has been lost by ENG 2 PUMP LO PR:
Turn on YELLOW ELEC PUMP.
If blue system has been lost by ELEC PUMP LO PR:
Manually confirm RAT on.
Minimum RAT speed: 140 kt
Turn off associated pumps.
Do not use speed brakes.
For approach and landing:
Note: Slats and flaps extend slowly.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
Apply necessary landing performance corrections.
Note: Spoilers are partially inoperative.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
HYDRAULIC
GLG A319-112 FLEET EMER-29 P 3/4
AFM C 14 DEC 13
HYD - G + Y SYS LO PR
Ident.: EMER-29-00007050.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320)
LAND ASAP
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Maneuver with care.
Turn off PTU.
Turn off associated pumps.
If yellow system has been lost by ENG 2 PUMP LO PR:
Turn on YELLOW ELEC PUMP.
For approach and landing:
Note: Slats extend slowly.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
Approach speed = VREF + 25 kt
Apply necessary landing performance corrections.
Note: 1. Flaps are inoperative.
2. Most spoilers are inoperative.
3. Stabilizer control is inoperative.
4. Antiskid is inoperative.
5. Nosewheel steering is inoperative.
Apply maximum brake pressure: 1 000 PSI.
Note: Brakes are on YELLOW ACCU. Only 7 full brake applications are available.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
HYDRAULIC
Intentionally left blank
GLG A319-112 FLEET EMER-29 P 4/4
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
LANDING GEAR
GLG A319-112 FLEET EMER-32 P 1/2
AFM A to B 25 AUG 15
L/G - GEAR NOT DOWNLOCKED
Ident.: EMER-32-00007052.0001001 / 04 APR 11 APPROVED
Criteria: SA
Recycle landing gear.
If unsuccessful after 2 min:
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
LOSS OF BRAKING
Ident.: EMER-32-00009809.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If autobrake selected:
Take over brake control with brake pedals.
If no braking available:
Apply maximum reverse thrust.
Release brake pedals.
Turn off antiskid.
Press brake pedals.
Apply maximum brake pressure 1 000 PSI.
If still no braking:
Use short and successive applications of the parking brake.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
LANDING GEAR
Intentionally left blank
GLG A319-112 FLEET EMER-32 P 2/2
AFM 25 AUG 15
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
NAVIGATION
GLG A319-112 FLEET EMER-34 P 1/2
AFM A 06 JAN 15
ABNORMAL V ALPHA PROT
Ident.: TDU / EMER-34-00016060.0001001 / 05 DEC 14 APPROVED
Criteria: SA
Impacted DU: NONE
Belongs to TR502 Issue 1
At any time, with a speed above VLS, if the aircraft goes to a continuous nose down
pitch rate that cannot be stopped with backward sidestick inputs, immediately:
Keep on one ADR.
Turn off two ADRs.
If the Alpha Max strip (red) hides completely the Alpha Prot strip (black and amber) in a
stabilized wings-level flight path (without an increase in load factor):
Keep on one ADR.
Turn off two ADRs.
In case of dispatch with one ADR inoperative, switch only one ADR to OFF.
CAUTION RISK OF ERRONEOUS DISPLAY OF THE VSW STRIP (RED AND BLACK)
Consider using the Flight Path Vector (FPV).
If the Alpha Prot strip (black and amber) rapidly moves by more than 30 kt during flight
maneuvers (with an increase in load factor), with AP ON and speed brakes retracted:
Keep on one ADR.
Turn off two ADRs.
In case of dispatch with one ADR inoperative, switch only one ADR to OFF.
CAUTION RISK OF ERRONEOUS DISPLAY OF THE VSW STRIP (RED AND BLACK)
Consider using the Flight Path Vector (FPV).
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
NAVIGATION
Intentionally left blank
GLG A319-112 FLEET EMER-34 P 2/2
AFM 06 JAN 15
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
POWER PLANT
GLG A319-112 FLEET EMER-70 P 1/2
AFM A → 25 JAN 11
DUAL ENG FAILURE (BOTH ENGINES FLAME OUT)
Ident.: EMER-70-00007039.0011001 / 23 NOV 09 APPROVED
Criteria: (319-111 or 319-112 or 319-115)
LAND ASAP
Note: 1. Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
2. Wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
The minimum speed for correct CSMG operation is 140 kt.
Manually confirm emergency electrical power on.
Set all thrust levers to idle.
Turn off then on FAC 1.
Note: For communications, only VHF 1 and ATC 1 are available.
If there is fuel remaining on board:
Attempt engines relight with optimum relight speed 300 kt.
Refer to ABN-70 ENG RELIGHT IN FLIGHT.
Determine landing strategy.
Notify ATC.
If no engine relight after 30 s:
Set both engine master levers to OFF during 30 s then ON.
If engine relight unsuccessful:
Use crew oxygen masks above FL 100.
Start APU when below FL 250.
When below FL 200 and APU available:
Turn off wing anti-ice and re-attempt engines relight (one at a time) using APU
bleed.
If engine relight still unsuccessful:
Optimum speed: green dot
Prepare cabin and cockpit.
Turn on cabin signs.
Turn off galleys and COMMERCIAL (if installed).
Use rudder with care.
Turn on RAM AIR when below FL 150.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
POWER PLANT
GLG A319-112 FLEET EMER-70 P 2/2
AFM ← A to B 25 JAN 11
Continued from the previous page DUAL ENG FAILURE (BOTH ENGINES FLAME OUT)
If no fuel on board:
Optimum speed: 215 kt then green dot.
Determine landing strategy.
Notify ATC.
Use crew oxygen masks above FL 100.
Prepare cabin and cockpit.
Turn on cabin signs.
Turn off galleys and COMMERCIAL (if installed).
Use rudder with care.
Turn on RAM AIR when below FL 150.
For approach and landing:
Minimum approach speed: 150 kt
Use FLAPS 3 for landing.
Note: 1. Flaps are inoperative.
2. Slats extend slowly.
If forced landing anticipated:
Apply forced landing procedure. Refer to EMER-90 FORCED LANDING.
If ditching anticipated:
Apply ditching procedure. Refer to EMER-90 DITCHING.
Note: 1. Antiskid is inoperative. Refer to ABN-32 BRAKES - A-SKID N-WS FAULT or OFF.
2. Most spoilers are inoperative.
ENG - 1(2) OIL LO PR
Ident.: EMER-70-00007040.0001001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
If OIL PR below 13 PSI:
Shut down affected engine.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 1/8
AFM A to B 12 SEP 17
STALL RECOVERY
Ident.: EMER-90-00013505.0001001 / 04 APR 11 APPROVED
Criteria: SA
Apply nose down pitch control.
Use lateral control to level wings.
When out of stall:
Smoothly increase thrust as needed.
Check that speed brakes are retracted.
Smoothly recover the flight path.
If in clean configuration and below 20 000 ft:
Select FLAPS 1.
EMER DESCENT
Ident.: TDU / EMER-90-00016883.0001001 / 07 OCT 15 APPROVED
Criteria: SA
Impacted DU: 00006626 EMER DESCENT
Belongs to TR566 Issue 1
Use crew oxygen masks.
Turn on cabin signs.
Initiate an emergency descent.
Set all thrust levers to idle (if autothrust is not active).
Extend full speed brakes.
Descend at the maximum appropriate speed.
CAUTION If structural damage suspected, reduce speed as appropriate and maneuver with
care.
Set ENG START selector to IGN START.
Notify ATC of the nature of emergency.
Notify the cabin of emergency descent.
Consider squawk 7700 on ATC transponder.
Maximum flight level is the higher one of: FL 100 or MEA-MORA.
If cabin altitude above 14 000 ft:
Manually confirm passengers oxygen masks on.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 2/8
AFM C 12 SEP 17
EMER DESCENT
Ident.: EMER-90-00006626.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Impacted by TDU: 00016883 EMER DESCENT
Use crew oxygen masks.
Notify the cabin of emergency descent.
Turn on cabin signs.
Initiate an emergency descent.
Set all thrust levers to idle (if autothrust not engaged).
Extend full speed brakes.
Descend at maximum appropriate speed to the higher one of: FL 100 or MEA-MORA.
CAUTION If structural damage suspected, reduce speed as appropriate and maneuver with
care.
Set ENG START selector to IGN START.
Notify ATC of the nature of emergency.
Consider squawk 7700 on ATC transponder.
Maximum flight level is the higher one of: FL 100 or MEA-MORA.
If cabin altitude above 14 000 ft:
Manually confirm passengers oxygen masks on.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 3/8
AFM D 12 SEP 17
EMERGENCY EVACUATION
Ident.: EMER-90-00006625.0001001 / 23 NOV 09 APPROVED
Criteria: SA
When aircraft stopped:
Set parking brake to ON.
Notify ATC with VHF 1.
Alert cabin crew.
If MAN CAB PR has been used:
Check cabin differential pressure at zero before opening the doors.
Set both engine master levers to OFF.
Push all FIRE pushbuttons (engines and APU).
Discharge all fire agents (engines and APU) as required.
If evacuation required:
Initiate evacuation.
If evacuation not required:
Notify cabin crew and passengers to remain seated.
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 4/8
AFM E → 12 SEP 17
DITCHING
Ident.: EMER-90-00006622.0002001 / 14 JAN 15 APPROVED
Criteria: ((A319 or A320 or A321) and 31276)
Notify ATC and cabin crew of the nature of emergency or use transponder (if available) as required.
Prepare cockpit and cabin.
Turn off TAWS - GPWS.
Turn on cabin signs.
Turn on emergency exit lights.
Turn off COMMERCIAL.
Set landing elevation to sea level.
If time and conditions permit:
Turn on Emergency Locator Transmitter (ELT) (if installed).
For approach:
Keep landing gear up.
Use maximum available slats/flaps.
Note: In case of dual engine failure, use FLAPS 3.
Set ENG MODE selector to NORM.
At 2 000 ft AGL:
Check CAB PR MODE SEL is in AUTO position.
Turn off all bleeds (engines and APU).
Notify cabin crew for ditching.
Set DITCHING to ON.
Note: Touchdown should be made at 11 ° pitch attitude with minimum aircraft vertical speed.
At 500 ft AGL:
Order brace for impact.
At touchdown:
Set both engine master levers to OFF.
Shut down APU.
After ditching:
Notify ATC with VHF 1.
Push all FIRE pushbuttons (engines and APU).
Discharge all fire agents (engines and APU).
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 5/8
AFM ← E 12 SEP 17
Continued from the previous page DITCHING
Initiate evacuation.
Check emergency locator transmitter is emitting (if installed).
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 6/8
AFM F → 12 SEP 17
FORCED LANDING
Ident.: EMER-90-00006621.0002001 / 14 JAN 15 APPROVED
Criteria: ((A319 or A320 or A321) and 31276)
Notify ATC and cabin crew of the nature of emergency or use transponder (if available) as required.
Prepare cockpit and cabin.
Turn off TAWS - GPWS.
Turn on cabin signs.
Turn on emergency exit lights.
Turn off COMMERCIAL.
Manually set the landing elevation.
If time and conditions permit:
Turn on Emergency Locator Transmitter (ELT) (if installed).
For approach:
Turn on RAM AIR.
Extend landing gear.
Note: In case of dual engine failure, extend landing gear by gravity. Refer to ABN-32 L/G
GRAVITY EXTENSION.
Use maximum available slats/flaps.
Note: In case of dual engine failure, use FLAPS 3.
Arm ground spoilers.
Maximum brake pressure: 1 000 PSI.
At 2 000 ft AGL:
Notify cabin crew for landing.
At 500 ft AGL:
Order brace for impact.
At touchdown:
Set both engine master levers to OFF.
Shut down APU.
After landing:
When aircraft stopped:
Set parking brake to ON.
Notify ATC with VHF 1.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 7/8
AFM ← F 12 SEP 17
Continued from the previous page FORCED LANDING
Push all FIRE pushbuttons (engines and APU).
Discharge all fire agents (engines and APU).
If evacuation required:
Initiate evacuation.
If evacuation not required:
Notify cabin crew and passengers to remain seated.
Check emergency locator transmitter is emitting (if installed).
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET EMER-90 P 8/8
AFM G 12 SEP 17
EMERGENCY LANDING (ALL ENGINES FAILURE)
Ident.: EMER-90-00021836.0002001 / 11 AUG 17 APPROVED
Criteria: (A319 or A320 or A321)
Start APU (if available).
Use FLAPS 2.
Approach speed:
GW(t) 40 50 60 70 80 90 95
GW(1000 lb) 90 110 130 155 175 200 210
VAPP(kt) 150 150 163 173 183 193 198
For ditching:
Keep landing gear up.
Set DITCHING to ON.
For forced landing:
Arm ground spoilers.
Extend landing gear by gravity Refer to ABN-32 L/G GRAVITY EXTENSION
At 500 ft AGL or below:
Order brace for impact.
For flare:
Touchdown should be made with minimum aircraft vertical speed, and for ditching target 11 °
pitch attitude.
At touchdown:
Set both engine master levers to OFF.
Shut down APU.
Apply Emergency Evacuation procedure: Refer to EMER-90 EMERGENCY EVACUATION.
ABNORMAL PROCEDURES
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 1/6
AFM 08 AUG 17
ABN-GEN GENERAL
INTRODUCTION......................................................................................................................................................A
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE...................................................... B
ABN-OEI ONE ENGINE INOPERATIVE
ABN-OEI-TO TAKEOFF
ENGINE FAILURE BEFORE V1 (REJECTED TAKEOFF)..................................................................................... A
ENGINE FAILURE BETWEEN V1 AND V2............................................................................................................B
ENGINE FAILURE DURING INITIAL CLIMB OUT.................................................................................................C
ABN-OEI-LDG APPROACH AND LANDING
APPROACH AND LANDING...................................................................................................................................A
MISSED APPROACH (FROM INTERMEDIATE APPROACH CONFIGURATION)................................................B
BALKED LANDING..................................................................................................................................................C
ABN-21 AIR COND/PRESS/VENT
AIR - PACK 1 + 2 FAULT.......................................................................................................................................A
CAB PR - SYS 1 + 2 FAULT..................................................................................................................................B
CAB PR - SAFETY VALVE OPEN......................................................................................................................... C
COND - HOT AIR FAULT.......................................................................................................................................D
VENT - SKIN VALVE FAULT..................................................................................................................................E
ABN-22 AUTO FLIGHT SYSTEM
ABN-22-AUTOFLT AUTO FLIGHT SYSTEM
AUTO FLT - FCU 1(2) FAULT................................................................................................................................A
AUTO FLT - RUD TRV LIM SYS............................................................................................................................B
AUTO FLT - FAC 1+2 FAULT................................................................................................................................ C
AUTO FLT - YAW DAMPER SYS.......................................................................................................................... D
ABN-22-CATII FAILURES OR WARNINGS DURING A CAT II APPROACH WITH OR WITHOUT
AUTOMATIC LANDING
Multiple Failures or Warnings (CAT II)....................................................................................................................A
Altitude Loss with Autopilot Malfunction (CAT II)....................................................................................................B
Failure Leading to Slats/Flaps less than FLAPS 3 (CAT II)................................................................................... C
Antiskid System and/or Nosewheel Steering Failure (CAT II)................................................................................ D
Alpha Floor Activation (CAT II)............................................................................................................................... E
One Engine Failure (CAT II)....................................................................................................................................F
Red "RA" Flag on two PFDs (CAT II).................................................................................................................... G
Amber "CHECK ATT" Flag on two PFDs (CAT II)................................................................................................. H
Red "ATT" Flag on one PFD (CAT II)......................................................................................................................I
Diagonal Line or "INVALID DATA" on one PFD and one ND (CAT II)....................................................................J
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 2/6
AFM 08 AUG 17
Continued from the previous page
Amber "CHECK HDG" Flag on two PFDs and on two NDs (CAT II)......................................................................K
Red "HDG" Flag on one PFD and one ND (CAT II)............................................................................................... L
Red "SPD" Flag on one PFD (CAT II)................................................................................................................... M
"AP OFF" Warning (CAT II).................................................................................................................................... N
Loss of "CAT 2" Capability (CAT II)....................................................................................................................... O
LOC or G/S Excessive Deviation on PFD (CAT II).................................................................................................P
"AUTOLAND" Light (CAT II)................................................................................................................................... Q
A/THR Fault (CAT II)...............................................................................................................................................R
No "LAND" at 350 ft (CAT II)..................................................................................................................................S
Incorrect Selected Course at 350 ft > 5 deg (CAT II).............................................................................................T
No "FLARE" at 30 ft (CAT II)..................................................................................................................................U
ABN-22-CATIIIDH FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
Multiples Failures or Warnings (CAT III with DH)................................................................................................... A
Failure Leading to Slats/Flaps less than CONF 3 (CAT III with DH)...................................................................... B
Nosewheel Steering Failure (CAT III with DH)....................................................................................................... C
Antiskid Failure (CAT III with DH)...........................................................................................................................D
Alpha Floor Activation (CAT III with DH)................................................................................................................ E
One Engine Failure (CAT III with DH).....................................................................................................................F
Auto Callout RA Failure (CAT III with DH)............................................................................................................. G
Red "RA" Flag on two PFDs (CAT III with DH)......................................................................................................H
Amber "CHECK ATT" Flag on two PFDs (CAT III with DH).................................................................................... I
Red "ATT" Flag on one PFD (CAT III with DH)...................................................................................................... J
Amber "CHECK HDG" Flag on two PFDs and two NDs (CAT III with DH)............................................................ K
Red "HDG" Flag on one PFD and one ND (CAT III with DH).................................................................................L
Red "SPD" Flag on one PFD (CAT III with DH).................................................................................................... M
"AP OFF" Warning (CAT III with DH)..................................................................................................................... N
Capability Decrease (Except if due to A/THR Loss) (CAT III with DH).................................................................. O
Total Loss of A/THR ("CAT 3" Decreases to "CAT 2") (CAT III with DH)...............................................................P
LOC or G/S Excessive Deviation on PFD (CAT III with DH)................................................................................. Q
"AUTOLAND" Light (CAT III with DH).................................................................................................................... R
No "LAND" at 350 ft (CAT III with DH)...................................................................................................................S
Incorrect Selected Course at 350 ft > 5 deg (CAT III with DH).............................................................................. T
No "FLARE" at 30 ft (CAT III with DH)...................................................................................................................U
ABN-22-CATIIInoDH FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
Multiple Failures or Warnings (CAT III no DH)....................................................................................................... A
Failure Leading to Slats/Flaps less than CONF 3 (CAT III no DH)........................................................................ B
Nosewheel Steering Failure (CAT III no DH)..........................................................................................................C
Antiskid Failure (CAT III no DH)............................................................................................................................. D
Alpha Floor Activation (CAT III no DH)...................................................................................................................E
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 3/6
AFM 08 AUG 17
Continued from the previous page
One Engine Failure (CAT III no DH).......................................................................................................................F
Auto Callout RA Failure (CAT III no DH)............................................................................................................... G
Red "RA" Flag on two PFDs (CAT III no DH)........................................................................................................ H
Amber "CHECK ATT" Flag on two PFDs (CAT III no DH).......................................................................................I
Red "ATT" Flag on one PFD (CAT III no DH).........................................................................................................J
Amber "CHECK HDG" Flag on two PFDs and two NDs (CAT III no DH)...............................................................K
Red "HDG" Flag on one PFD and one ND (CAT III no DH)...................................................................................L
Red "SPD" Flag on one PFD (CAT III no DH).......................................................................................................M
"AP OFF" Warnings (CAT III no DH)......................................................................................................................N
Capability Decrease (Except if due to A/THR Loss) (CAT III no DH).................................................................... O
Total Loss of A/THR ("CAT 3" Decreases to "CAT 2") (CAT III no DH)................................................................. P
LOC or G/S Excessive Deviation on PFD (CAT III no DH)....................................................................................Q
"AUTOLAND" Light (CAT III no DH).......................................................................................................................R
No "LAND" at 350 ft (CAT III no DH)..................................................................................................................... S
Incorrect Selected Course at 350 ft > 5 deg (CAT III no DH).................................................................................T
No "FLARE" at 30 ft (CAT III no DH)..................................................................................................................... U
ABN-24 ELECTRICAL POWER
ELEC - AC ESS BUS FAULT.................................................................................................................................A
ELEC - AC BUS 1 FAULT...................................................................................................................................... B
ELEC - AC BUS 2 FAULT......................................................................................................................................C
ELEC - DC ESS BUS FAULT.................................................................................................................................D
ELEC - DC BUS 1 FAULT......................................................................................................................................E
ELEC - DC BUS 2 FAULT...................................................................................................................................... F
ELEC - DC EMER CONFIG................................................................................................................................... G
ELEC - DC BUS 1 + 2 FAULT............................................................................................................................... H
ELEC - DC ESS BUS SHED....................................................................................................................................I
ABN-27 FLIGHT CONTROLS
F/CTL - FLAPS FAULT........................................................................................................................................... A
F/CTL - FLAPS LOCKED........................................................................................................................................B
F/CTL - SLATS FAULT...........................................................................................................................................C
F/CTL - SLATS LOCKED........................................................................................................................................D
APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATION FACTOR..............................E
PERFORMANCE LIMITATION FOR LANDING IN CLEAN CONFIGURATION..................................................... F
F/CTL - SPLR FAULT.............................................................................................................................................G
F/CTL - GND SPLR FAULT....................................................................................................................................H
F/CTL - SPD BRK DISAGREE.................................................................................................................................I
F/CTL - SPD BRK FAULT....................................................................................................................................... J
F/CTL - RUDDER JAM........................................................................................................................................... K
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 4/6
AFM 08 AUG 17
Continued from the previous page
F/CTL - STOP RUDDER INPUT............................................................................................................................. L
F/CTL - L (R) ELEV FAULT................................................................................................................................... M
F/CTL - ELAC 1(2) FAULT..................................................................................................................................... N
F/CTL - SEC FAULT...............................................................................................................................................O
F/CTL - FCDC 1 + 2 FAULT...................................................................................................................................P
F/CTL - STABILIZER JAM......................................................................................................................................Q
F/CTL - ATLN LAW (PROT LOST).........................................................................................................................R
F/CTL - DIRECT LAW (PROT LOST).....................................................................................................................S
ABN-28 FUEL
FUEL - L(R) TK PUMP 1+2 LO PR........................................................................................................................A
FUEL - L(R) WING TK LO LVL.............................................................................................................................. B
FUEL - L+R WING TK LO LVL.............................................................................................................................. C
FUEL - CTR TK PUMPS LO PR............................................................................................................................ D
FUEL GRAVITY FEEDING......................................................................................................................................E
FUEL - L INNER (R INNER) (L OUTER) (R OUTER) TK HI TEMP.......................................................................F
FUEL IMBALANCE..................................................................................................................................................G
FUEL LEAK............................................................................................................................................................. H
ABN-29 HYDRAULIC
HYD - G SYS LO PR..............................................................................................................................................A
HYD - Y SYS LO PR.............................................................................................................................................. B
HYD - B SYS LO PR..............................................................................................................................................C
HYD - RSVR LO AIR PR........................................................................................................................................D
HYD - RSVR OVHT................................................................................................................................................ E
HYD - RSVR LO LVL..............................................................................................................................................F
ABN-30 ICE AND RAIN PROTECTION
ANTI ICE - CAPT (F/O) PROBES HEAT FAULT................................................................................................... A
DOUBLE AOA HEAT FAILURE.............................................................................................................................. B
WING A.ICE - SYS FAULT or OFF........................................................................................................................C
ANTI ICE - CAPT + F/O (CAPT + STBY) (F/O + STBY) PITOT HEAT FAULT..................................................... D
ANTI ICE - ALL PITOT HEAT FAULT.................................................................................................................... E
ABN-31 INDICATING/RECORDING SYSTEM
FWS - FWC 1 + 2 FAULT...................................................................................................................................... A
FWS - SDAC 1 + 2 FAULT.....................................................................................................................................B
DISPLAY UNIT FAILURE........................................................................................................................................C
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 5/6
AFM 08 AUG 17
Continued from the previous page
ABN-32 LANDING GEAR
L/G GRAVITY EXTENSION.................................................................................................................................... A
L/G - GEAR NOT UPLOCKED............................................................................................................................... B
L/G - GEAR UPLOCK FAULT................................................................................................................................ C
L/G - SHOCK ABSORBER FAULT.........................................................................................................................D
L/G - DOORS NOT CLOSED................................................................................................................................. E
BRAKES - A-SKID N-WS FAULT or OFF...............................................................................................................F
BRAKES - AUTO BRK FAULT...............................................................................................................................G
BRAKES - HOT.......................................................................................................................................................H
AUTOBRAKE.............................................................................................................................................................I
ABN-34 NAVIGATION
NAV - RA 1+2 FAULT.............................................................................................................................................A
NAV - IR 1+2 (1+3) (2+3) FAULT...........................................................................................................................B
NAV IR DISAGREE.................................................................................................................................................C
NAV - ADR 1+2 FAULT.......................................................................................................................................... D
NAV - ADR 1+3 FAULT.......................................................................................................................................... E
NAV - ADR 2+3 FAULT.......................................................................................................................................... F
ADR 1+2+3 FAULT.................................................................................................................................................G
NAV ADR DISAGREE.............................................................................................................................................H
UNRELIABLE AIRSPEED INDICATION...................................................................................................................I
UNRELIABLE AIRSPEED INDICATION.................................................................................................................. J
ABN-36 PNEUMATIC
AIR - ENG 1(2) BLEED HI TEMP...........................................................................................................................A
AIR - ENG 1(2) BLEED FAULT.............................................................................................................................. B
AIR - ENG 1(2) BLEED ABNORM PR................................................................................................................... C
AIR - X BLEED FAULT...........................................................................................................................................D
AIR - L (R) WING LEAK......................................................................................................................................... E
AIR - ENG 1(2) BLEED LEAK................................................................................................................................ F
AIR - ENG 1(2) BLEED LO TEMP......................................................................................................................... G
AIR - ENG 1 + 2 BLEED LO TEMP.......................................................................................................................H
ABN-52 DOORS
DOOR - DOOR NOT CLOSED...............................................................................................................................A
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET ABN-PLP-TOC P 6/6
AFM 08 AUG 17
Continued from the previous page
ABN-70 POWER PLANT
ENG - STALL...........................................................................................................................................................A
ENG COMPRESSOR VANE/ENG STALL on ground.............................................................................................B
ENG - FAIL..............................................................................................................................................................C
ENG - SHUTDOWN................................................................................................................................................ D
ENG - REV PRESSURIZED................................................................................................................................... E
ENG - REVERSE UNLOCKED............................................................................................................................... F
ENG - REVERSER FAULT.....................................................................................................................................G
ENG - THR LEVER FAULT.................................................................................................................................... H
ENG - THR LEVER DISAGREE...............................................................................................................................I
ENG - OIL HI TEMP................................................................................................................................................J
ENG - FADEC FAULT.............................................................................................................................................K
ENG - FADEC HI TEMP (FADEC OVHT)...............................................................................................................L
ENG - N1 (N2) (EGT) OVERLIMIT........................................................................................................................ M
ENG RELIGHT IN FLIGHT..................................................................................................................................... N
ABN-90 MISCELLANEOUS
BOMB ON BOARD..................................................................................................................................................A
OVERWEIGHT LANDING....................................................................................................................................... B
REJECTED TAKEOFF WITH ALL ENGINES OPERATIVE................................................................................... C
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
GENERAL
GLG A319-112 FLEET ABN-GEN P 1/2
AFM A to B → 08 AUG 17
INTRODUCTION
Ident.: ABN-GEN-00007087.0001001 / 14 JAN 15 APPROVED
Criteria: SA
The procedures contained in this chapter have been established and are recommended by the
aircraft manufacturer.
The following important remarks apply:
1. These procedures give information related to system and operational requirements and cover the
actions to be followed in case of failures which are not considered as emergency cases (these
cases are covered in EMERGENCY PROCEDURES chapter).
2. Only particular operations which are considered useful to highlight are presented. The procedures
which are considered to be "basic airmanship" are therefore not covered.
3. For a definition of LAND ASAP,Refer to GEN-DEF LAND ASAP Definition.
When actions depend on a condition, a dot (•) or a square (■) identifies this condition. The square is
used when there is a choice between one or more conditions and only one is applicable.
These procedures are approved by the Airworthiness Authorities as acceptable procedures for
operation of the aircraft. This approval does not prevent the operator from developing equivalent
procedures, provided these procedures are approved by appropriate Operational Authorities.
In case of discrepancy between procedures displayed on the ECAM and procedures stated in the
AFM, the AFM procedures have always precedence.
Unless otherwise specified in the procedures, the minimum speed to be used for approach and
landing is the VLS corresponding to the configuration requested by the procedure.
Note: VLS, when mentioned in a procedure, is the one corresponding to the configuration
requested by the procedure (e.g. if the procedure requests to use FLAPS 2, take VLS of
CONF 2).
LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE
Ident.: ABN-GEN-00015178.0001001 / 14 JUL 17 APPROVED
Criteria: SA
RUNWAY CONDITION DETERMINATION
The flight crew shall obtain the runway condition and/or the depth and type of runway contaminant
to make the basic assessment of actual condition. Estimated Surface Friction (Mu) or Pilot Reports
of Braking Action (PiRep) or similar qualitative information may be used in addition.
Landing distance determination must not consider a better Braking Action than the one related to
the runway condition.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
GENERAL
GLG A319-112 FLEET ABN-GEN P 2/2
AFM ← B 08 AUG 17
Runway Condition Max Reported Braking Action
Dry 6 - DRY
Wet 5 - GOOD
Compacted Snow 4 - GOOD to MEDIUM
More than 3 mm of Dry or Wet Snow 3 - MEDIUM
More than 3 mm of Standing Water or Slush 2 - MEDIUM to POOR
Ice (Cold and Dry) 1 - POOR
LANDING DISTANCE DETERMINATION
The landing distance to be applied in the case of failure is the Operational Landing Distance
(OLD).
The OLD can be determined by selecting the failure case in the IN-FLIGHT FAILURE field of
the AFM_OCTO interface, using the database given in the PERFORMANCE chapter of this
manual (Refer to PERF-OCTO Performance Database), combined with LSAE05.fail file using the
AFM_OCTO approved FM module at revision 32 or higher.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
TAKEOFF
GLG A319-112 FLEET ABN-OEI-TO P 1/4
AFM A 16 MAR 15
ENGINE FAILURE BEFORE V1 (REJECTED TAKEOFF)
Ident.: ABN-OEI-TO-00007100.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Immediately reduce all engine thrust levers to idle.
Monitor autobrake operation.
Take over control with brake pedals if necessary.
Note: 1. If autobrake is not used, maximum brakes must be applied simultaneously with
reduction of thrust levers.
2. If takeoff is rejected above 100 kt, it is recommended that maximum reverse thrust is
selected.
3. It is mandatory to use the maximum reverse thrust when the performance takes benefit
of the reverse thrust effect.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
TAKEOFF
GLG A319-112 FLEET ABN-OEI-TO P 2/4
AFM B 16 MAR 15
ENGINE FAILURE BETWEEN V1 AND V2
Ident.: ABN-OEI-TO-00007102.0001001 / 14 JAN 15 APPROVED
Criteria: SA
If the engine failure occurs before VR:
Use rudder conventionally to maintain runway centerline.
At VR:
Rotate the aircraft with a positive side stick input to achieve a normal and continuous rotation
rate to a pitch attitude of 12.5 °.
Once airborne and with positive rate of climb:
Retract landing gear.
Maintain airspeed not below V2.
SRS guidance should be followed when FD pitch order is established.
Use rudder to prevent yaw. Shortly after lift off, the β target will appear. Adjust rudder position
to zero the β target. Control heading conventionally with bank, keeping β target zeroed with the
rudder.
At acceleration height:
Level off.
If aircraft in configuration 2 or 3:
Accelerate up to F speed and select configuration 1.
Accelerate up to S speed and select configuration 0.
At slats zero, β target will disappear: center the sideslip indication conventionally.
Accelerate up to green dot speed and start climbing at this speed.
Reduce thrust to maximum continuous (If already in the MCT/FLX gate, move thrust lever to CL
and back to MCT).
Note: In the case of takeoff performed with reduced thrust (flexible takeoff), even if the one
engine out takeoff performance is always met with reduced thrust, selection of full takeoff
thrust may be done after engine failure.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
TAKEOFF
GLG A319-112 FLEET ABN-OEI-TO P 3/4
AFM C 16 MAR 15
ENGINE FAILURE DURING INITIAL CLIMB OUT
Ident.: ABN-OEI-TO-00007103.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Proceed as for takeoff with engine failure between V1 and V2 (Refer to ABN-OEI-TO ENGINE
FAILURE BETWEEN V1 AND V2). However, if failure occurs above V2, it is recommended to
maintain the speed reached after recovery, or SRS commanded attitude. In any case, the speed
must not be below V2.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
TAKEOFF
Intentionally left blank
GLG A319-112 FLEET ABN-OEI-TO P 4/4
AFM 16 MAR 15
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
APPROACH AND LANDING
GLG A319-112 FLEET ABN-OEI-LDG P 1/2
AFM A to B 14 DEC 13
APPROACH AND LANDING
Ident.: ABN-OEI-LDG-00007104.0002001 / 02 DEC 13 APPROVED
Criteria: (A319 or A321)
Set ENG MODE selector to IGN START.
Select the standard configuration (CONF3 and CONF FULL) for approach and landing.
Minimum final approach and landing speed: 1.23 VS1G of the landing configuration.
Note: 1. On the ECAM F/CTL page, check that the rudder trim compensates the aircraft in the
correct direction.
2. If the engine is inoperative before starting the approach, the minimum DH to perform
automatic approach, automatic landing and automatic roll out must be at least 50 ft.
MISSED APPROACH (FROM INTERMEDIATE APPROACH CONFIGURATION)
Ident.: ABN-OEI-LDG-00007105.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Apply go-around thrust.
Rotate the aircraft to a pitch attitude of 12.5 ° or as directed by SRS pitch command bar.
Maintain intermediate approach speed.
Use rudder to prevent yaw. Adjust rudder position to zero the β target. Control heading
conventionally with bank, keeping β target zeroed with the rudder.
At acceleration height:
Level off.
If aircraft in configuration 2 or 3:
Accelerate up to F speed and select configuration 1.
Accelerate up to S speed and select configuration 0.
At slats zero, β target will disappear: center the sideslip indication conventionally.
Accelerate up to green dot speed and start climbing at this speed.
Reduce thrust to maximum continuous.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
APPROACH AND LANDING
GLG A319-112 FLEET ABN-OEI-LDG P 2/2
AFM C 14 DEC 13
BALKED LANDING
Ident.: ABN-OEI-LDG-00007106.0001001 / 23 NOV 09 APPROVED
Criteria: (A319 or A320 or A321)
Apply go-around thrust.
Rotate the aircraft to a pitch of 12.5 ° or as directed by the SRS pitch command bar.
Retract slats/flaps one step.
Maintain final approach and landing speed.
When positive rate of climb established:
Retract landing gear.
If necessary, maintain a speed above the required speed to comply with approach climb
gradient. Refer to PERF-LDG Approach Climb and Landing Climb.
Use rudder to prevent yaw. Adjust rudder position to zero the β target. Control heading
conventionally with bank, keeping β target zeroed with the rudder.
At acceleration height:
Level off.
If aircraft in configuration 2 or 3:
Accelerate up to F speed and select configuration 1.
Accelerate up to S speed and select configuration 0.
At slats zero, β target will disappear: center the sideslip indication conventionally.
Accelerate up to green dot speed and start climbing at this speed.
Reduce thrust to maximum continuous.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AIR COND/PRESS/VENT
GLG A319-112 FLEET ABN-21 P 1/2
AFM A to C 05 DEC 11
AIR - PACK 1 + 2 FAULT
Ident.: ABN-21-00007161.0001001 / 04 APR 11 APPROVED
Criteria: SA
Turn off both packs.
Descend to the higher one of: FL 100 or MEA.
Note: If only one pack was overheated, recover the affected pack once overheat has
disappeared.
When at or below FL 100 or MEA and cabin differential pressure below 1 PSI:
Turn on RAM AIR.
CAB PR - SYS 1 + 2 FAULT
Ident.: ABN-21-00006672.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Use manual pressurization mode.
Monitor cabin altitude and differential pressure are within limits.
During final approach, maintain the cabin vertical speed switch in the UP position.
Check cabin differential pressure at zero before opening doors.
CAB PR - SAFETY VALVE OPEN
Ident.: ABN-21-00007162.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 35220)
If cabin differential pressure below 0 PSI:
Expect HI CAB rate.
Reduce aircraft vertical speed.
If cabin differential pressure above 8 PSI:
Use manual pressurization mode.
Monitor cabin altitude and differential pressure are within limits.
If unsuccessful:
Reduce aircraft altitude.
During final approach, maintain the cabin vertical speed switch in the UP position.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AIR COND/PRESS/VENT
GLG A319-112 FLEET ABN-21 P 2/2
AFM D to E 05 DEC 11
COND - HOT AIR FAULT
Ident.: ABN-21-00007164.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off hot air (if not automatically done).
If unsuccessful:
Turn off both packs. Refer to ABN-21 AIR - PACK 1 + 2 FAULT.
VENT - SKIN VALVE FAULT
Ident.: ABN-21-00007165.0001001 / 04 APR 11 APPROVED
Criteria: SA
Set ventilation blower to OVRD.
Set ventilation extract to OVRD.
If unsuccessful:
Maximum flight level is the higher one of: FL 100 or MEA.
Use manual pressurization mode.
Maintain the cabin vertical speed switch in the UP position.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
AUTO FLIGHT SYSTEM
GLG A319-112 FLEET ABN-22-AUTOFLT P 1/2
AFM A to D 13 JUN 17
AUTO FLT - FCU 1(2) FAULT
Ident.: ABN-22-AUTOFLT-00009309.0001001 / 23 NOV 09 APPROVED
Criteria: SA
At each baro setting change on FCU, crosscheck the validity of both PFD altitude information with
the standby altimeter.
AUTO FLT - RUD TRV LIM SYS
Ident.: ABN-22-AUTOFLT-00006936.0005001 / 03 AUG 10 APPROVED
Criteria: ((A318 or A319) and 37871)
Use rudder with care above 140 kt.
Turn off then on both FACs one after the other.
Use differential braking if necessary as soon as main gears are on ground.
Maximum crosswind for landing: 15 kt.
Do not use autobrake.
AUTO FLT - FAC 1+2 FAULT
Ident.: ABN-22-AUTOFLT-00009311.0002001 / 15 MAY 17 APPROVED
Criteria: ((318-121 or 318-122) or ((318-111 or 318-112 or A319) and (36847 or 37871)))
Use rudder with care above 140 kt.
Turn off then on both FACs one after the other.
If unsuccessful:
Turn off both FACs.
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT
LOST).
For go-around, set thrust levers to TOGA.
AUTO FLT - YAW DAMPER SYS
Ident.: ABN-22-AUTOFLT-00009310.0001001 / 03 AUG 10 APPROVED
Criteria: SA
Turn off then on both FACs one after the other.
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
AUTO FLIGHT SYSTEM
Intentionally left blank
GLG A319-112 FLEET ABN-22-AUTOFLT P 2/2
AFM 13 JUN 17
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 1/10
AFM A to D 25 JAN 11
MULTIPLE FAILURES OR WARNINGS (CAT II)
Ident.: ABN-22-CATII-00009313.0001001 / 23 NOV 09 APPROVED
Criteria: SA
In case of multiple failures or warnings, the most limiting applies.
ALTITUDE LOSS WITH AUTOPILOT MALFUNCTION (CAT II)
Ident.: ABN-22-CATII-00009795.0001001 / 23 NOV 09 APPROVED
Criteria: SA
DEMONSTRATED ALTITUDE LOSS BELOW GLIDE SLOPE WITH AUTOPILOT MALFUNCTION
In approach one AP engaged in APPR mode, with take over 1 s after failure recognition, the path
deviation is negligible.
FAILURE LEADING TO SLATS/FLAPS LESS THAN FLAPS 3 (CAT II)
Ident.: ABN-22-CATII-00009315.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Revert to CAT I minima.
Disengage the autopilot no later than 500 ft.
ANTISKID SYSTEM AND/OR NOSEWHEEL STEERING FAILURE (CAT II)
Ident.: ABN-22-CATII-00009338.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Disconnect the autopilot at touchdown or when the failure occurs during landing roll.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 2/10
AFM E to F 25 JAN 11
ALPHA FLOOR ACTIVATION (CAT II)
Ident.: ABN-22-CATII-00009342.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If activation occurs above 1 000 ft:
Check the speed.
Disconnect and reengage the autothrust mode (TOGA LK should disappear from the FMA).
If activation occurs below 1 000 ft:
Go around if visual references are not sufficient.
Note: Alpha floor protection is inhibited below 100 ft at landing.
ONE ENGINE FAILURE (CAT II)
Ident.: ABN-22-CATII-00009343.0002001 / 23 NOV 09 APPROVED
Criteria: (A319 or A321)
Note: Automatic approach, landing and rollout have been demonstrated with one engine
inoperative before initiating the approach.
If failure occurs above 1 000 ft:
Apply the standard One Engine Inoperative procedure.Refer to ABN-OEI-LDG APPROACH
AND LANDING.
If failure occurs between 1 000 ft and DH:
Go around if visual references are not sufficient.
If failure occurs below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 3/10
AFM G to H 25 JAN 11
RED "RA" FLAG ON TWO PFDS (CAT II)
Ident.: ABN-22-CATII-00009344.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears above 1 000 ft:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
Note: AP/FD not available in APPR mode.
AMBER "CHECK ATT" FLAG ON TWO PFDS (CAT II)
Ident.: ABN-22-CATII-00009349.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check aircraft attitude with the standby horizon.
Use switching to recover valid data.
If alert disappears:
A CAT II approach is still possible.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and DH:
Go around if visual references are not sufficient using standby horizon.
If alert appears below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 4/10
AFM I to J 25 JAN 11
RED "ATT" FLAG ON ONE PFD (CAT II)
Ident.: ABN-22-CATII-00009350.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT II approach is still possible.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
DIAGONAL LINE OR "INVALID DATA" ON ONE PFD AND ONE ND (CAT II)
Ident.: ABN-22-CATII-00009351.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Use switching to recover valid data.
If alert disappears:
A CAT II approach is still possible.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If alert appears below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 5/10
AFM K 25 JAN 11
AMBER "CHECK HDG" FLAG ON TWO PFDS AND ON TWO NDS (CAT II)
Ident.: ABN-22-CATII-00009352.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check heading with standby compass.
Use switching to recover valid data.
If alert disappears:
A CAT II approach is still possible.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If alert appears below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 6/10
AFM L to M 25 JAN 11
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT II)
Ident.: ABN-22-CATII-00009353.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT II approach is still possible.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
RED "SPD" FLAG ON ONE PFD (CAT II)
Ident.: ABN-22-CATII-00009354.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT II approach is still possible.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 7/10
AFM N to O 25 JAN 11
"AP OFF" WARNING (CAT II)
Ident.: ABN-22-CATII-00009355.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears above 1 000 ft:
Try to recover.
If no recovery:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
LOSS OF "CAT 2" CAPABILITY (CAT II)
Ident.: ABN-22-CATII-00009314.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If CAT 2 not displayed on FMA above 1 000 ft:
Try to recover.
If no recovery:
Revert to CAT I minima.
If CAT 2 disappears on FMA between 1 000 ft and DH:
Go around if visual references are not sufficient.
If CAT 2 disappears on FMA below DH:
Land if visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 8/10
AFM P to R 25 JAN 11
LOC OR G/S EXCESSIVE DEVIATION ON PFD (CAT II)
Ident.: ABN-22-CATII-00009356.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 200 ft:
Monitor ILS/MLS tracking.
If alert appears between 200 ft and DH:
Go around if visual references are not sufficient.
If alert appears below DH:
Land if external references are sufficient.
"AUTOLAND" LIGHT (CAT II)
Ident.: ABN-22-CATII-00009357.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears between 200 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual reference are sufficient.
A/THR FAULT (CAT II)
Ident.: ABN-22-CATII-00009358.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 1 000 ft:
Change over the autopilot and try to reengage the autothrust.
If unsuccessful:
Control the thrust manually.
If alert appears between 1 000 ft and DH:
Control the thrust manually.
If alert appears below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
GLG A319-112 FLEET ABN-22-CATII P 9/10
AFM S to U 25 JAN 11
NO "LAND" AT 350 FT (CAT II)
Ident.: ABN-22-CATII-00009359.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Go around or perform a manual landing if visual references are sufficient.
INCORRECT SELECTED COURSE AT 350 FT > 5 DEG (CAT II)
Ident.: ABN-22-CATII-00009360.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Continue the landing and disconnect autopilot at 50 ft at the latest.
NO "FLARE" AT 30 FT (CAT II)
Ident.: ABN-22-CATII-00009361.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Disconnect the autopilot.
Land manually.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
Intentionally left blank
GLG A319-112 FLEET ABN-22-CATII P 10/10
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 1/12
AFM A to C 25 JAN 11
MULTIPLES FAILURES OR WARNINGS (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009366.0001001 / 23 NOV 09 APPROVED
Criteria: SA
In case of multiple failures or warnings, the most limiting applies.
FAILURE LEADING TO SLATS/FLAPS LESS THAN CONF 3 (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009383.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Revert to CAT I minima.
Disconnect the autopilot no later than 500 ft.
NOSEWHEEL STEERING FAILURE (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009382.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 350 ft:
Revert to CAT III with DH 50 ft.
At touchdown, disconnect the autopilot.
If failure occurs between 350 ft and 100 ft:
Go around if visual references are not sufficient.
At touchdown, disconnect the autopilot.
If failure occurs below 100 ft:
Continue the landing.
At touchdown, disconnect the autopilot.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
If failure appears during landing roll:
Disconnect autopilot.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 2/12
AFM D to E 25 JAN 11
ANTISKID FAILURE (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009381.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 350 ft:
Revert to CAT III SINGLE minima.
At touchdown, disconnect the autopilot.
If failure occurs between 350 ft and 100 ft:
Go around if visual references are not sufficient.
At touchdown, disconnect the autopilot.
If failure occurs below 100 ft:
Continue the landing.
At touchdown, disconnect the autopilot.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
If failure appears at landing roll:
Disconnect autopilot.
ALPHA FLOOR ACTIVATION (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009380.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If activation occurs above 1 000 ft:
Check speed.
Disconnect and reengage the autothrust mode (TOGA LK should disappear from the FMA).
If activation occurs below 1 000 ft:
Go around if visual references are not sufficient.
Note: At landing, alpha floor protection is inhibited below 100 ft.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 3/12
AFM F to G 25 JAN 11
ONE ENGINE FAILURE (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009379.0002001 / 23 NOV 09 APPROVED
Criteria: (A319 or A321)
Note: Automatic approach, landing and rollout have been demonstrated with one engine
inoperative before initiating the approach.
If failure occurs above 1 000 ft:
Apply the standard One Engine Inoperative procedure. Refer to ABN-OEI-LDG APPROACH
AND LANDING.
Revert to CAT III SINGLE minima.
If failure occurs between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If failure occurs below 100 ft:
Continue the landing.
AUTO CALLOUT RA FAILURE (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009378.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If failure occurs below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 4/12
AFM H 25 JAN 11
RED "RA" FLAG ON TWO PFDS (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009377.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears above 1 000 ft:
Revert to CAT I minima.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
Note: AP/FD is not available in APPR mode.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 5/12
AFM I 25 JAN 11
AMBER "CHECK ATT" FLAG ON TWO PFDS (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009386.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check aircraft attitude with the standby horizon.
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III Dual is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient using standby horizon.
If alert appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate using standby horizon.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 6/12
AFM J 25 JAN 11
RED "ATT" FLAG ON ONE PFD (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009385.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT III SINGLE is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If warning appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 7/12
AFM K 25 JAN 11
AMBER "CHECK HDG" FLAG ON TWO PFDS AND TWO NDS (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009376.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check heading with standby compass.
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If alert appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 8/12
AFM L 25 JAN 11
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009375.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If alert appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 9/12
AFM M 25 JAN 11
RED "SPD" FLAG ON ONE PFD (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009374.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If alert appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 10/12
AFM N to O 25 JAN 11
"AP OFF" WARNING (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009373.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears above 1 000 ft:
Try to reengage autopilot.
If unsuccessful:
Revert to the available capability.
If warning appears between 1 000 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
CAPABILITY DECREASE (EXCEPT IF DUE TO A/THR LOSS) (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009372.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 1 000 ft:
Try to recover.
If unsuccessful:
Revert to the available capability.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 11/12
AFM P to Q 25 JAN 11
TOTAL LOSS OF A/THR ("CAT 3" DECREASES TO "CAT 2") (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009384.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 1 000 ft:
Disconnect AP1 (or change over if only one autopilot is engaged) and try to reengage the
autothrust.
If successful:
Continue to CAT III SINGLE minima.
If not successful:
Continue to CAT II minima.
Control the thrust manually.
If alert appears between 1 000 ft and 100 ft:
Continue to CAT II minima.
Control the thrust manually.
If alert appears below 100 ft:
Continue the landing.
Note: A go-around must be performed if visual references are not sufficient at 50 ft for a
CAT III SINGLE or at CAT II DH as appropriate.
Control the thrust manually.
LOC OR G/S EXCESSIVE DEVIATION ON PFD (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009371.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 200 ft:
Monitor ILS/MLS tracking.
If failure occurs between 200 ft and DH:
Go around if visual references are not sufficient.
If failure occurs below DH:
Land if external visual references are sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
GLG A319-112 FLEET ABN-22-CATIIIDH P 12/12
AFM R to U 25 JAN 11
"AUTOLAND" LIGHT (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009370.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning appears between 200 ft and DH:
Go around if visual references are not sufficient.
If warning appears below DH:
Land if external visual references are sufficient.
NO "LAND" AT 350 FT (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009369.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Go around or perform a manual landing if visual references are sufficient.
INCORRECT SELECTED COURSE AT 350 FT > 5 DEG (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009368.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Revert to CAT II minima.
Disconnect autopilot at 50 ft at the latest.
NO "FLARE" AT 30 FT (CAT III WITH DH)
Ident.: ABN-22-CATIIIDH-00009367.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If visual references are not sufficient:
Go around.
If visual references are sufficient:
Disconnect autopilot.
Land manually.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 1/12
AFM A to C 14 DEC 13
MULTIPLE FAILURES OR WARNINGS (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009393.0001001 / 23 NOV 09 APPROVED
Criteria: SA
In case of multiple failures or warnings, the most limiting applies.
FAILURE LEADING TO SLATS/FLAPS LESS THAN CONF 3 (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009394.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Revert to CAT I minima.
Disconnect autopilot no later than 500 ft.
NOSEWHEEL STEERING FAILURE (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009395.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 350 ft:
Revert to CAT III with DH 50 ft.
At touchdown, disconnect the autopilot.
If failure occurs between 350 ft and 100 ft:
Go around if visual references are not sufficient.
At touchdown, disconnect the autopilot.
If failure occurs below 100 ft:
Continue the landing.
At touchdown, disconnect the autopilot.
If failure occurs during the landing roll:
Disconnect autopilot.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 2/12
AFM D to E 14 DEC 13
ANTISKID FAILURE (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009396.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 350 ft:
Revert to CAT III SINGLE minima.
At touchdown, disconnect autopilot.
If failure occurs between 350 ft and 100 ft:
Go around if visual references are not sufficient.
At touchdown, disconnect autopilot.
If failure occurs below 100 ft:
Continue the landing.
At touchdown, disconnect autopilot.
If failure occurs during the landing roll:
Disconnect autopilot.
ALPHA FLOOR ACTIVATION (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009397.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If activation occurs above 1 000 ft:
Check the speed.
Disconnect and reengage the autothrust mode (TOGA LK should disappear from the FMA).
If activation occurs below 1 000 ft:
Go around if visual references are not sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 3/12
AFM F to H 14 DEC 13
ONE ENGINE FAILURE (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009413.0002001 / 23 NOV 09 APPROVED
Criteria: (A319 or A321)
If failure occurs above 1 000 ft:
Apply the standard One Engine Inoperative procedure.Refer to ABN-OEI-LDG APPROACH
AND LANDING.
Revert to CAT III SINGLE minima.
If failure occurs between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If failure occurs below 100 ft:
Continue the landing.
AUTO CALLOUT RA FAILURE (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009398.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If failure occurs below 100 ft:
Continue the landing.
RED "RA" FLAG ON TWO PFDS (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009399.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If warning occurs above 1 000 ft:
Revert to CAT I minima.
If warning appears below 1 000 ft:
Go around if visual references are not sufficient.
Note: AP/FD is not available in APPR mode.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 4/12
AFM I 14 DEC 13
AMBER "CHECK ATT" FLAG ON TWO PFDS (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009400.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check aircraft attitude with the standby horizon.
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient using standby horizon.
If alert appears below 100 ft:
Continue the landing.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 5/12
AFM J 14 DEC 13
RED "ATT" FLAG ON ONE PFD (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009401.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If warning appears below 100 ft:
Continue the landing.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 6/12
AFM K 14 DEC 13
AMBER "CHECK HDG" FLAG ON TWO PFDS AND TWO NDS (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009402.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If alert appears above 1 000 ft:
Check heading with standby compass.
Use switching to recover valid data.
If alert disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If alert persists:
Revert to CAT I minima.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If alert appears below 100 ft:
Continue the landing.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 7/12
AFM L 14 DEC 13
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009403.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If warning appears below 100 ft:
Continue the landing.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 8/12
AFM M to N 14 DEC 13
RED "SPD" FLAG ON ONE PFD (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009404.0001001 / 23 NOV 09 APPROVED
Criteria: SA
CAUTION Do not make any switching below 1 000 ft.
If warning appears above 1 000 ft:
Use switching to recover valid data.
If warning disappears:
A CAT III SINGLE approach is still possible.
Note: In case of diagonal line or "INVALID DATA" on one PFD and one ND due to DMC
failure, a CAT III DUAL is still possible after DMC switching. If warning does not
disappear, revert to CAT I.
If warning persists:
Revert to CAT I minima.
If warning appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
If warning appears below 100 ft:
Continue the landing .
"AP OFF" WARNINGS (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009405.0001001 / 02 DEC 13 APPROVED
Criteria: SA
If warning appears above 1 000 ft:
Try to reengage the autopilot.
If unsuccessful:
Revert to the available capability.
If warning appears below 1 000 ft:
Go around if visual references are not sufficient.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 9/12
AFM O to P 14 DEC 13
CAPABILITY DECREASE (EXCEPT IF DUE TO A/THR LOSS) (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009406.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 1 000 ft:
Try to reengage the autopilot.
If unsuccessful:
Revert to the available capability.
If alert appears between 1 000 ft and 100 ft:
Go around if visual references are not sufficient.
TOTAL LOSS OF A/THR ("CAT 3" DECREASES TO "CAT 2") (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009407.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert appears above 1 000 ft:
Disconnect the AP1 and try to reengage the autothrust.
If successful:
Continue to CAT III SINGLE minima.
If not successful:
Continue to CAT II minima.
Control the thrust manually.
If alert appears between 1 000 ft and 100 ft:
Continue to CAT II minima.
Control the thrust manually.
If alert appears below 100 ft:
Continue the landing.
Control the thrust manually.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 10/12
AFM Q to T 14 DEC 13
LOC OR G/S EXCESSIVE DEVIATION ON PFD (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009408.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If failure occurs above 200 ft:
Monitor ILS/MLS tracking.
If failure occurs below 200 ft:
Go around if visual references are not sufficient.
"AUTOLAND" LIGHT (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009409.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If alert occurs below 200 ft:
Go around if visual references are not sufficient.
NO "LAND" AT 350 FT (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009410.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Go around or perform a manual landing if visual references are sufficient.
INCORRECT SELECTED COURSE AT 350 FT > 5 DEG (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009411.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Revert to CAT II minima.
Disconnect autopilot at 50 ft at the latest.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
GLG A319-112 FLEET ABN-22-CATIIInoDH P 11/12
AFM U 14 DEC 13
NO "FLARE" AT 30 FT (CAT III NO DH)
Ident.: ABN-22-CATIIInoDH-00009412.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If visual references are not sufficient:
Go around.
If visual references are sufficient:
Disconnect autopilot.
Land manually.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
Intentionally left blank
GLG A319-112 FLEET ABN-22-CATIIInoDH P 12/12
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ELECTRICAL POWER
GLG A319-112 FLEET ABN-24 P 1/4
AFM A to C 10 SEP 14
ELEC - AC ESS BUS FAULT
Ident.: ABN-24-00007139.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 37871)
Set AC ESS FEED to ALTN.
Set ATC/XPDR to SYS 2.
ELEC - AC BUS 1 FAULT
Ident.: ABN-24-00007140.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Set ventilation blower to OVRD.
Note: 1. Blue hydraulic system is inoperative. Refer to ABN-29 HYD - B SYS LO PR.
2. Spoilers are partially inoperative.
ELEC - AC BUS 2 FAULT
Ident.: ABN-24-00007141.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Set ventilation extract to OVRD.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ELECTRICAL POWER
GLG A319-112 FLEET ABN-24 P 2/4
AFM D to E 10 SEP 14
ELEC - DC ESS BUS FAULT
Ident.: ABN-24-00007143.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Note: 1. Wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
2. For communication, only VHF 2 or VHF 3 are available.
Select audio switching.
Check baro reference on FCU.
Turn off GPWS.
For approach and landing:
Note: Slats and flaps extend slowly.
If no ice accretion:
Apply necessary landing performance corrections.
If ice accretion:
Approach speed = VLS + 10 kt
Apply necessary landing performance corrections.
Note: 1. Blue hydraulic system is inoperative.Refer to ABN-29 HYD - B SYS LO PR.
2. Spoilers are partially inoperative. Refer to ABN-27 F/CTL - SPLR FAULT.
ELEC - DC BUS 1 FAULT
Ident.: ABN-24-00007148.0002001 / 02 DEC 13 APPROVED
Criteria: (SA and 151269)
Set ventilation blower to OVRD.
Set ventilation extract to OVRD.
Avoid icing conditions.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ELECTRICAL POWER
GLG A319-112 FLEET ABN-24 P 3/4
AFM F to H 10 SEP 14
ELEC - DC BUS 2 FAULT
Ident.: ABN-24-00007150.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Set AIR DATA switching to F/O 3.
Check baro reference on FCU.
Note: 1. The Cockpit Door Locking System (CDLS) is inoperative (if installed).
2. Slats and flaps extend slowly.
3. Half spoilers are inoperative.
4. SEC 2+3 are inoperative. Refer to ABN-27 F/CTL - SEC FAULT.
ELEC - DC EMER CONFIG
Ident.: ABN-24-00007152.0001001 / 02 DEC 13 APPROVED
Criteria: SA
LAND ASAP
Manually confirm emergency electrical power on.
Minimum speed: 140 kt
Apply necessary landing performance corrections.
ELEC - DC BUS 1 + 2 FAULT
Ident.: ABN-24-00007154.0002001 / 02 DEC 13 APPROVED
Criteria: (((A320 or A321) and 21678) or A319)
Note: The Cockpit Door Locking System (CDLS) is inoperative (if installed).
Set ventilation blower to OVRD.
Set ventilation extract to OVRD.
Check baro reference on FCU.
For approach and landing:
Note: Slats and flaps extend slowly.
Apply necessary landing performance corrections.
Note: 1. Antiskid is inoperative. Refer to ABN-32 BRAKES - A-SKID N-WS FAULT or OFF.
2. Half spoilers are inoperative.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ELECTRICAL POWER
GLG A319-112 FLEET ABN-24 P 4/4
AFM I 10 SEP 14
ELEC - DC ESS BUS SHED
Ident.: ABN-24-00007159.0002001 / 02 DEC 13 APPROVED
Criteria: (SA and 151269)
Set ventilation extract to OVRD.
Avoid icing conditions.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 1/10
AFM A to B 08 AUG 17
F/CTL - FLAPS FAULT
Ident.: ABN-27-00007108.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Speed is limited to the VFE corresponding to the next more extended flaps configuration.
Refer to LIM-SPD VFE.
When speed below VFE:
Recycle flaps lever.
If unsuccessful:
Apply flaps locked procedure. Refer to ABN-27 F/CTL - FLAPS LOCKED.
F/CTL - FLAPS LOCKED
Ident.: ABN-27-00006637.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Speed is limited to the VFE corresponding to the next more extended flaps configuration.
Refer to LIM-SPD VFE.
If flaps position below 3:
Use FLAPS 3 for landing.
Turn off GPWS flap mode.
If flaps position at 3:
Use FLAPS 3 for landing.
Turn on GPWS LDG FLAP 3.
If flaps position above 3:
Use FLAPS FULL for landing.
Turn on GPWS LDG FLAP 3.
Apply necessary approach speed and landing performance corrections. Refer to ABN-27
APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATION FACTOR.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 2/10
AFM C to D 08 AUG 17
F/CTL - SLATS FAULT
Ident.: ABN-27-00007109.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Speed is limited to the VFE corresponding to the next more extended slats configuration.
Refer to LIM-SPD VFE.
When speed below VFE :
Recycle flaps lever.
If unsuccessful :
Apply slats locked procedure. Refer to ABN-27 F/CTL - SLATS LOCKED.
F/CTL - SLATS LOCKED
Ident.: ABN-27-00006638.0002001 / 23 NOV 09 APPROVED
Criteria: ((A318 or A319 or A320) and 20024)
Speed is limited to the VFE corresponding to the next more extended slats configuration.
Refer to LIM-SPD VFE.
If slats not at 0:
Set FUEL MODE SEL to MAN.
Set center tank pumps as required.
For landing:
Use FLAPS 3.
Turn off center tank pumps.
Turn on GPWS LDG FLAP 3.
Apply necessary approach speed and landing performance corrections. Refer to ABN-27
APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATION FACTOR.
Note: If SLATS FAULT by double SFCC failure, flight controls are in alternate law. Refer to
ABN-27 F/CTL - ALTN LAW (PROT LOST).
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 3/10
AFM E 08 AUG 17
APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATION FACTOR
Ident.: ABN-27-00006879.0005001 / 02 DEC 13 APPROVED
Criteria: A319
APPROACH SPEED INCREMENT
LANDING DISTANCE MULTIPLICATION FACTOR
Flaps at or above
0 and below 1+F
Flaps at or above
1+F and below 2
Flaps at or above
2 and below 3 Flaps at 3 Flaps above 3
Slats at or
above 0
and below 1
(1)VREF + 45 kt VREF + 30 kt VREF + 25 kt VREF + 25 kt not allowed
Slats at or
above 1 and
at or below 3
VREF + 25 kt VREF + 15 kt VREF + 10 kt VREF + 10 kt VREF + 10 kt
Slats above 3 VREF + 25 kt VREF + 15 kt VREF + 10 kt VREF + 5 kt VREF + 5 kt
(1) If flaps and slats are jammed at position 0, the approach speed increment is VREF + 60 kt, then at
500 ft, reduce speed to obtain VREF + 50 kt at threshold.
For the landing distance apply necessary landing performance corrections.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 4/10
AFM F → 08 AUG 17
PERFORMANCE LIMITATION FOR LANDING IN CLEAN CONFIGURATION
Ident.: ABN-27-00007110.0003001 / 03 AUG 10 APPROVED
Criteria: A319
The following graph gives information on compatibility between weight, maximum tire speed and
maximum brake energy for landing in clean configuration.
Maximum tire speed: Refer to LIM-32 Tire Speed.
Landing in Clean Configuration
Wind effect on determined weight:
‐ Headwind: add 0.2 t (440 lb) per kt of headwind
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 5/10
AFM ← F to J 08 AUG 17
Continued from the previous page PERFORMANCE LIMITATION FOR LANDING IN CLEAN CONFIGURATION
‐ Tailwind: substract 1.5 t (3 307 lb) per kt of tailwind.
F/CTL - SPLR FAULT
Ident.: ABN-27-00006639.0001001 / 02 DEC 13 APPROVED
Criteria: SA
If spoilers 3+4 affected:
Do not use speed brakes.
For landing:
Apply necessary landing performance corrections.
F/CTL - GND SPLR FAULT
Ident.: ABN-27-00007114.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Refer to ABN-27 F/CTL - SPLR FAULT.
F/CTL - SPD BRK DISAGREE
Ident.: ABN-27-00007117.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Retract speed brakes.
Refer to ABN-27 F/CTL - SPLR FAULT.
F/CTL - SPD BRK FAULT
Ident.: ABN-27-00007118.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Refer to ABN-27 F/CTL - SPLR FAULT.
Note: Associated ground spoilers are only available through thrust reversers selection.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 6/10
AFM K to M 08 AUG 17
F/CTL - RUDDER JAM
Ident.: ABN-27-00007119.0001001 / 02 DEC 13 APPROVED
Criteria: SA
For approach and landing:
Avoid crosswind from the side where the rudder is deflected.
Maximum crosswind: 15 kt
Apply necessary landing performance corrections.
Do not use autobrake.
Use differential braking if necessary as soon as main gears are on ground.
Do not use asymmetric reverse thrust.
Below 70 kt, consider using nosewheel steering handle.
F/CTL - STOP RUDDER INPUT
Ident.: ABN-27-00015241.0001001 / 02 DEC 13 APPROVED
Criteria: (SA and 154473)
CAUTION Avoid large and rapid rudder inputs.
When "STOP RUDDER INPUT" aural warning is triggered:
Release immediately the rudder pedals.
F/CTL - L (R) ELEV FAULT
Ident.: ABN-27-00007120.0004001 / 02 DEC 13 APPROVED
Criteria: (A318 or A319)
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Do not use speed brakes.
Maximum speed: 320 kt
Use FLAPS 3 for landing.
Set GPWS LDG FLAP 3 to ON.
Approach speed = VREF + 15 kt
Apply necessary landing performance corrections.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 7/10
AFM N to O 08 AUG 17
F/CTL - ELAC 1(2) FAULT
Ident.: ABN-27-00007121.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off then on affected ELAC.
Note: If both ELACs affected, turn off then on both ELACs one after the other.
If reset not successful:
Turn off affected ELAC.
Note: If both ELACs affected:
‐ Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT
LOST).
‐ Ailerons are inoperative.
F/CTL - SEC FAULT
Ident.: ABN-27-00006640.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Turn off then on affected SEC.
If reset not successful:
Turn off affected SEC.
If SEC 1 or SEC 1+2 or SEC 1+3 affected:
Do not use speed brakes.
Apply necessary landing performance corrections.
If SEC 2 or SEC 3 or SEC 2+3 affected:
Apply necessary landing performance corrections.
If all SECs are inoperative:
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT
LOST).
Do not use speed brakes.
Apply necessary landing performance corrections.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 8/10
AFM P to R 08 AUG 17
F/CTL - FCDC 1 + 2 FAULT
Ident.: ABN-27-00007131.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Monitor flight controls overhead panel.
Note: 1. Flight controls indications are not available on ECAM.
2. Control law status is not available on PFD.
F/CTL - STABILIZER JAM
Ident.: ABN-27-00007132.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
If manual pitch trim available:
Use manual pitch trim to maintain elevator at zero position (indication on ECAM F/CTL page).
F/CTL - ATLN LAW (PROT LOST)
Ident.: ABN-27-00006618.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
Maximum speed : 320 kt
For approach and landing:
Use FLAPS 3 for landing.
Set GPWS LDG FLAPS 3 to ON.
Approach speed = VREF + 10 kt
Apply necessary landing performance corrections.
Note: 1. When landing gear extended and autopilots off, controls revert to direct law.
2. If manual pitch trim not available, extend landing gear when in CONF 3 and at
approach speed in order to delay the reversion to direct law.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
GLG A319-112 FLEET ABN-27 P 9/10
AFM S 08 AUG 17
F/CTL - DIRECT LAW (PROT LOST)
Ident.: ABN-27-00006671.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
Maximum speed: 320 kt / M 0.77
If manual pitch trim available:
Use manual pitch trim.
Maneuver with care.
Use speed brakes with care.
For approach and landing:
Use FLAPS 3 for landing.
Set GPWS LDG FLAPS 3 to ON.
Approach speed = VREF + 10 kt
Apply necessary landing performance corrections.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FLIGHT CONTROLS
Intentionally left blank
GLG A319-112 FLEET ABN-27 P 10/10
AFM 08 AUG 17
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 1/6
AFM A to B 10 SEP 14
FUEL - L(R) TK PUMP 1+2 LO PR
Ident.: ABN-28-00007194.0002001 / 23 NOV 09 APPROVED
Criteria: ((A319 or A320) and 20024)
CAUTION Do not apply this procedure if a fuel leak is suspected. Refer to ABN-28 FUEL
LEAK.
If center tank not empty:
Manually perform a fuel transfer from the center tank.
When center tank empty:
If above FL 150:
Open crossfeed valve.
Set ENG MODE selector to IGN START.
Turn off affected side tank pumps.
When L(R) tank fuel required:
Apply fuel gravity feeding procedure. Refer to ABN-28 FUEL GRAVITY FEEDING.
FUEL - L(R) WING TK LO LVL
Ident.: ABN-28-00007198.0002001 / 23 NOV 09 APPROVED
Criteria: ((A319 or A320) and 20024)
CAUTION Do not apply this procedure if a fuel leak is suspected. Refer to ABN-28 FUEL
LEAK.
If center tank not empty:
Manually perform a fuel transfer from the center tank.
If fuel imbalance:
Open crossfeed valve.
Turn off affected side pumps.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 2/6
AFM C to D 10 SEP 14
FUEL - L+R WING TK LO LVL
Ident.: ABN-28-00007200.0004001 / 02 DEC 13 APPROVED
Criteria: (SA and 151269)
LAND ASAP
If center tank not empty:
Manually perform a fuel transfer from the center tank.
Turn on all wing tank pumps.
If no fuel leak:
Open crossfeed valve.
If gravity fuel feeding:
Close crossfeed valve.
FUEL - CTR TK PUMPS LO PR
Ident.: ABN-28-00009364.0003001 / 02 DEC 13 APPROVED
Criteria: ((A318 or A319 or A320) and 151269)
Turn off both center tank pumps.
Close crossfeed valve.
Note: 1. Center tank fuel is unusable.
2. Gravity feeding from center tank is not possible.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 3/6
AFM E 10 SEP 14
FUEL GRAVITY FEEDING
Ident.: ABN-28-00006624.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Descend to gravity feed ceiling (if applicable):
Flight conditions at the time of gravity feeding Gravity feed ceiling
Flight time above FL 300 greater
than 30 min (Fuel deaerated) Current FL (1)
Flight time above FL 300 lower
than 30 min (Fuel non-deaerated) FL 300 (1)
Aircraft flight level never exceeded
FL 300 (Fuel non-deaerated)
The highest of:
‐FL 150 (1)
‐ 7 000 ft above takeoff airport altitude
(1) In case JET B fuel is used, the gravity feed ceiling is FL 100 in all cases.
When reaching gravity feed ceiling:
Set ENG MODE selector to IGN START.
Avoid negative g load factor.
Close crossfeed valve.
If only one engine is running and is fed by gravity:
Open crossfeed valve.
Adjust bank angle 1 ° wing down on running engine side.
Use rudder trim to get constant course and neutral stick.
When fuel imbalance at or above 1 000 kg (2 204 lb):
Increase bank angle to 2 ° or 3 ° wing down on running engine side.
Note: Fuel from opposite wing is used until imbalance is reduced to 0.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 4/6
AFM F to G 10 SEP 14
FUEL - L INNER (R INNER) (L OUTER) (R OUTER) TK HI TEMP
Ident.: ABN-28-00007201.0001001 / 23 NOV 09 APPROVED
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or A318)
Turn off galleys.
On ground:
If fuel temperature above 60 °C in outer tank or 54 °C in inner tank:
Delay takeoff.
Set affected engine master lever to OFF.
In flight:
If fuel temperature above 60 °C in outer tank or 54 °C in inner tank:
Increase engine fuel flow on affected side.
If fuel temperature above 65 °C in outer tank or 57 °C in inner tank:
Start APU as required.
If opposite IDG not fault:
Turn off affected IDG.
FUEL IMBALANCE
Ident.: ABN-28-00007203.0002001 / 23 NOV 09 APPROVED
Criteria: ((319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or
A318) and 20024)
Compare the FOB + FU with the FOB at departure. If the difference is significant, or if the FOB + FU
decreases, suspect a fuel leak.
CAUTION Do not apply this procedure if a fuel leak is suspected. Refer to ABN-28 FUEL
LEAK.
Open wing crossfeed valve.
Turn off fuel pumps on the lighter side and on center tank.
When fuel balanced:
Turn on wing and center fuel pumps.
Close wing crossfeed valve.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 5/6
AFM H → 10 SEP 14
FUEL LEAK
Ident.: ABN-28-00006692.0003001 / 23 NOV 09 APPROVED
Criteria: ((320-111 or 320-211 or 320-212 or 320-214 or 320-231 or 320-232 or 320-233 or A318 or A319) and 20024)
A fuel leak may be detected if:
‐ The sum of the FOB and the FU is significantly less than the FOB at engine start, or decreases,
or
‐ A passenger observes fuel spray from engine/pylon or wing tip, or
‐ The total fuel quantity decreases at an abnormal rate, or
‐ A fuel imbalance develops, or
‐ The fuel quantity of a tank decreases too fast (leak from engine/pylon or a hole in a tank), or
‐ Fuel flow is excessive (leak from engine), or
‐ Fuel is smelt in the cabin.
If visibility permits, a visual check from the cabin may enable identification of the leak source.
When a leak is confirmed:
LAND ASAP
If leak from engine/pylon confirmed:
Shut down affected engine.
Note: If the leak stops, the wing crossfeed valve can now be selected open to
re-balance the fuel quantity or to enable use of fuel from both wings. Do not
restart the engine.
If leak from engine/pylon not confirmed or leak not located:
Keep wing crossfeed valve closed.
CAUTION Do not open the wing crossfeed valve, even if requested by another ECAM
procedure.
Turn off both center tank pumps.
Monitor inner fuel tank quantities and look for one tank depleting faster.
If one inner tank depletes faster than the other by at least 300 kg (661 lb) in less
than 30 min:
Shut down affected engine.
Note: If the leak stops, the wing crossfeed valve can now be selected open to
re-balance the fuel quantity or to enable use of fuel from both wings. Do not
restart the engine.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
FUEL
GLG A319-112 FLEET ABN-28 P 6/6
AFM ← H 10 SEP 14
Continued from the previous page FUEL LEAK
Monitor fuel leak.
Turn on both center tank pumps.
Note: If the leak continues after engine shutdown, suspect leak from wing and
consider restarting the engine. The wing crossfeed valve can be selected
open.
If both inner tanks deplete at a similar rate:
Note: The wing crossfeed valve can be selected open.
If fuel smell in the cabin:
If APU running:
Shut down APU.
When inner wing tank fuel quantity below 3 t (6 614 lb):
Turn on both center tank pumps.
For landing:
CAUTION Do not use reverse.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
HYDRAULIC
GLG A319-112 FLEET ABN-29 P 1/4
AFM A to C 14 DEC 13
HYD - G SYS LO PR
Ident.: ABN-29-00006656.0005001 / 02 DEC 13 APPROVED
Criteria: SA
If hydraulic system not recovered:
For approach and landing:
Note: Slats and flaps extend slowly.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
Apply necessary landing performance corrections.
Note: Spoilers are partially inoperative.
HYD - Y SYS LO PR
Ident.: ABN-29-00006657.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
If hydraulic system not recovered:
For approach and landing:
Note: Flaps extend slowly.
Apply necessary landing performance corrections.
Note: Spoilers are partially inoperative.
HYD - B SYS LO PR
Ident.: ABN-29-00006658.0001001 / 02 DEC 13 APPROVED
Criteria: SA
If hydraulic system not recovered:
For approach and landing:
Note: Slats extend slowly.
Apply necessary landing performance corrections.
Note: Spoilers are partially inoperative.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
HYDRAULIC
GLG A319-112 FLEET ABN-29 P 2/4
AFM D to E 14 DEC 13
HYD - RSVR LO AIR PR
Ident.: ABN-29-00009203.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If pressure fluctuates:
Turn off associated hydraulic pumps.
If green hydraulic system affected:
Set PTU to OFF.
Apply green hydraulic system low pressure procedure. Refer to ABN-29 HYD - G SYS LO
PR.
If yellow hydraulic system affected:
Set PTU to OFF.
Apply yellow hydraulic system low pressure procedure. Refer to ABN-29 HYD - Y SYS LO
PR.
Note: System may be recovered at low altitude.
HYD - RSVR OVHT
Ident.: ABN-29-00009204.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off associated hydraulic pumps.
If green hydraulic system affected:
Set PTU to OFF.
Apply green hydraulic system low pressure procedure. Refer to ABN-29 HYD - G SYS LO PR.
If yellow hydraulic system affected:
Set PTU to OFF.
Apply yellow hydraulic system low pressure procedure. Refer to ABN-29 HYD - Y SYS LO PR.
Note: System may be recovered if OVHT indication has disappeared.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
HYDRAULIC
GLG A319-112 FLEET ABN-29 P 3/4
AFM F 14 DEC 13
HYD - RSVR LO LVL
Ident.: ABN-29-00009205.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off associated hydraulic pumps.
If green hydraulic system affected:
Set PTU to OFF.
Apply green hydraulic system low pressure procedure. Refer to ABN-29 HYD - G SYS LO PR.
If yellow hydraulic system affected:
Set PTU to OFF.
Apply yellow hydraulic system low pressure procedure. Refer to ABN-29 HYD - Y SYS LO PR.
Note: If blue system affected, EMER GEN is inoperative.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
HYDRAULIC
Intentionally left blank
GLG A319-112 FLEET ABN-29 P 4/4
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ICE AND RAIN PROTECTION
GLG A319-112 FLEET ABN-30 P 1/2
AFM A to C 16 MAR 15
ANTI ICE - CAPT (F/O) PROBES HEAT FAULT
Ident.: ABN-30-00007178.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If ADR 3 available:
Use AIR DATA switching as appropriate.
DOUBLE AOA HEAT FAILURE
Ident.: ABN-30-00007179.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 31283)
If icing conditions cannot be avoided:
Turn off one of affected ADRs.
WING A.ICE - SYS FAULT OR OFF
Ident.: ABN-30-00006619.0012001 / 14 JAN 15 APPROVED
Criteria: (SA and 37871)
Turn off wing anti-ice.
Avoid icing conditions.
If severe ice accretion:
Note: With anti-ice failed, the AOA protections are still efficient.
Minimum speed: VLS +10/G DOT.
For landing:
Apply necessary landing performance correction.
Maneuver with care.
Note: Avoid large roll inputs at high AOA and high thrust setting. In the case of abnormal
response in pitch or roll, release the backstick and reduce thrust.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
ICE AND RAIN PROTECTION
GLG A319-112 FLEET ABN-30 P 2/2
AFM D to E 16 MAR 15
ANTI ICE - CAPT + F/O (CAPT + STBY) (F/O + STBY) PITOT HEAT FAULT
Ident.: ABN-30-00009388.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 35220)
If non-related ADR on and operative:
Turn off one of affected ADRs.
If non-related ADR faulty or off:
If icing conditions expected:
Turn off one of affected ADRs.
Consider applying unreliable airspeed procedure. Refer to ABN-34 UNRELIABLE
AIRSPEED INDICATION.
ANTI ICE - ALL PITOT HEAT FAULT
Ident.: ABN-30-00009389.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 35220)
Turn off one of appropriate affected ADRs.
If icing conditions expected:
Turn off another one of appropriate affected ADRs.
Consider applying unreliable airspeed procedure. Refer to ABN-34 UNRELIABLE AIRSPEED
INDICATION.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
GLG A319-112 FLEET ABN-31 P 1/4
AFM A to B 14 DEC 13
FWS - FWC 1 + 2 FAULT
Ident.: ABN-31-00007209.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Monitor systems.
Monitor overhead panel.
Note: ECAM cautions and warnings are lost, but ECAM system pages are available. Regularly
call ECAM system pages for systems checks.
FWS - SDAC 1 + 2 FAULT
Ident.: ABN-31-00007210.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Monitor overhead panel.
Note: Only ECAM ENG, FUEL, F/CTL, WHEEL pages are available.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
GLG A319-112 FLEET ABN-31 P 2/4
AFM C → 14 DEC 13
DISPLAY UNIT FAILURE
Ident.: ABN-31-00007211.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Affected DU blank or display distorted:
Turn off affected DU as required.
If ECAM DUs affected:
Use ECAM/ND SEL.
If EFIS DUs affected:
Use PFD/ND XFR.
Diagonal line or "INVALID DATA" on affected DU:
Attempt to recover affected DU by using associated DMC switching.
If unsuccessful:
Turn off then on affected DU.
Inversion of EWD and SD displays:
Turn off then on ECAM upper display.
Affected DU(s) or MCDU flashes intermittently:
If Captain PFD or ND, both ECAM DUs or upper ECAM DU, or MCDU 1 is (are)
affected:
Turn off GEN 1.
If DU(s) stop(s) flashing:
Keep GEN 1 off for the rest of the flight.
Use the sideslip indication to verify if the rudder trim needs to be reset. If necessary,
reset the rudder trim.
Note: Intermittent Electrical Power Supply Interruptions may cause offset in the
rudder trim.
Select AP and/or autothrust as required.
APU may be started (Refer to NORM-49 Auxiliary Power Unit (APU)) and APU
generator may be used (if available).
If DU(s) do(es) not stop flashing:
Restore GEN 1.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
GLG A319-112 FLEET ABN-31 P 3/4
AFM ← C 14 DEC 13
Continued from the previous page DISPLAY UNIT FAILURE
If First Officer PFD or ND, lower ECAM DU, or MCDU 2 is (are) affected:
Turn off GEN 2.
If DU(s) stop(s) flashing:
Keep GEN 2 off for the rest of the flight.
Use the sideslip indication to verify if the rudder trim needs to be reset. If necessary,
reset the rudder trim.
Note: Intermittent Electrical Power Supply Interruptions may cause offset in the
rudder trim.
Select AP and/or autothrust as required.
APU may be started (Refer to NORM-49 Auxiliary Power Unit (APU)) and APU
generator may be used (if available).
If DU(s) do(es) not stop flashing:
Restore GEN 2.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
Intentionally left blank
GLG A319-112 FLEET ABN-31 P 4/4
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
LANDING GEAR
GLG A319-112 FLEET ABN-32 P 1/4
AFM A to C 10 SEP 14
L/G GRAVITY EXTENSION
Ident.: ABN-32-00006663.0001001 / 23 NOV 09 APPROVED
Criteria: (A319 or A320 or A321)
Pull and turn the gravity extension handle and pull down landing gear lever.
Confirm landing gear locked down.
Note: Nosewheel steering is inoperative.
L/G - GEAR NOT UPLOCKED
Ident.: ABN-32-00007168.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If landing gear not downlocked:
Maximum speed: VLO (Retraction)
Recycle landing gear.
If unsuccessful:
Pull down landing gear lever.
If landing gear downlocked:
Maximum speed: VLE
If landing gear doors closed and landing gear not uplocked:
Avoid excessive g load factor.
L/G - GEAR UPLOCK FAULT
Ident.: ABN-32-00007169.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Maximum speed: VLE
Keep landing gear down.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
LANDING GEAR
GLG A319-112 FLEET ABN-32 P 2/4
AFM D to G 10 SEP 14
L/G - SHOCK ABSORBER FAULT
Ident.: ABN-32-00007170.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 37871)
If landing gear not uplocked:
Maximum speed: VLE.
Keep landing gear down.
L/G - DOORS NOT CLOSED
Ident.: ABN-32-00007171.0001001 / 23 NOV 09 APPROVED
Criteria: SA
When speed below VLO (Retraction):
Recycle landing gear.
If unsuccessful:
Maximum speed: VLO (Extension)
BRAKES - A-SKID N-WS FAULT OR OFF
Ident.: ABN-32-00006623.0005001 / 02 DEC 13 APPROVED
Criteria: SA
Apply maximum brake pressure 1 000 PSI.
Note: Nosewheel steering is inoperative.
Apply necessary landing performance corrections.
BRAKES - AUTO BRK FAULT
Ident.: ABN-32-00007175.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
Apply necessary landing performance corrections.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
LANDING GEAR
GLG A319-112 FLEET ABN-32 P 3/4
AFM H to I 10 SEP 14
BRAKES - HOT
Ident.: ABN-32-00007176.0004001 / 02 DEC 13 APPROVED
Criteria: (SA and 153741)
On ground:
Turn on brake fans (if installed).
Note: For parking, prefer chocks.
Delay takeoff for cooling.
In flight after takeoff:
If performance permits:
Maximum speed: VLE/VLO
Keep landing gear down for cooling.
AUTOBRAKE
Ident.: ABN-32-00007177.0001001 / 23 NOV 09 APPROVED
Criteria: SA
In the case of malfunction, take over brake control with brake pedals. If green DECEL light
(corresponding to the selected mode) fails to illuminate, disarm autobrake and proceed as
circumstances dictate.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
LANDING GEAR
Intentionally left blank
GLG A319-112 FLEET ABN-32 P 4/4
AFM 10 SEP 14
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 1/6
AFM A to C 11 JUL 17
NAV - RA 1+2 FAULT
Ident.: ABN-34-00007212.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: At landing gear extension, flight controls are in direct law. Refer to ABN-27 F/CTL -
DIRECT LAW (PROT LOST).
NAV - IR 1+2 (1+3) (2+3) FAULT
Ident.: ABN-34-00007213.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Use ATT HDG switching as appropriate.
NAV IR DISAGREE
Ident.: ABN-34-00007214.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Flight controls are in direct law.
Use standby horizon to determine the faulty IR.
If disagree confirmed:
Turn off faulty IR.
Turn off then on ELAC 2.
Turn off then on ELAC 1.
Note: Flight controls revert to alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT
LOST).
If disagree not confirmed:
Flight controls remain in direct law. Refer to ABN-27 F/CTL - DIRECT LAW (PROT LOST).
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 2/6
AFM D to F 11 JUL 17
NAV - ADR 1+2 FAULT
Ident.: ABN-34-00007186.0001001 / 15 MAY 17 APPROVED
Criteria: SA
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Set AIR DATA switching to CAPT 3.
Turn off ADR 1 and ADR 2.
For go-around, set thrust levers to TOGA.
NAV - ADR 1+3 FAULT
Ident.: ABN-34-00007187.0002001 / 15 MAY 17 APPROVED
Criteria: (SA and 37871)
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Set AIR DATA switching to NORM.
Set ATC/XPDR to SYS 2.
Turn off ADR 1 and ADR 3.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
For go-around, set thrust levers to TOGA.
NAV - ADR 2+3 FAULT
Ident.: ABN-34-00009566.0002001 / 15 MAY 17 APPROVED
Criteria: (SA and 37871)
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Set AIR DATA switching to NORM.
Set ATC/XPDR to SYS 1.
Turn off ADR 2 and ADR 3.
For go-around, set thrust levers to TOGA.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 3/6
AFM G to H 11 JUL 17
ADR 1+2+3 FAULT
Ident.: ABN-34-00006691.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Turn off all ADRs.
Use standby instruments.
Note: 1. Automatic cabin pressurization system is inoperative. Refer to ABN-21 CAB PR - SYS 1
+ 2 FAULT.
2. Rudder travel limiter is inoperative. Refer to ABN-22-AUTOFLT AUTO FLT - RUD TRV
LIM SYS.
Extend landing gear by gravity. Refer to ABN-32 L/G GRAVITY EXTENSION.
NAV ADR DISAGREE
Ident.: ABN-34-00007192.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Flight controls are in alternate law. Refer to ABN-27 F/CTL - ALTN LAW (PROT LOST).
Use both PFDs and standby airspeed indicator to determine the faulty ADR.
Turn off faulty ADR.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 4/6
AFM I → 11 JUL 17
UNRELIABLE AIRSPEED INDICATION
Ident.: TDU / ABN-34-00009811.0003001 / 11 FEB 16 APPROVED
Criteria: (A318 or 319-100 or 320-200 or 321-100 or 321-200)
Impacted DU: 00006690 UNRELIABLE AIRSPEED INDICATION
Belongs to TR562 Issue 1
Note: Unreliable airspeed indication may be due to radome damage, or due to air probe failure
or obstruction. If the failure is due to radome destruction, the drag will be increased and
therefore N1 must be increased by 5 %.
If the safe conduct of the flight is impacted:
Disconnect autopilot.
Turn off flight directors.
Disconnect autothrust.
If below thrust reduction altitude:
Apply TOGA thrust.
Target a pitch attitude of 15 °.
If above thrust reduction altitude:
Apply CLB thrust.
When below FL 100:
Target a pitch attitude of 10 °.
When above FL 100:
Target a pitch attitude of 5 °.
If in CONF 0 or 1 or 2 or 3:
Maintain the slats/flaps in their current configuration.
If in CONF FULL:
Select CONF3 and maintain.
Check that speed brakes are retracted.
When airborne:
Retract landing gear.
Note: Respect stall warning.
When flight path stabilized:
Turn on probe and window heat.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 5/6
AFM ← I 11 JUL 17
Continued from the previous page UNRELIABLE AIRSPEED INDICATION
Adjust pitch attitude and thrust regarding flight phase and aircraft configuration to obtain and
maintain target speed.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET ABN-34 P 6/6
AFM J 11 JUL 17
UNRELIABLE AIRSPEED INDICATION
Ident.: ABN-34-00006690.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Impacted by TDU: 00009811 UNRELIABLE AIRSPEED INDICATION
Note: Unreliable airspeed indication may be due to radome damage, or due to air probe failure
or obstruction. If the failure is due to radome destruction, the drag will be increased and
therefore N1 must be increased by 5 %.
If the safe conduct of the flight is impacted:
Disconnect autopilot.
Turn off flight directors.
Disconnect autothrust.
If below thrust reduction altitude:
Apply TOGA thrust.
Target a pitch attitude of 15 °.
If above thrust reduction altitude:
Apply CLB thrust.
When below FL 100:
Target a pitch attitude of 10 °.
When above FL 100:
Target a pitch attitude of 5 °.
Maintain slats/flaps in their current configuration.
Check that speed brakes are retracted.
When airborne:
Retract landing gear.
Note: Respect stall warning.
When flight path stabilized:
Turn on probe and window heat.
Adjust pitch attitude and thrust regarding flight phase and aircraft configuration to obtain and
maintain target speed.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PNEUMATIC
GLG A319-112 FLEET ABN-36 P 1/4
AFM A to C 10 SEP 14
AIR - ENG 1(2) BLEED HI TEMP
Ident.: ABN-36-00015197.0001001 / 02 DEC 13 APPROVED
Criteria: (SA and 151269)
If wing anti-ice off:
Turn off affected side pack.
If wing anti-ice on:
‐ Turn off affected side pack, or
‐ Turn off wing anti-ice.
Note: If wing anti-ice is shut off, Refer to ABN-30 WING A.ICE - SYS FAULT or OFF
AIR - ENG 1(2) BLEED FAULT
Ident.: ABN-36-00007180.0004001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320) and 151269)
Turn off affected side engine bleed (if not automatically done).
If wing anti-ice off:
Set PACK FLOW to LO.
If wing anti-ice on:
Turn off affected side pack.
Open crossbleed valve.
AIR - ENG 1(2) BLEED ABNORM PR
Ident.: ABN-36-00007181.0004001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320) and 151269)
If wing anti-ice off:
Set PACK FLOW to LO.
If wing anti-ice on:
Turn off affected side pack.
Open crossbleed valve.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PNEUMATIC
GLG A319-112 FLEET ABN-36 P 2/4
AFM D to F 10 SEP 14
AIR - X BLEED FAULT
Ident.: ABN-36-00007184.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Use crossbleed valve manual control.
Note: If crossbleed valve failed closed and one bleed inoperative, wing anti-ice is inoperative.
Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
AIR - L (R) WING LEAK
Ident.: ABN-36-00007188.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off affected side engine bleed (if not automatically done).
If left wing leak:
Turn off APU bleed (if not automatically done).
Close crossbleed valve (if not automatically done).
Note: Wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
AIR - ENG 1(2) BLEED LEAK
Ident.: ABN-36-00007190.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Turn off affected side engine bleed (if not automatically done).
If engine 1 pylon leak:
Turn off APU bleed (if not automatically done).
Close crossbleed valve (if not automatically done).
Note: Wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PNEUMATIC
GLG A319-112 FLEET ABN-36 P 3/4
AFM G to H 10 SEP 14
AIR - ENG 1(2) BLEED LO TEMP
Ident.: ABN-36-00009345.0001001 / 23 NOV 09 APPROVED
Criteria: (A321 or ((A318 or A319 or A320) and 21566))
Disconnect autothrust.
Increase affected engine thrust.
If unsuccessful:
If opposite bleed available:
Open crossbleed valve.
Turn off affected side engine bleed.
Turn off affected side pack (if the other pack is on).
AIR - ENG 1 + 2 BLEED LO TEMP
Ident.: ABN-36-00009346.0001001 / 23 NOV 09 APPROVED
Criteria: (A321 or ((A318 or A319 or A320) and 21566))
Disconnect autothrust.
Increase engines thrust.
Note: If unsuccessful, wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT
or OFF.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
PNEUMATIC
Intentionally left blank
GLG A319-112 FLEET ABN-36 P 4/4
AFM 10 SEP 14
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
DOORS
GLG A319-112 FLEET ABN-52 P 1/2
AFM A 08 APR 11
DOOR - DOOR NOT CLOSED
Ident.: ABN-52-00010780.0001001 / 04 APR 11 APPROVED
Criteria: SA
If abnormal cabin vertical speed:
Maximum flight level is the higher one of: FL 100 or MEA.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
DOORS
Intentionally left blank
GLG A319-112 FLEET ABN-52 P 2/2
AFM 08 APR 11
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 1/8
AFM A to B 22 SEP 15
ENG - STALL
Ident.: TDU / ABN-70-00016178.0001001 / 03 SEP 15 APPROVED
Criteria: SA
Impacted DU: NONE
Belongs to TR500 Issue 1
Set affected engine thrust lever to IDLE.
Check engine parameters of the affected engine.
If abnormal engine parameters:
Shut down the affected engine.
If normal engine parameters:
Turn on engine anti-ice of the affected side.
Increase thrust slowly on the affected engine.
If a stall recurs:
Reduce thrust on the affected engine.
If a stall does not recur:
Continue engine operation.
ENG COMPRESSOR VANE/ENG STALL ON GROUND
Ident.: TDU / ABN-70-00009732.0001001 / 21 OCT 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
Impacted DU: NONE
Belongs to TR34 Issue 1
ON GROUND:
If the ECAM displays any of the following caution:
‐ ENG 1(2) COMPRESSOR VANE
‐ ENG 1(2) START FAULT
‐ ENG 1(2) STALL.
Before flight:
Report the ECAM caution in the logbook and contact immediately the maintenance in
order to check if the departure is allowed.
After landing:
Report the ECAM caution in the logbook even if the ECAM caution has disappeared.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 2/8
AFM C to E 22 SEP 15
ENG - FAIL
Ident.: ABN-70-00006885.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If no damage:
Attempt an immediate engine relight setting ENG MODE selector to IGN START and engine
thrust lever to idle.
If no engine relight after 30 s:
Shut down affected engine.
Consider engine relight. Refer to ABN-70 ENG RELIGHT IN FLIGHT.
If engine damage:
Push relevant FIRE pb and discharge AGENT 1 after 10 s.
ENG - SHUTDOWN
Ident.: ABN-70-00007091.0001001 / 23 NOV 09 APPROVED
Criteria: SA
LAND ASAP
If relevant FIRE pb not pushed:
If wing anti-ice on:
Turn off affected side pack.
Open crossbleed valve.
Set ENG MODE selector to IGN START.
If no fuel leak:
Monitor fuel imbalance.
If relevant FIRE pb pushed:
Close crossbleed valve.
Note: Wing anti-ice is inoperative. Refer to ABN-30 WING A.ICE - SYS FAULT or OFF.
ENG - REV PRESSURIZED
Ident.: ABN-70-00007092.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Set affected engine thrust lever to idle.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 3/8
AFM F to G 22 SEP 15
ENG - REVERSE UNLOCKED
Ident.: ABN-70-00007093.0002001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320 or A321) and 30660)
If FADEC sets affected engine to idle:
LAND ASAP
Set affected engine thrust lever to idle.
Maximum speed: 300 kt/M 0.78
If buffet:
Reduce speed to 240 kt.
Shut down affected engine.
If reversers actually deployed:
Apply full rudder trim towards live engine.
Control heading with roll.
For approach and landing:
Use FLAPS 1 for landing.
Turn off GPWS flap mode.
Approach speed = VREF + 55 kt.
Set 5 ° rudder trim towards live engine.
Disconnect autothrust.
Minimize drag until on glide slope.
At 800 ft AGL:
Target speed = VREF + 40 kt.
Apply necessary landing performance corrections.
ENG - REVERSER FAULT
Ident.: ABN-70-00009156.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 30660)
If FADEC sets affected engine to idle:
LAND ASAP
Set affected engine thrust lever to idle.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 4/8
AFM H to K 22 SEP 15
ENG - THR LEVER FAULT
Ident.: ABN-70-00009157.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 30660)
LAND ASAP
Engage autothrust (if not already engaged).
ENG - THR LEVER DISAGREE
Ident.: ABN-70-00009158.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 30660)
LAND ASAP
Engage autothrust (if not already engaged).
ENG - OIL HI TEMP
Ident.: ABN-70-00007095.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Shut down affected engine.
ENG - FADEC FAULT
Ident.: ABN-70-00007096.0004001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213) and (36847 or 37871))
On ground, do not set affected engine thrust lever above idle.
In flight, set affected engine thrust lever to idle.
Confirm engine status using other ECAM system pages (ELEC, HYD, BLEED).
If abnormal engine operation:
Shut down affected engine.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 5/8
AFM L to M 22 SEP 15
ENG - FADEC HI TEMP (FADEC OVHT)
Ident.: ABN-70-00007097.0002001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213) and (36847 or 37871))
On ground:
Shut down affected engine.
Set ENG MODE selector to NORM.
Check FADEC ground power off.
In flight:
Note: Reducing engine power should decrease temperature.
Confirm engine status using other ECAM system pages (ELEC, HYD, BLEED).
If abnormal engine operation:
Shut down affected engine.
ENG - N1 (N2) (EGT) OVERLIMIT
Ident.: ABN-70-00007098.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Move affected engine thrust lever to reduce N1 (N2) (EGT) below limit.
If overlimit persists after throttle back to idle position:
Shut down the affected engine.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 6/8
AFM N → 22 SEP 15
ENG RELIGHT IN FLIGHT
Ident.: ABN-70-00006620.0009001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
Maximum flight level: FL 275
Set affected engine master lever to OFF.
Set affected engine thrust lever to idle.
Set ENG MODE selector to IGN START.
Open crossbleed valve if necessary.
Set engine master lever to ON.
Note: Engine light up must be achieved within 30 s after fuel flow increases.
When idle reached:
Set ENG MODE selector to NORM.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
GLG A319-112 FLEET ABN-70 P 7/8
AFM ← N 22 SEP 15
Continued from the previous page ENG RELIGHT IN FLIGHT
In Flight Engine Relight Envelope
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
POWER PLANT
Intentionally left blank
GLG A319-112 FLEET ABN-70 P 8/8
AFM 22 SEP 15
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET ABN-90 P 1/4
AFM A → 08 APR 11
BOMB ON BOARD
Ident.: ABN-90-00007024.0002001 / 04 APR 11 APPROVED
Criteria: ((A319 or A320 or A321) and 31276)
FLIGHT CREW PROCEDURES
Establish communication between cockpit and cabin.
If landing and evacuation possible within 30 min:
Notify ATC / Company.
Land and initiate evacuation.
If not possible:
Level off.
Manually control the cabin pressure in order not to increase the cabin altitude.
Notify ATC / Company.
Descend the aircraft in order to reach aircraft altitude equal to the higher one of: cabin
altitude + 2 500 ft or MEA.
Avoid sharp maneuvers.
Maximum cabin differential pressure: 1 PSI.
When aircraft altitude equal to cabin altitude + 2 500 ft or MEA:
Maintain cabin differential pressure at 1 PSI.
Turn off galleys.
When bomb is secured at the LRBL or if bomb cannot be moved:
Turn on emergency exit light.
Turn off COMMERCIAL.
If fuel permits:
Use at least FLAPS 1.
Extend landing gear.
For approach and landing:
Set cabin altitude mode to AUTO.
Reduce the differential pressure to zero.
If evacuation required:
Initiate evacuation.
If evacuation not required:
Notify cabin crew and passengers.
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET ABN-90 P 2/4
AFM ← A to B 08 APR 11
Continued from the previous page BOMB ON BOARD
CABIN CREW PROCEDURES
If landing and evacuation not possible within 30 min:
If the bomb can be moved, move it to the prepared Least Risk Bomb Location (centre of the
right hand aft cabin door).
OVERWEIGHT LANDING
Ident.: ABN-90-00007107.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If circumstances dictate, landing may be made at a weight corresponding to the maximum structural
takeoff weight.
If the overweight landing procedure follows a failure requesting to land in FLAPS 3 or
below:
Use the requested FLAPS setting for landing.
For go-around:
Select FLAPS 1.
Otherwise:
If approach climb performance requirement is met in CONF 3:
Use FLAPS FULL for landing.
For go-around:
Select FLAPS 3.
If approach climb performance requirement is not met in CONF 3:
Use FLAPS 3 for landing.
For go-around:
Select FLAPS 1.
Note: 1. At this weight the maximum touchdown vertical speed should not exceed 360 ft/min.
2. Air conditioning should be turned off or supplied by APU.
3. Approach climb requirement must be checked.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
MISCELLANEOUS
GLG A319-112 FLEET ABN-90 P 3/4
AFM C 08 APR 11
REJECTED TAKEOFF WITH ALL ENGINES OPERATIVE
Ident.: ABN-90-00007183.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Immediately reduce all thrust levers to idle.
Monitor autobrake operation.
Take over brake control with brake pedals if necessary.
Note: If autobrake is not used, maximum brakes must be applied simultaneously with reduction
of thrust levers.
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
MISCELLANEOUS
Intentionally left blank
GLG A319-112 FLEET ABN-90 P 4/4
AFM 08 APR 11
NORMAL PROCEDURES
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET NORM-PLP-TOC P 1/2
AFM 10 OCT 17
NORM-GEN GENERAL
Introduction...............................................................................................................................................................A
NORM-PFLT PREFLIGHT CHECKS
Electrical...................................................................................................................................................................A
Cockpit Door............................................................................................................................................................ B
Braking Efficiency Test............................................................................................................................................C
NORM-TO TAKEOFF
Takeoff Procedure................................................................................................................................................... A
NORM-FLT FLIGHT
Buffet Onset.............................................................................................................................................................A
Flight in Severe Turbulence.................................................................................................................................... B
NORM-LDG APPROACH AND LANDING
Normal Landing........................................................................................................................................................A
Balked Landing (All Engines Operating)................................................................................................................. B
Reverse Thrust........................................................................................................................................................ C
Autobrake.................................................................................................................................................................D
NORM-22 AUTO FLIGHT SYSTEM
NORM-22-CONF Demonstrated System Configuration
AP/FD, Speed modes, Autothrust........................................................................................................................... A
Takeoff..................................................................................................................................................................... B
Climb, Cruise, Descent............................................................................................................................................C
Non Precision Approach..........................................................................................................................................D
CAT I ILS Approach................................................................................................................................................ E
CAT II ILS Approach............................................................................................................................................... F
CAT II/III ILS Approach and Automatic Approach.................................................................................................. G
Go-around................................................................................................................................................................H
Altitude Loss after Automatic Go-around Initiation................................................................................................... I
NORM-22-NPA Non Precision Approach
General.....................................................................................................................................................................A
Instrument Approach Using NAV Mode.................................................................................................................. B
NORM-22-PA Precision Approach
CAT II and CAT III Approach and/or Automatic Landing........................................................................................A
Required Equipment for CAT II and CAT III Approach and Landing...................................................................... B
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET NORM-PLP-TOC P 2/2
AFM 10 OCT 17
Continued from the previous page
NORM-28 FUEL
Fuel System.............................................................................................................................................................A
NORM-30 ICE AND RAIN PROTECTION
Operations in Icing Conditions................................................................................................................................ A
Rain Repellent (If Activated)....................................................................................................................................B
NORM-34 NAVIGATION
Ground Proximity Warning System (GPWS)...........................................................................................................A
Inertial Reference System (IRS)..............................................................................................................................B
Reduced Vertical Separation Minimum (RVSM)..................................................................................................... C
Windshear Warning and Guidance System............................................................................................................ D
NORM-49 AUXILIARY POWER UNIT
Auxiliary Power Unit (APU)..................................................................................................................................... A
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
GENERAL
GLG A319-112 FLEET NORM-GEN P 1/2
AFM A 16 MAR 15
INTRODUCTION
Ident.: NORM-GEN-00009222.0001001 / 14 JAN 15 APPROVED
Criteria: SA
The procedures contained in this chapter have been established and are recommended by the
aircraft manufacturer.
Only particular operations which are considered useful to highlight are presented. The procedures
which are considered to be "basic airmanship" are therefore not covered.
When actions depend on a condition, a dot (•) or a square (■) identifies this condition. The square is
used when there is a choice between one or more conditions and only one is applicable.
These procedures are approved by the Airworthiness Authorities as acceptable procedures for
a convenient use of the aircraft. This approval does not prevent the operator from developing
equivalent procedures provided these procedures are approved by appropriate operational
authorities.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
GENERAL
Intentionally left blank
GLG A319-112 FLEET NORM-GEN P 2/2
AFM 16 MAR 15
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
PREFLIGHT CHECKS
GLG A319-112 FLEET NORM-PFLT P 1/2
AFM A to C 10 OCT 17
ELECTRICAL
Ident.: NORM-PFLT-00007056.0002001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A321)
Batteries conditions must be checked before the first flight of the day.
BAT 1+2 charge current must be reducing to a value below 60 A after BAT 1+2 OFF then ON.
COCKPIT DOOR
Ident.: NORM-PFLT-00007057.0001001 / 23 NOV 09 APPROVED
Criteria: SA
If required by local Airworthiness Authorities:
Check that the cockpit door is closed and locked before each flight.
BRAKING EFFICIENCY TEST
Ident.: NORM-PFLT-00007058.0001001 / 23 NOV 09 APPROVED
Criteria: SA
When starting to taxi or after any BSCU reset on ground:
As soon as the aircraft starts to move, check the efficiency of the braking system by pressing
brake pedals.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
PREFLIGHT CHECKS
Intentionally left blank
GLG A319-112 FLEET NORM-PFLT P 2/2
AFM 10 OCT 17
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
TAKEOFF
GLG A319-112 FLEET NORM-TO P 1/2
AFM A → 16 MAR 15
TAKEOFF PROCEDURE
Ident.: NORM-TO-00007059.0001001 / 14 JAN 15 APPROVED
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or
321-111 or 321-112 or 321-211 or 321-212 or 321-213 or A318)
Set slats, flaps and horizontal stabilizer as required.
Perform flight controls checks using the pedals and each sidestick.
Arm ground spoilers and select maximum autobrake.
Set ENG MODE selector as required.
Apply 50 % N1 on both engines with brakes on.
Note: Brakes may be released so as to perform a rolling takeoff.
If crosswind at or below 20 kt and no tailwind:
Release brakes with stick half forward.
Apply thrust up to the FLX/TOGA thrust whilst maintaining stick half forward up to 80 kt.
If crosswind above 20 kt or tailwind:
Release brakes with stick full forward.
Apply thrust rapidly to 70 % N1, then progressively to get FLX/TOGA thrust at 40 kt ground
speed, whilst maintaining stick close to full forward up to 80 kt.
Then release stick progressively to reach neutral at 100 kt.
Note: Once throttle is set to FLX MCT gate, any change to FLEX TEMP setting will not be taken
into account by FADEC for N1 TARGET computation.
Check takeoff N1 is set prior to reach 80 kt.
At VR:
Rotate the aircraft with a positive sidestick input to achieve a normal and continuous rotation rate
to the pitch attitude necessary to maintain an airspeed at or above V2 + 10 kt.
Once airborne and with a positive rate of climb:
Retract landing gear.
SRS guidance should be followed when FD pitch order is established.
At safe height:
Accelerate up to at least 1.18 VS1G of configuration (1+F) or ″F″ speed if CONF 2 or 3 in use.
Select slats/flaps position 1 and accelerate up to at least 1.23 VS1G of clean configuration ("S"
speed).
Select slats/flaps position 0 and accelerate up to 1.36 VS1G ("green dot" speed).
Disarm ground spoilers.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
TAKEOFF
GLG A319-112 FLEET NORM-TO P 2/2
AFM ← A 16 MAR 15
Note: 1. For takeoff in configuration 1 (1+F), F speed is not displayed.
2. If the takeoff is performed with packs off, pack 1 should be selected ON after thrust
reduction to CLB.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FLIGHT
GLG A319-112 FLEET NORM-FLT P 1/4
AFM A → 07 MAR 17
BUFFET ONSET
Ident.: NORM-FLT-00007063.0003001 / 03 AUG 10 APPROVED
Criteria: A319
At any flight conditions, it is possible to determine maneuvering margins before buffet onset occurs,
by reference to the following graphs.
Example 1 (Weight in kg):
• For:
‐ M = 0.72
‐ Flight Level = 310
‐ Weight = 70 t
‐ CG = 35 %
• Results: Buffet onset at
‐ M = 0.72 with 55 ° bank angle or at 1.75 g
‐ Low Speed (1 g): M = 0.54
Example 2 (Weight in lb):
• For:
‐ M = 0.72
‐ Flight Level = 310
‐ Weight = 140 000 lb
‐ CG = 35 %
• Results: Buffet onset at
‐ M = 0.72 with 59 ° bank angle or at 1.9 g
‐ Low Speed (1 g): M = 0.51
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FLIGHT
GLG A319-112 FLEET NORM-FLT P 2/4
AFM ← A → 07 MAR 17
BUFFET ONSET (Weight in kg)
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FLIGHT
GLG A319-112 FLEET NORM-FLT P 3/4
AFM ← A to B → 07 MAR 17
BUFFET ONSET (Weight in lb)
FLIGHT IN SEVERE TURBULENCE
Ident.: NORM-FLT-00007066.0007001 / 14 FEB 17 APPROVED
Criteria: A319
Turn on seat belts signs.
Disconnect autothrust.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FLIGHT
GLG A319-112 FLEET NORM-FLT P 4/4
AFM ← B 07 MAR 17
Respect the following recommended speed:
Recommended Speed in Severe Turbulence
The recommended speed is:
‐ Below FL 200: 250 kt IAS
‐ At or above FL 200: 275 kt IAS/M 0.76
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
APPROACH AND LANDING
GLG A319-112 FLEET NORM-LDG P 1/2
AFM A to D → 25 JAN 11
NORMAL LANDING
Ident.: NORM-LDG-00007067.0001001 / 23 NOV 09 APPROVED
Criteria: (A319 or A320 or A321)
The minimum final approach speed is 1.23 VS1G of the landing configuration.
Set ENG MODE selector as required.
Note: The flare height should be increased for landing at high altitude airports particularly with
high approach speeds or for approaches with increased glide slope or to uphill sloping
runways.
BALKED LANDING (ALL ENGINES OPERATING)
Ident.: NORM-LDG-00007068.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Apply go-around thrust.
Rotate to achieve a positive rate of climb and establish the required pitch attitude (not to exceed 18 °)
as directed by SRS pitch command bar.
Retract slats/flaps one step.
Maintain the final approach speed.
When a positive rate of climb established:
Retract landing gear.
REVERSE THRUST
Ident.: NORM-LDG-00007069.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Note: Reverse thrust may be applied before the nosewheel is on ground (even with one engine
inoperative).
Maximum reverse thrust may be applied down to 70 kt IAS.
AUTOBRAKE
Ident.: NORM-LDG-00007070.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Autobrake may be used provided the available landing distance is compatible with the performance
of the associated selected automatic mode.
Its use does not relieve the pilot of the responsibility to achieve a safe stop within the available
runway length, if necessary by taking over brake control with brake pedals.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
APPROACH AND LANDING
GLG A319-112 FLEET NORM-LDG P 2/2
AFM ← D 25 JAN 11
Disengagement of automatic braking system may be done either by firm action on the brake pedals
or by pressing the pushbutton of the armed mode.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
DEMONSTRATED SYSTEM CONFIGURATION
GLG A319-112 FLEET NORM-22-CONF P 1/2
AFM A to E 13 JUN 17
AP/FD, SPEED MODES, AUTOTHRUST
Ident.: NORM-22-CONF-00009463.0001001 / 23 NOV 09 APPROVED
Criteria: SA
All AP/FD modes may be used with or without autothrust except if specified.
Autothrust may be used with or without AP/FD, in selected or managed speed/Mach.
TAKEOFF
Ident.: NORM-22-CONF-00009464.0001001 / 02 DEC 13 APPROVED
Criteria: SA
Autopilot engagement is approved with use of SRS + (HDG, TRK, RWY, RWY TRK or NAV) at or
above 100 ft AGL and at least 5 s after liftoff.
At acceleration altitude, the use of CLB or OP CLB or V/S or FPA or ALT* or ALT mode is approved.
Use of FD is approved in the same modes after the rotation.
CLIMB, CRUISE, DESCENT
Ident.: NORM-22-CONF-00009465.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 24414)
The use of AP or FD in the following modes is approved:
‐ Lateral modes: HDG, TRK, NAV
‐ Vertical modes: V/S, FPA, ALT*, ALT, ALT CRZ, ALT CST, OP CLB, OP DES, CLB, DES.
NON PRECISION APPROACH
Ident.: NORM-22-CONF-00009466.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The following modes are approved to be used with AP and/or FD:
‐ Lateral modes: LOC, HDG, TRK, NAV, APP NAV
‐ Vertical modes: ALT*, ALT, V/S, FPA, FINAL APP.
CAT I ILS APPROACH
Ident.: NORM-22-CONF-00009467.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The use of AP and/or FD with or without autothrust is approved in APPR modes (GS*, LOC*, GS,
LOC, LAND).
Dual AP engagement is approved.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
DEMONSTRATED SYSTEM CONFIGURATION
GLG A319-112 FLEET NORM-22-CONF P 2/2
AFM F to I 13 JUN 17
CAT II ILS APPROACH
Ident.: NORM-22-CONF-00009468.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The use of AP with or without FD with or without autothrust is approved in APPR modes (GS*, LOC*,
GS, LOC, LAND).
Dual AP engagement is approved.
One engine may be inoperative.
Note: Compliance with CAT II approach criteria has been demonstrated with CAT II or CAT III
performance quality ILS beam only.
CAT II/III ILS APPROACH AND AUTOMATIC APPROACH
Ident.: NORM-22-CONF-00009469.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The use of AP with or without FD with autothrust for CAT III and with or without autothrust for CAT II
is approved in APPR modes (GS*, LOC*, GS, LOC, LAND, FLARE, ROLL OUT) in CONF FULL and
CONF 3.
Dual AP engagement is approved.
Note: 1. CAT III Dual approach is not available with one engine inoperative.
2. Compliance with CAT II and CAT III approach and landing criteria has been
demonstrated with CAT II and CAT III performance quality ILS beam only.
GO-AROUND
Ident.: NORM-22-CONF-00009470.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The use of AP and/or FD is approved with use of SRS + (GA TRK, HDG, TRK or NAV) modes.
At acceleration altitude, the use of CLB or OP CLB or V/S or FPA or ALT* or ALT mode is approved.
ALTITUDE LOSS AFTER AUTOMATIC GO-AROUND INITIATION
Ident.: NORM-22-CONF-00009472.0003001 / 23 NOV 09 APPROVED
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115)
Initiation Height (ft) Height Loss (ft)
50 ft to 100 ft 30 ft
40 ft 25 ft
30 ft 20 ft
20 ft 15 ft
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
NON PRECISION APPROACH
GLG A319-112 FLEET NORM-22-NPA P 1/2
AFM A to B 14 DEC 13
GENERAL
Ident.: NORM-22-NPA-00009575.0001001 / 02 DEC 13 APPROVED
Criteria: SA
The final approach (FAF or FAP to runway or MAP), as extracted from the navigation database and
inserted in the primary F-PLN including altitude constraints, must not be modified by the crew.
Before starting the approach, the crew must check the lateral and vertical profile of the FMS
approach against the published approach chart.
INSTRUMENT APPROACH USING NAV MODE
Ident.: NORM-22-NPA-00009576.0004001 / 02 DEC 13 APPROVED
Criteria: ((A319 or A320 or A321) and ((25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635) and 150110))
For approach procedure with A/C in GPS PRIMARY
If GPS PRIMARY LOST indication appears on ND during the approach:
Discontinue the approach, unless:
‐ GPS PRIMARY is lost on only one FMGC, the approach can be continued using AP/FD
associated to the other FMGC.
‐ GPS is not required and navigation accuracy is confirmed against the radio navaid raw
data, or
If FM/GPS POS DISAGREE ECAM caution is triggered during the approach:
Discontinue the approach unless radio navaid raw data is available and indicates correct
navigation to continue the approach using selected FMGS modes.
For RNAV(GNSS) approaches with LNAV/VNAV Minimum:
Between the FAP and the DA, discontinue the approach as soon as the deviation below the
vertical path exceed 75 ft unless external visual references are sufficient.
For approach procedure without GPS PRIMARY
Before starting the approach, check FM position accuracy with radio navaid raw data.
If HIGH accuracy is lost during a VOR, VOR/DME, NDB or NDB/DME instrument
approach procedure:
The approach can be continued in NAV mode if the navigation accuracy is confirmed against
the radio navaid raw data.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
NON PRECISION APPROACH
Intentionally left blank
GLG A319-112 FLEET NORM-22-NPA P 2/2
AFM 14 DEC 13
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
PRECISION APPROACH
GLG A319-112 FLEET NORM-22-PA P 1/4
AFM A → 16 MAR 15
CAT II AND CAT III APPROACH AND/OR AUTOMATIC LANDING
Ident.: NORM-22-PA-00009482.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A321)
Before the approach:
Select DH (or «NO» DH if applicable).
Note: For automatic landing in CAT I or better weather condition, select appropriate MDA.
During interception of final approach:
Arm APPR mode.
Check approach phase is active on MCDU PERF page.
Engage second autopilot if available.
Engage autothrust (not required for CAT II).
Note: Approach speed is VLS + wind correction (minimum wind correction: 5 kt, maximum
wind correction: 15 kt).
Check desired capability on PFD.
Note: If APPR is selected at high altitude, CAT 1 only will be displayed initially on FMA. The
valid capability will be displayed at lower altitude.
During final approach and landing:
At 350 ft RA, check ″LAND″ is displayed on PFD and ILS/MLS course on heading scale.
At 30 ft, check ”FLARE” is displayed on PFD.
At 10 ft, reduce thrust to idle.
At touchdown, check ”ROLL OUT” is displayed on PFD.
At the latest when leaving the runway, disconnect the autopilot.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
PRECISION APPROACH
GLG A319-112 FLEET NORM-22-PA P 2/4
AFM ← A to B → 16 MAR 15
Note: 1. For CAT II automatic approach, the autopilot should be disconnected at or above
80 ft if manual landing is intended.
2. For CAT III A automatic approach and landing, the autopilot may be disconnected at
touchdown if external visual references are sufficient.
3. A callout (indicating that a flight parameter is exceeded) must be made if:
‐ Speed goes below VAPP - 5 kt or above VAPP + 10 kt
‐ Pitch attitude goes below -2.5 ° or above +10 ° nose up
‐ Bank angle goes above 7 °
‐ Descent rate goes above 1 000 ft/min
‐ Excessive LOC or GLIDE deviation occurs.
4. For CAT II approach climb performance, refer to FCOM In Flight Performance
Chapter.
5. Whenever the required landing distance for automatic landing is higher than the
required landing distance for manual landing, corrections to be added to the required
landing distance for manual landing (provided by the Performance Engineer's
Programs/AFM_OCTO approved FM module at the latest approved revision reported
in Performance chapter of this AFM) are given in the Automatic Landing Distance
Increment chapter of this AFM Refer to PERF-LDG Autoland Landing Distance
Increments. The required landing distance for automatic landing is calculated with
the same braking conditions as for manual landing (i.e. full pilot braking at main
landing gear touchdown) but with a lower multiplicative coefficient (1.15 instead of
1.66).
REQUIRED EQUIPMENT FOR CAT II AND CAT III APPROACH AND LANDING
Ident.: NORM-22-PA-00009476.0001001 / 14 JAN 15 APPROVED
Criteria: SA
Required Equipment CAT II CAT III Single CAT III Dual
AP 1 AP engaged 1 AP engaged 2 AP engaged
AP disconnect P/B 2 2 2
Autothrust 0 1 1
ILS or MLS Receiver 2 2 2
Attitude Indication N°1+N°2+STBY N°1+N°2+STBY N°1+N°2+STBY
PFD/ND Displays 2/1 2/2 2/2
Radio Altimeter 1 (But two display) 2 2
Auto Callout Radio Altimeter 1(3) 1 1
DH Indication 1(1) 1(1) 1(1)
Flight Warning Computer 1 1 2
"AP OFF" warning 1 1 2
"AUTOLAND" light 1 1 1
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
PRECISION APPROACH
GLG A319-112 FLEET NORM-22-PA P 3/4
AFM ← B 16 MAR 15
Continued from the previous page
Required Equipment CAT II CAT III Single CAT III Dual
Rain Repellent (if activated)
or Windshield Wipers 1(2) 1(2) 1(2)
Windshield Heat 1(2) 1(2) 1(2)
Nosewheel steering 1(5) 1(5) 1
Antiskid 1(5) 1(5) 1
BSCU Channel 1(5) 1(5) 1
Beam Excessive Deviation 1(1) 2 2
FMA 1 2 2
"A/THR OFF" caution 0 1 1
Rudder Travel Limit 1(4) 1(4) 1(4)
Yaw Damper/Rudder Trim 1/1 1/1 2/2
ELAC 1 1 2
ADR/IR 2/2 2/2 3/3
FAC 1 1 2
Hydraulic Circuit 2 2 3
FMGC Electrical Supply Split 0 0 1
(1) One unit required for the PM.
(2) One unit required for the PF.
(3) Required only for autoland.
(4) Required only for autoland with crosswind above 12 kt.
(5) Required only for autoland rollout.
Note: 1. Compliance with CAT II approach and landing criteria has been demonstrated with CAT
II and CAT III performance quality ILS/MLS beam only.
2. Compliance with CAT III approach and landing criteria has been demonstrated with CAT
II and CAT III performance quality ILS/MLS beam only.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
PRECISION APPROACH
Intentionally left blank
GLG A319-112 FLEET NORM-22-PA P 4/4
AFM 16 MAR 15
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FUEL
GLG A319-112 FLEET NORM-28 P 1/2
AFM A 25 JAN 11
FUEL SYSTEM
Ident.: NORM-28-00009172.0001001 / 23 NOV 09 APPROVED
Criteria: ((A320 and 20024) or (A318 or A319 or A321))
Tanks must be emptied in the following order:
1. Center tank
2. Wing tanks.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
FUEL
Intentionally left blank
GLG A319-112 FLEET NORM-28 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
ICE AND RAIN PROTECTION
GLG A319-112 FLEET NORM-30 P 1/2
AFM A to B 25 JAN 11
OPERATIONS IN ICING CONDITIONS
Ident.: NORM-30-00007071.0001001 / 23 NOV 09 APPROVED
Criteria: SA
For icing conditions definition: Refer to LIM-70 Operations in Icing Conditions.
When icing conditions are encountered:
Turn on engine anti-ice.
Set wing anti-ice as required.
If there is evidence of significant ice accretion and to take into account ice formation on
non heated structure:
If CONF FULL:
Minimum speed: VLS + 5 kt
If CONF below FULL:
Minimum speed: VLS + 10 kt
CAUTION 1. Extended flight in icing conditions with slats extended should be avoided.
2. Apply performance adjustments according to the note of the Approach Climb and
Landing Climb, Refer to PERF-LDG Approach Climb and Landing Climb.
RAIN REPELLENT (IF ACTIVATED)
Ident.: NORM-30-00007080.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Use rain repellent in the case of heavy rain only.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
ICE AND RAIN PROTECTION
Intentionally left blank
GLG A319-112 FLEET NORM-30 P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET NORM-34 P 1/2
AFM A to C 13 JUN 17
GROUND PROXIMITY WARNING SYSTEM (GPWS)
Ident.: NORM-34-00007081.0001001 / 23 NOV 09 APPROVED
Criteria: SA
When a warning occurs:
Pull up using full back stick.
Apply takeoff thrust and climb until the warning ceases.
Warnings may be considered cautionary during daylight VMC conditions provided the cause of
the warning can be identified immediately.
When a caution occurs:
Adjust the flight path/configuration so that the caution alert ceases.
INERTIAL REFERENCE SYSTEM (IRS)
Ident.: NORM-34-00009174.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Ensure IRS alignment is complete and all IR are in the NAV mode before the aircraft is moved.
When an IR is in the ATT mode:
Magnetic heading will drift after initialization in a manner similar to a directional gyro and requires
crew monitoring and periodic manual heading updates to ensure adequate accuracy.
REDUCED VERTICAL SEPARATION MINIMUM (RVSM)
Ident.: NORM-34-00009175.0002001 / 23 NOV 09 APPROVED
Criteria: (A318 or ((A319 or A320 or A321) and (31039 or 31528)))
The following table gives the minimum equipment/functions required to begin RVSM operation.
Required Equipment/Functions Quantity
ADR 2
ATC Transponder 1
Flight Warning Computer (for Altitude Alert function) 1
Autopilot 1
PFD function (for altitude indication) 2
FCU (for altitude target selection and
OP CLB/OP DES mode engagement) 1
Minimum Equipment/Functions Required to begin RVSM Operation
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
NAVIGATION
GLG A319-112 FLEET NORM-34 P 2/2
AFM D 13 JUN 17
WINDSHEAR WARNING AND GUIDANCE SYSTEM
Ident.: NORM-34-00009761.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 22249)
Windshear detection is available below 1 300 ft at takeoff, approach and go-around.
In the case of warning, TOGA power application provides guidance in SRS mode, using FD or AP .
If engaged AP may be used for go-around.
FD guidance may lead to speeds of VALPHAMAX (top of the red strip along the speed scale of the
PFD).
The aircraft configuration should not be changed before end of windshear conditions.
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUXILIARY POWER UNIT
GLG A319-112 FLEET NORM-49 P 1/2
AFM A 25 JAN 11
AUXILIARY POWER UNIT (APU)
Ident.: NORM-49-00006923.0009001 / 23 NOV 09 APPROVED
Criteria: (SA and 25888)
STARTING IN FLIGHT
Up to 41 000 ft, using main electrical power supply.
Up to 25 000 ft, using batteries.
AIR BLEED EXTRACTION IN FLIGHT
At ISA:
Two air conditioning packs up to 15 000 ft (GEN LOAD 100 % (90 KVA) maximum).
One air conditioning pack, up to 22 500 ft (GEN LOAD 77 % (70 KVA) maximum).
Engine starting assistance up to 20 000 ft.
Airbleed extraction for wing anti-ice is not permitted.
MAXIMUM GEN LOAD DURING ENG START ON GROUND
At ISA, 100 % (90 KVA) from sea level up to 14 500 ft.
At ISA + 35 °C, from 90 % (81 KVA) at sea level to 71 % (70 KVA) at 14 500 ft.
FLIGHT WITH APU REMOVED
Flight with APU removed is authorized in accordance with SIL 49-009 revision 7 (or higher).
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
AUXILIARY POWER UNIT
Intentionally left blank
GLG A319-112 FLEET NORM-49 P 2/2
AFM 25 JAN 11
PERFORMANCE
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET PERF-PLP-TOC P 1/2
AFM 12 DEC 17
PERF-GEN GENERAL
Introduction...............................................................................................................................................................A
Aircraft Configuration............................................................................................................................................... B
Maximum Demonstrated Crosswind at Takeoff and Landing................................................................................. C
PERF-CAL AIRSPEED AND ALTITUDE CALIBRATION
PERF-CAL-TO TAKEOFF
Speed Corrections in Ground Effect....................................................................................................................... A
Speed Corrections out of Ground Effect.................................................................................................................B
Altitude Corrections................................................................................................................................................. C
PERF-CAL-CRU CRUISE (Clean Configuration)
Speed and Mach Corrections..................................................................................................................................A
Altitude Corrections..................................................................................................................................................B
PERF-CAL-LDG LANDING
Speed Corrections in Ground Effect....................................................................................................................... A
Speed Corrections Out of Ground Effect................................................................................................................B
Altitude Corrections................................................................................................................................................. C
PERF-TO TAKEOFF PERFORMANCE
Speeds Definitions...................................................................................................................................................A
Distances Definitions............................................................................................................................................... B
Takeoff Performance............................................................................................................................................... C
Takeoff Flight Path.................................................................................................................................................. D
PERF-FLT IN FLIGHT PERFORMANCE
In-Flight Performance.............................................................................................................................................. A
PERF-LDG LANDING PERFORMANCE
Approach Climb and Landing Climb....................................................................................................................... A
Approach and Landing Speeds Definition...............................................................................................................B
Landing Distance Definitions...................................................................................................................................C
Landing Performance.............................................................................................................................................. D
Autoland Landing Distance Increments...................................................................................................................E
1PERF-OCTO PERFORMANCE DATABASE
General.....................................................................................................................................................................A
Performance Database............................................................................................................................................B
Complementary Performance Data File .................................................................................................................C
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET PERF-PLP-TOC P 2/2
AFM 12 DEC 17
Continued from the previous page
PERF-ENG ENGINE MANAGEMENT
Takeoff Thrust..........................................................................................................................................................A
Maximum Continuous Thrust...................................................................................................................................B
Go-Around Thrust....................................................................................................................................................C
PERF-FLEX REDUCED THRUST TAKEOFF
Reduced Thrust Takeoff..........................................................................................................................................A
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
GLG A319-112 FLEET PERF-PLP-SOH P 1/2
AFM 12 DEC 17
Localization
Title
Toc
Index
ID Reason
PERF-PLP-TOC
PERFORMANCE DATABASE
1Documentation update: Deletion of the "00021722.0001001
Complementary Performance Data File" documentary unit.
PERF-OCTO
Complementary Performance Data
File
C1Documentation update: Addition of "Complementary Performance
Data File" documentary unit
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
Intentionally left blank
GLG A319-112 FLEET PERF-PLP-SOH P 2/2
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
GENERAL
GLG A319-112 FLEET PERF-GEN P 1/2
AFM A 25 JAN 11
INTRODUCTION
Ident.: PERF-GEN-00006988.0001001 / 23 NOV 09 APPROVED
Criteria: SA
In compliance with airworthiness regulations, an aircraft is cleared to take off from any airport if the
weight allows it to achieve the takeoff, "en route", and landing performance included in this chapter.
Note: The performance and speeds of the lowest weight at which the Performance Engineer's
Programs/AFM_OCTO approved FM module is able to give results can be considered as
valid from this weight down to the certified minimum weight.
The considered atmosphere is the international standard atmosphere.
Performance are related to VS1G.
Wind speed is measured at the height of 10 m (32.8 ft).
The results provided by he Performance Engineer's Programs/AFM_OCTO approved FM module
must be used in conjunction with the gross weight, operational and environmental limitations given in
theLIMITATIONS chapter of this AFM.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
GENERAL
GLG A319-112 FLEET PERF-GEN P 2/2
AFM B to C 25 JAN 11
AIRCRAFT CONFIGURATION
Ident.: PERF-GEN-00007266.0001001 / 23 NOV 09 APPROVED
Criteria: (A319 or A320 or A321)
The performance has been established in the following configuration :
Slats / Flaps Engine Thrust Remarks
Takeoff 1+F
2
3
Takeoff thrust Ground spoilers armed.
Dry runway
Acceleration Stop Distance (ASD) made using only
wheel brakes, brakes supplied by green hydraulic
system, antiskid ON and ground spoilers.
Wet runway
Acceleration Stop Distance (ASD) made using only
wheel brakes, brakes supplied by green hydraulic
system, antiskid ON, ground spoilers and with or
without thrust reversers.
En route 0 Maximum Continuous Thrust
(MCT)
Go-around 2
3
Go-around thrust taking
Mach number into account
Landing 3
FULL
Landing distances established with brake pedals
depressed upon main landing gear touchdown, brakes
supplied by green hydraulic system, antiskid ON and
using ground spoilers.
Systems which may be ON or OFF:
‐ Air conditioning
‐ Wing anti-ice or engine anti-ice.
Note: For normal operation, use of thrust reversers is recommended.
MAXIMUM DEMONSTRATED CROSSWIND AT TAKEOFF AND LANDING
Ident.: PERF-GEN-00007267.0001001 / 03 AUG 10 APPROVED
Criteria: (A319 or A320 or A321)
At takeoff and landing: 38 kt (gust included).
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
TAKEOFF
GLG A319-112 FLEET PERF-CAL-TO P 1/4
AFM A → 25 JAN 11
SPEED CORRECTIONS IN GROUND EFFECT
Ident.: PERF-CAL-TO-00007268.0003001 / 23 NOV 09 APPROVED
Criteria: A319
CAPTAIN AND FIRST OFFICER ADR 1 OR 2
ADR 3
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
TAKEOFF
GLG A319-112 FLEET PERF-CAL-TO P 2/4
AFM ← A 25 JAN 11
STANDBY AIRSPEED INDICATOR
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
TAKEOFF
GLG A319-112 FLEET PERF-CAL-TO P 3/4
AFM B 25 JAN 11
SPEED CORRECTIONS OUT OF GROUND EFFECT
Ident.: PERF-CAL-TO-00007269.0004001 / 23 NOV 09 APPROVED
Criteria: A319
ADR 1 OR 2 OR 3
ΔV = IAS - CAS ≤ ± 1 kt
STANDBY AIRSPEED INDICATOR
CONF. 1
CONF. 2
CONF. 3
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
TAKEOFF
GLG A319-112 FLEET PERF-CAL-TO P 4/4
AFM C 25 JAN 11
ALTITUDE CORRECTIONS
Ident.: PERF-CAL-TO-00007270.0004001 / 23 NOV 09 APPROVED
Criteria: A319
ADR 1 OR 2 OR 3
ΔZP ≤ ± 20 ft
STANDBY ALTITUDE INDICATOR
CONF. 1
CONF. 2
CONF. 3 L/G UP
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
CRUISE (CLEAN CONFIGURATION)
GLG A319-112 FLEET PERF-CAL-CRU P 1/2
AFM A to B 25 JAN 11
SPEED AND MACH CORRECTIONS
Ident.: PERF-CAL-CRU-00007271.0002001 / 23 NOV 09 APPROVED
Criteria: (((A320 or A321) and (25490 or 25570)) or A319)
ADR 1 OR 2 OR 3
ΔM ≤ 0.007
ΔV ≤ ± 1.8 kt
ALTITUDE CORRECTIONS
Ident.: PERF-CAL-CRU-00007272.0002001 / 23 NOV 09 APPROVED
Criteria: (((A320 or A321) and (25490 or 25570)) or A319)
ADR 1 OR 2 OR 3
ΔZP ≤ ± 150 ft
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
CRUISE (CLEAN CONFIGURATION)
Intentionally left blank
GLG A319-112 FLEET PERF-CAL-CRU P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 1/6
AFM A → 25 JAN 11
SPEED CORRECTIONS IN GROUND EFFECT
Ident.: PERF-CAL-LDG-00007273.0003001 / 23 NOV 09 APPROVED
Criteria: A319
CAPTAIN AND FIRST OFFICER ADR 1 OR 2
ADR 3
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 2/6
AFM ← A 25 JAN 11
STANDBY AIRSPEED INDICATOR
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 3/6
AFM B → 25 JAN 11
SPEED CORRECTIONS OUT OF GROUND EFFECT
Ident.: PERF-CAL-LDG-00007274.0004001 / 03 AUG 10 APPROVED
Criteria: A319
ADR 1 OR 2 OR 3
ΔV = IAS - CAS ≤ ± 1 kt
STANDBY AIRSPEED INDICATOR
CONF 3 LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 4/6
AFM ← B 25 JAN 11
CONF FULL
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 5/6
AFM C → 25 JAN 11
ALTITUDE CORRECTIONS
Ident.: PERF-CAL-LDG-00007275.0004001 / 03 AUG 10 APPROVED
Criteria: A319
ADR 1 OR 2 OR 3
ΔZP ≤ ± 20 ft
STANDBY ALTITUDE INDICATOR
CONF 3 LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
LANDING
GLG A319-112 FLEET PERF-CAL-LDG P 6/6
AFM ← C 25 JAN 11
CONF FULL
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
TAKEOFF PERFORMANCE
GLG A319-112 FLEET PERF-TO P 1/4
AFM A 08 APR 11
SPEEDS DEFINITIONS
Ident.: PERF-TO-00006991.0001001 / 23 NOV 09 APPROVED
Criteria: SA
V1:
V1 is the highest speed at which the decision must be made:
‐ To continue the takeoff, or
‐ To stop the aircraft.
VR:
VR is the speed at which rotation is initiated to reach V2 before an altitude of 35 ft.
V2:
V2 is the takeoff safety speed reached before the altitude of 35 ft with one engine failed and
providing not less than the minimum second segment gradient (2.4 %).
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
TAKEOFF PERFORMANCE
GLG A319-112 FLEET PERF-TO P 2/4
AFM B 08 APR 11
DISTANCES DEFINITIONS
Ident.: PERF-TO-00006992.0001001 / 23 NOV 09 APPROVED
Criteria: SA
STOPWAY (SWY):
Extension to runway, adequate for deceleration of the aircraft in the case of aborted takeoff.
CLEARWAY (CWY):
Area beyond the runway which can be taken into account for TOD calculation.
TAKEOFF DISTANCE AVAILABLE (TODA):
Sum of the TORA and the CWY available.
TAKEOFF RUN AVAILABLE (TORA):
Length of runway available and suitable for the ground run of an aircraft taking off.
ACCELERATE-STOP DISTANCE AVAILABLE (ASDA):
Sum of the TORA and the SWY available.
TAKEOFF DISTANCE (TOD):
Distance covered from the brake release to a point at which the aircraft is at the 35 ft height (15 ft
height on wet runway). The TOD must not exceed the TODA.
TAKEOFF RUN (TOR):
Distance covered from the brake release to a point at which the aircraft is half of the segment
between the liftoff speed (VLOF) and 35 ft height (15 ft height on wet runway). The TOR must not
exceed the TORA.
ACCELERATE-STOP DISTANCE (ASD):
Distance necessary to accelerate the aircraft to V1, reject the takeoff at V1 and come to a full stop.
The ASD must not exceed the ASDA.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
TAKEOFF PERFORMANCE
GLG A319-112 FLEET PERF-TO P 3/4
AFM C 08 APR 11
TAKEOFF PERFORMANCE
Ident.: PERF-TO-00006904.0001001 / 23 NOV 09 APPROVED
Criteria: SA
For takeoff performance determination on dry and wet runway, the Performance Engineer's
Programs/AFM_OCTO approved FM module at the latest approved revision must be used. Refer to
PERF-OCTO Performance Database.
CAUTION For takeoff performance on wet runways the takeoff weight must be the lowest of the
computed one on dry runways and the computed one on wet runways.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
TAKEOFF PERFORMANCE
GLG A319-112 FLEET PERF-TO P 4/4
AFM D 08 APR 11
TAKEOFF FLIGHT PATH
Ident.: PERF-TO-00006935.0001001 / 04 APR 11 APPROVED
Criteria: SA
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
IN FLIGHT PERFORMANCE
GLG A319-112 FLEET PERF-FLT P 1/2
AFM A 08 APR 11
IN-FLIGHT PERFORMANCE
Ident.: PERF-FLT-00006995.0006001 / 04 APR 11 APPROVED
Criteria: A319
For en route net flight path (single engine cruise) performance determination, the Performance
Engineer's Programs/AFM_OCTO approved FM module at the latest approved revision must be
used. Refer to PERF-OCTO Performance Database.
Note: In the case of severe icing conditions, ice accretion may occur on aircraft surfaces that are
not heated. If ice accretion occurs, reduce the one-engine inoperative net ceiling by the
following amount, as applicable:
‐ By 4 000 ft when the aircraft weight is below or equal to 60 000 kg (132 277 lb)
‐ By 7 500 ft when the aircraft weight is above or equal to 75 000 kg (165 347 lb).
Apply a linear interpolation between these two aircraft weights.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
IN FLIGHT PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET PERF-FLT P 2/2
AFM 08 APR 11
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
LANDING PERFORMANCE
GLG A319-112 FLEET PERF-LDG P 1/4
AFM A to B 14 DEC 13
APPROACH CLIMB AND LANDING CLIMB
Ident.: PERF-LDG-00006909.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A321)
The approach climb speed is at least 1.23 VS1G of the approach configuration, approach speed up
to 1.41 VS1G is permitted.
For approach and landing climb limiting weight determination the Performance Engineer's
Programs/AFM_OCTO approved FM modules at the latest approved revision must be used. Refer to
PERF-OCTO Performance Database
Note: 1. The go around gradient conditions in landing configuration with two engines operative
are never limiting.
2. When icing conditions are predicted during the flight and TAT is below 10 °C and there is
evidence of significant ice accretion, to take into account ice formation on the non heated
structure:
‐ Decrease the approach/landing climb limiting weight by 7.2 %.
‐ For landing, increase the approach and landing speeds by:
‐ 10 kt in CONF 3
‐ 5 kt in CONF FULL
‐ For landing distance determination select ice accretion in the AFM_OCTO input data
Interface.
APPROACH AND LANDING SPEEDS DEFINITION
Ident.: PERF-LDG-00006996.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The final approach speed (landing speed) is the minimum recommended speed at 50 ft height for
normal landing. It is equal to 1.23 VS1G of the landing configuration.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
LANDING PERFORMANCE
GLG A319-112 FLEET PERF-LDG P 2/4
AFM C to D 14 DEC 13
LANDING DISTANCE DEFINITIONS
Ident.: PERF-LDG-00006997.0001001 / 23 NOV 09 APPROVED
Criteria: SA
ACTUAL LANDING DISTANCE (ALD)
The Actual Landing Distance (ALD) represents the distance from the 50 ft height point to complete
stop on a smooth, dry, hard-surfaced runway. It is determined with brake pedals depressed at
main landing gear touch down, and assumes the use of ground spoilers and antiskid. In normal
operation, the use of thrust reversers is recommended.
REQUIRED LANDING DISTANCE (RLD)
The Required Landing Distance (RLD) is the Actual Landing Distance (ALD) divided by 0.6
assuming the surface is dry.
Under wet runway conditions, the Required Landing Distance (RLD) is increased by 15 %.
LANDING PERFORMANCE
Ident.: PERF-LDG-00006910.0001001 / 23 NOV 09 APPROVED
Criteria: SA
For landing distance determination, the Performance Engineer's Programs/AFM_OCTO approved
FM modules at the latest approved revision must be used. Refer to PERF-OCTO Performance
Database.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
LANDING PERFORMANCE
GLG A319-112 FLEET PERF-LDG P 3/4
AFM E → 14 DEC 13
AUTOLAND LANDING DISTANCE INCREMENTS
Ident.: PERF-LDG-00006998.0007001 / 23 NOV 09 APPROVED
Criteria: (319-111 or 319-112 or 319-115)
When performing an automatic landing , the required landing distance on dry runway of this chapter
must be increased as follows:
CONF FULL
WEIGHT WIND
(kt) LANDING DISTANCE INCREMENT
0 0
5 0
10 0
15 0
20 0
25 0
42 000 kg
(92 600 lb)
30 12 m/40 ft
0 0
5 0
10 0
15 0
20 0
25 11 m/36 ft
45 000 kg
(92 200 lb)
30 30 m/99 ft
0 0
5 0
10 0
15 0
20 0
25 17 m/55 ft
50 000 kg
(110 230 lb)
30 34 m/112 ft
0 0
5 0
10 0
15 0
20 0
25 0
55 000 kg
(121 250 lb)
30 11 m/37 ft
0 0
5 0
10 0
15 0
20 0
25 0
60 000 kg
(132 280 lb)
30 0
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
LANDING PERFORMANCE
GLG A319-112 FLEET PERF-LDG P 4/4
AFM ← E 14 DEC 13
Continued from the previous page
CONF FULL
WEIGHT WIND
(kt) LANDING DISTANCE INCREMENT
0 0
5 0
10 0
15 0
20 0
25 0
65 000 kg
(143 300 lb)
30 0
Increase by 15 % on foreseen wet runway.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PERFORMANCE DATABASE
GLG A319-112 FLEET PERF-OCTO P 1/4
AFM A 12 DEC 17
GENERAL
Ident.: PERF-OCTO-00021844.0001001 / 11 AUG 17 APPROVED
Criteria: (318-111 or 318-112 or 318-121 or 318-122 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 319-131 or 319-132 or
319-133 or 320-211 or 320-212 or 320-214 or 320-215 or 320-216 or 320-231 or 320-232 or 320-233 or 321-111 or 321-112 or 321-131 or
321-211 or 321-212 or 321-213 or 321-231 or 321-232)
The aircraft performance database is provided in the Performance Engineer’s Program
(PEP)/AFM_OCTO Approved FM module. The aircraft performance database provides the
performance data applicable to an aircraft model, Refer to PERF-OCTO Performance Database.
The aircraft performance database must be combined with the following applicable data files:
‐ The in-flight failure data file for landing that provides the performance impact for landing
in the case of an aircraft system failure, Refer to EMER-GEN LANDING DISTANCE
DETERMINATION IN CASE OF IN-FLIGHT FAILURE and Refer to ABN-GEN LANDING
DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE.
‐ The MCDL performance penalties data file that provides the performance impact related to the
MCDL items, Refer to MCDL-GEN-PERF Performance Penalties calculated with AFM_OCTO
Software
‐ The complementary performance data file (CPDF) that provides the complementary performance
data, Refer to PERF-OCTO Complementary Performance Data File .
Note: The three above-listed data files are applicable to an aircraft type.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PERFORMANCE DATABASE
GLG A319-112 FLEET PERF-OCTO P 2/4
AFM B 12 DEC 17
PERFORMANCE DATABASE
Ident.: PERF-OCTO-00006895.0028001 / 23 NOV 09 APPROVED
Criteria: (319-112 and (32619 or 33239))
Takeoff, final takeoff, en route net flight path (single engine), go-around and landing performance are
provided in the Performance Engineer's Programs/AFM_OCTO approved FM module:
‐ At the revision 21.0 or higher using approved aircraft database reference AD112E01 or,
‐ At the revision 26.0 or higher using approved aircraft database reference AD112H02.
Note: 1. Only the PC version of this program is approved.
2. For operations on runways with a slope between 2 % and 3 % (optional: mod 37251),
only the approved database reference AD112H02 must be used.
3. For takeoff on PFC/grooved runways (optional: mod 35075), only the approved database
reference AD112H02 must be used.
4. For landing on PFC/grooved runways (optional: mod 37457), only the approved database
reference AD112H02 must be used.
5. For derated takeoff (optional: mod 36481), only the approved database reference
AD112H02 must be used.
6. For extended flex temperature (optional: mod 36750) performance computation, only the
approved database reference AD112H02 must be used.
7. For alternate CG (optional: mod 34126) performance computation, only the approved
database reference AD112H02 must be used.
Launch PEP.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PERFORMANCE DATABASE
GLG A319-112 FLEET PERF-OCTO P 3/4
AFM C 12 DEC 17
COMPLEMENTARY PERFORMANCE DATA FILE
1Ident.: PERF-OCTO-00021722.0005001 / 07 NOV 17 APPROVED
Criteria: SA
In addition to the aircraft performance database, the Complementary Performance Data File (CPDF
) provides complementary performance data. The CPDF is applicable to the A320 Family and
contains:
‐ Approved data and
‐ Not approved data.
Note: Only the approved version of the CPDF database is referenced in the AFM.
The performance data listed in the table below (i.e. Performance Data Column) requires the
approved Complementary Performance Data File (CPDF ) to be used for aircraft operations.
Approved CPDF Required version of
PEP/AFM_OCTO FM module Performance Data(1) Applicability
CP32FA01 V34 or higher ‐ Computerized performance
penalties in the case of ice
accretion
A320 Family (except neo)
‐ Integration of ROW data A320 Family (except neo)CP32FA02 V34 or higher
‐ Autoland A321neo equipped with CFM
engines and Autoland
V34 or higher ‐ Introduction of wet snow and
dry snow contaminants
A320 Family without Sharklet
V35 or higher ‐ Autoland A321neo equipped with Pratt &
Whitney engines and Autoland
CP32FA03
V34 or higher (V35 or higher for
neo) ‐ Tachometer inoperative item
for MMEL
A320 Family equipped with
BSCU L4.10
(1) Only the performance data that is inserted between two successive CPDF files is listed. The most
recent version of the CPDF combines all the listed Performance Data.
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
PERFORMANCE DATABASE
Intentionally left blank
GLG A319-112 FLEET PERF-OCTO P 4/4
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
GLG A319-112 FLEET PERF-ENG P 1/6
AFM A → 25 JAN 11
TAKEOFF THRUST
Ident.: PERF-ENG-00006989.0022001 / 23 NOV 09 APPROVED
Criteria: 319-112
CFM 56-5B6 - TAKEOFF M = .0
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
GLG A319-112 FLEET PERF-ENG P 2/6
AFM ← A 25 JAN 11
CFM 56-5B6 - TAKEOFF M = .0
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
GLG A319-112 FLEET PERF-ENG P 3/6
AFM B 25 JAN 11
MAXIMUM CONTINUOUS THRUST
Ident.: PERF-ENG-00007420.0015001 / 23 NOV 09 APPROVED
Criteria: (319-111 or 319-112)
CFM 56-5B5 / CFM 56-5B6 - MAXIMUM CONTINUOUS - VC = 230 kt
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
GLG A319-112 FLEET PERF-ENG P 4/6
AFM C → 25 JAN 11
GO-AROUND THRUST
Ident.: PERF-ENG-00007455.0012001 / 23 NOV 09 APPROVED
Criteria: 319-112
CFM 56-5B6 - GO-AROUND M = .225
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
GLG A319-112 FLEET PERF-ENG P 5/6
AFM ← C 25 JAN 11
CFM 56-5B6 - GO-AROUND M = .225
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
ENGINE MANAGEMENT
Intentionally left blank
GLG A319-112 FLEET PERF-ENG P 6/6
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
REDUCED THRUST TAKEOFF
GLG A319-112 FLEET PERF-FLEX P 1/2
AFM A 25 JAN 11
REDUCED THRUST TAKEOFF
Ident.: PERF-FLEX-00006990.0008001 / 23 NOV 09 APPROVED
Criteria: (319-112 and (32619 or 33239))
CFM56-5B6 N1 CORRECTIONS FOR AIR BLEED
AIR CONDITIONING ON - 0.7
ENG ANTI-ICE ON 0.0
FLEX TAKEOFF
N1
NO AIR BLEED
MACH .000 ENG AND WING ANTI-ICE ON 0.0
CFM56-5B6 REDUCED TAKEOFF THRUST
Example
Data:
‐ Flex temperature: +45 °C
‐ Pressure Altitude: 2 000 ft
‐ OAT: +20 °C
Result: FLEX TAKEOFF N1 = 88.4 %
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
REDUCED THRUST TAKEOFF
Intentionally left blank
GLG A319-112 FLEET PERF-FLEX P 2/2
AFM 25 JAN 11
APPENDICES AND
SUPPLEMENTS
Intentionally left blank
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 1 of 7
Airworthiness Directive
AD No.: 2017-0257R1
Issued: 09 January 2018
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation
(EC) 216/2008 on behalf of the European Union, its Member States and of the European third
countries that participate in the activities of EASA under Article 66 of that Regulation.
This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the
continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which
an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I,
Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EC) 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name:
AIRBUS
Type/Model designation(s):
A318, A319, A320 and A321 aeroplanes
Effective Date: Revision 1: 09 January 2018
Original issue: 29 December 2017
TCDS Number(s): EASA.A.064
Foreign AD: Not applicable
Revision: This AD revises EASA AD 2017-0257 dated 22 December 2017.
ATA 34 – Navigation – Back Up Speed Scale / Aircraft Flight Manual – Amendment
Manufacturer(s):
Airbus (formerly Airbus Industrie)
Applicability:
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114,
A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216,
A320-231, A320-232, A320-233, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211,
A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers that
have received Airbus modification (mod) 35871 in production or Airbus Service Bulletin (SB)
A320-34-1397 in service (introducing Air Data Monitoring and BUSS function), except aeroplanes
which have also received Airbus mod 159281 in production, or Airbus SB A320-34-1658 or
A320-34-1659 in service (installing reversible BUSS function).
Reason:
In extreme icing conditions, pitot probes may induce erroneous airspeed indications. Airbus
developed a Back-up Speed Scale (BUSS and reversible BUSS, based on angle of attack (AoA) value)
displayed on the Primary Flight Display (PFD), together with a PFD Back-Up Altitude Scale based on
Global Positioning System (GPS) altitude, to provide flight crews with reliable information on
airspeed. This BUSS is intended to be used below flight level (FL) 250 only (above FL250, the BUSS is
disconnected). Following new investigation related to AoA probes blockages, it was identified that,
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 2 of 7
when two AoA sensors are adversely affected by icing conditions at the same time, data displayed
on the BUSS could be erroneous.
This condition, if not corrected, could lead to an increased flight crew workload, possibly resulting in
reduced control of the aeroplane.
To address this potential unsafe condition, Airbus established specific operational instructions to be
applied by the flight crew under certain defined conditions. The relevant procedure has been
incorporated into the applicable A320 family Airplane Flight Manual (AFM) since 07 March 2017
(publication date).
For the reason described above, this AD requires a one-time AFM amendment to introduce the
additional operational procedure.
After EASA AD 2017-0257 was issued, an error was detected in the Applicability, which should have
been limited to aeroplanes equipped with the BUSS function.
This AD is therefore revised to correct the Applicability. The wording of the Reason and Credit
paragraphs have also been improved and the original AFM pages have been inserted in the
Appendix.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
AFM Amendment:
(1) Within 30 days after 29 December 2017 [the effective date of the original issue of this AD],
amend the applicable AFM by incorporating the procedure as specified in Appendix 1 of this
AD, inform all flight crews, and, thereafter, operate the aeroplane accordingly.
(2) Amending the applicable AFM of an aeroplane to incorporate a later AFM revision, which
includes the procedure as specified in Appendix 1 of this AD, is acceptable to comply with the
requirements of paragraph (1) of this AD for that aeroplane.
Credit:
(3) Aeroplanes operated with an AFM having the NAV – ADR 1+2+3 FAULT procedure with an
approval date on or after 02 March 2017 are compliant with the requirements of this AD.
Ref. Publications:
Airbus A318, A319, A320 and A321 AFM Revision dated 07 March 2017.
The use of later approved revisions of the above-mentioned document is acceptable for compliance
with the requirements of this AD.
Remarks:
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 3 of 7
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD
with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs@easa.europa.eu.
4. For any question concerning the technical content of the requirements in this AD, please
contact: AIRBUS – Airworthiness Office – EIAS; Fax +33 5 61 93 44 51;
E-mail: account.airworth-eas@airbus.com.
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 4 of 7
Appendix 1 – AFM Procedure
EASA AD No.: 2017-0257R1
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Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 5 of 7
Appendix 1 – AFM Procedure (continued)
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 6 of 7
Appendix 1 – AFM Procedure (continued)
EASA AD No.: 2017-0257R1
TE.CAP.00110-006 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified.
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Page 7 of 7
Appendix 1 – AFM Procedure (end)
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET APP-PLP-TOC P 1/2
AFM 12 SEP 17
APP-NOI EXTERNAL NOISE
General.....................................................................................................................................................................A
External Noise..........................................................................................................................................................B
APP-TCAS TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
General.....................................................................................................................................................................A
Procedures...............................................................................................................................................................B
APP-INOP DISPATCH WITH INOPERATIVE ITEMS
General.....................................................................................................................................................................A
Performance.............................................................................................................................................................B
APP-LGDN FLIGHT WITH LANDING GEAR DOWN
APP-LGDN-GEN GENERAL
General.....................................................................................................................................................................A
APP-LGDN-LIM LIMITATIONS
Limitations................................................................................................................................................................ A
APP-LGDN-EMER EMERGENCY PROCEDURES
ENG DUAL FAILURE..............................................................................................................................................A
APP-LGDN-ABN ABNORMAL PROCEDURES
F/CTL FLIGHT CONTROLS FAILURE................................................................................................................... A
APP-LGDN-NORM NORMAL PROCEDURES
Preflight Check.........................................................................................................................................................A
APP-LGDN-PERF PERFORMANCE
Performance.............................................................................................................................................................A
APP-LGDN-APP APPENDICES AND SUPPLEMENTS
Appendices and Supplements.................................................................................................................................A
APP-INTX ENGINE INTERMIX
APP-INTX-GEN GENERAL
General.....................................................................................................................................................................A
APP-INTX-LIM LIMITATIONS
Limitations................................................................................................................................................................ A
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET APP-PLP-TOC P 2/2
AFM 12 SEP 17
Continued from the previous page
APP-INTX-ABN ABNORMAL PROCEDURES
ENG RELIGHT IN FLIGHT in case of SAC/DAC intermix......................................................................................A
ENG RELIGHT IN FLIGHT in case of SAC-TI intermix..........................................................................................B
APP-INTX-NORM NORMAL PROCEDURES
Takeoff Procedure................................................................................................................................................... A
APP-HAO HIGH ALTITUDE AIRPORTS OPERATIONS
APP-HAO-GEN GENERAL
General.....................................................................................................................................................................A
APP-HAO-LIM LIMITATIONS
Environmental Envelope..........................................................................................................................................A
APP-HAO-NORM NORMAL PROCEDURES
Normal Procedures..................................................................................................................................................A
APP-HAO-PERF PERFORMANCE
Performance.............................................................................................................................................................A
APP-TAWS TAWS-GPWS
General.....................................................................................................................................................................A
Limitations................................................................................................................................................................ B
Normal Procedures..................................................................................................................................................C
APP-NRWY NARROW RUNWAY
General.....................................................................................................................................................................A
Limitations................................................................................................................................................................ B
Procedures...............................................................................................................................................................C
Performance.............................................................................................................................................................D
APP-PFC OPERATIONS ON WET GROOVED/PFC RUNWAYS
General.....................................................................................................................................................................A
Performance.............................................................................................................................................................B
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
GLG A319-112 FLEET APP-NOI P 1/6
AFM A 25 JAN 11
GENERAL
Ident.: APP-NOI-00007036.0002001 / 23 NOV 09 APPROVED
Criteria: (321-111 or 321-112 or 321-131 or 321-231 or 321-232 or A318 or A319 or A320)
NOISE CHARACTERISTICS
No determination has been made by the EASA that the noise levels of this aircraft are or should be
acceptable for operation at, into, or out of, any airport.
NOISE LEVELS
Noise levels shown in this supplement comply with EASA CS-36, JAR 36, 14 CFR (FAR) Part 36
Stage 4, and ICAO Annex 16 Chapter 4, noise requirements and were obtained by analysis of
approved data from approved noise tests.
Identification of the maximum takeoff and landing weights applicable to a particular aircraft is
provided in the LIMITATIONS chapter of this AFM (Refer to LIM-WGHT Weight Limitations).
NOISE CERTIFICATION PROCEDURES
Compliance with EASA CS-36, JAR 36, 14 CFR (FAR) Part 36, and ICAO Annex 16 included the
following procedures:
‐ An all-engine takeoff configuration 1 + F was used with a constant climb speed equal to the
all-engine operating speed at 35 ft, which is at least V2 + 10 kt and not greater than V2 + 20 kt,
with a thrust cutback procedure initiated prior to over-flight of the flyover noise control point, with
APU off, air conditioning system off, mid center of gravity, and landing gear retracted.
‐ Landing approach on a 3 ° glide slope, at a speed of VREF + 10 kt, was used with APU on,
air conditioning system on, forward center of gravity, landing gear extended and configuration
FULL.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
GLG A319-112 FLEET APP-NOI P 2/6
AFM B → 25 JAN 11
EXTERNAL NOISE
Ident.: APP-NOI-00006882.0045001 / 23 NOV 09 APPROVED
Criteria: (319-112 and (25800 and 27772))
CONFIGURATION
Engines: CFM 56-5 B6/P or CFM 56-5 B6/3 - 23 500 lb ideal sea level static thrust.
Model: A319-112
Nacelle treatment: Basic configuration including inlet and fan duct treatments.
CERTIFICATED NOISE LEVELS
EASA CS-36, ICAO Annex 16 Chapter 4, JAR-36 and 14 CFR (FAR) Part 36 Stage 4 certificated
noise levels are determined by entering these graphs at the maximum weights defined in the
LIMITATIONS chapter of this AFM. Refer to LIM-WGHT Weight Limitations.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
GLG A319-112 FLEET APP-NOI P 3/6
AFM ← B → 25 JAN 11
Flyover Noise Levels
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
GLG A319-112 FLEET APP-NOI P 4/6
AFM ← B → 25 JAN 11
Lateral Noise Levels
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
GLG A319-112 FLEET APP-NOI P 5/6
AFM ← B 25 JAN 11
Approach Noise Levels
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
Intentionally left blank
GLG A319-112 FLEET APP-NOI P 6/6
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
GLG A319-112 FLEET APP-TCAS P 1/2
AFM A to B 12 JAN 17
GENERAL
Ident.: APP-TCAS-00007060.0005001 / 02 DEC 13 APPROVED
Criteria: ((SA and (150842 or 152353 or 153870 or 39146)) or (SA and 152830))
This supplement is applicable to operations with the TCAS.
TCAS Traffic Advisory and Resolution Advisory modes can be used without any restriction when
operating within the certified limits of the aircraft flight envelope.
The TCAS complies with TCAS II change 7.1 Minimum Operational Performance Standards
(DO-185B MOPS).
Unless amended in this supplement, all the chapters of this AFM remain applicable.
PROCEDURES
Ident.: APP-TCAS-00007062.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and (26877 or 27698 or 27740 or 27753 or 28738 or 28739 or 30163))
For normal TCAS operation, select :
‐ Transponder : ON or AUTO
‐ ALT report : ON
‐ TCAS : TA/RA
Select TA for :
‐ Dispatch with landing gear down
‐ Engine failure
‐ Operation near closely spaced parallel runway (less than 1 200 ft)
Maneuvers must not be based solely on information presented on the traffic display.
Compliance with a TCAS II Resolution Advisory (RA) is always required unless the pilot considers it
unsafe to do so. Compliance with a RA is required even if there is a conflict between the RA and an
Air Traffic Control (ATC) instruction to maneuver.
Go around procedure must be performed when a RA "Climb" or "Increase Climb" is triggered on final
approach.
CAUTION Once an RA has been issued, safe separation could be compromised if current
vertical speed is changed, except as necessary to comply with the RA. This is
because TCAS II-to-TCAS II coordination may be in progress with the intruder
aircraft, and any change in vertical speed that does not comply with the RA may
negate the effectiveness of the other aircraft's compliance with the RA.
Note: Following a TCAS II "clear of conflict" advisory, the pilot should expeditiously return to the
applicable ATC clearance unless otherwise directed by ATC.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
Intentionally left blank
GLG A319-112 FLEET APP-TCAS P 2/2
AFM 12 JAN 17
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
GLG A319-112 FLEET APP-INOP P 1/4
AFM A 25 JAN 11
GENERAL
Ident.: APP-INOP-00006946.0001001 / 23 NOV 09 APPROVED
Criteria: SA
This supplement is applicable to dispatch the aircraft with inoperative items affecting the certified
AFM performance.
The provision of performance data in this supplement does not constitute authorization to operate the
aircraft with the specified items inoperative.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
GLG A319-112 FLEET APP-INOP P 2/4
AFM B → 25 JAN 11
PERFORMANCE
Ident.: APP-INOP-00007064.0002001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 318-121 or 318-122 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or
320-212 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
For takeoff, en route net flight path and landing performance determination the Performance
Engineer's Program / AFM_OCTO approved FM module at the latest approved revision must be
used. Refer to PERF-OCTO Performance Database.
Select the relevant failure case in the SPECIAL CASES field of the input data for AFM performance
calculation.
The following table summarizes all the permitted dispatch cases and gives the affected AFM
performance:
Dispatch Case Affected Performance
One pair of spoilers inoperative in the retracted
position ‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
Note: In case only spoilers 5 are inop.
on each wing, the effect on ASD,
decision speed and landing distance
is negligible.
Two pairs (surfaces 1 and 2) of spoilers
inoperative in the retracted position ‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
ATA 27
All ground spoilers control system inoperative ‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
ATA 30
One or more engine de-icing valve in open
position ‐ Takeoff Distance (TOD)
‐ Takeoff Run (TOR)
‐ Accelerate Stop Distance (ASD)
‐ First and second segments
‐ Takeoff flight path
‐ Final takeoff gradient
‐ En route net flight path
‐ Approach and landing climb
ATA 32
One brake inoperative ‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
GLG A319-112 FLEET APP-INOP P 3/4
AFM ← B 25 JAN 11
Continued from the previous page
Dispatch Case Affected Performance
ATA 70
Ground idle system inoperative ‐ Accelerate Stop Distance (ASD)
‐ Landing distance
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
Intentionally left blank
GLG A319-112 FLEET APP-INOP P 4/4
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
GENERAL
GLG A319-112 FLEET APP-LGDN-GEN P 1/2
AFM A 25 JAN 11
GENERAL
Ident.: APP-LGDN-GEN-00007074.0001001 / 23 NOV 09 APPROVED
Criteria: SA
This supplement is applicable to dispatch a revenue flight with the landing gear down and the landing
gear doors closed.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
GENERAL
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-GEN P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
LIMITATIONS
GLG A319-112 FLEET APP-LGDN-LIM P 1/2
AFM A 25 JAN 11
LIMITATIONS
Ident.: APP-LGDN-LIM-00007075.0002001 / 23 NOV 09 APPROVED
Criteria: ((A320 and 28160) or (A318 or A319 or A321))
VMO/MMO : 235 kt/M 0.6
Flight in forecasted icing conditions is not permitted.
Ditching has not been demonstrated.
Managed vertical modes CLB and DES must not be used.
Managed speed (except in approach) must not be used.
The FMS fuel predictions must be disregarded.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-LIM P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
EMERGENCY PROCEDURES
GLG A319-112 FLEET APP-LGDN-EMER P 1/2
AFM A 25 JAN 11
ENG DUAL FAILURE
Ident.: APP-LGDN-EMER-00007079.0006001 / 23 NOV 09 APPROVED
Criteria: (((320-214 or 320-215 or 320-216) and 28160) or (319-111 or 319-112 or 319-115 or 321-111 or 321-112 or 321-211 or 321-212 or
321-213))
If APU running:
Perform an assisted relight
If APU not running:
Attempt an APU start
If unsuccessful:
Accelerate to 300 kt to attempt a windmill relight. In that case, disregard VMO warning.
Flight controls are in direct law: Use "man pitch trim" as necessary.
In approach:
Set CONF 1 above or at 200 kt.
Do not select flaps/slats below 200 kt.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
EMERGENCY PROCEDURES
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-EMER P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
ABNORMAL PROCEDURES
GLG A319-112 FLEET APP-LGDN-ABN P 1/2
AFM A 25 JAN 11
F/CTL FLIGHT CONTROLS FAILURE
Ident.: APP-LGDN-ABN-00007078.0001001 / 23 NOV 09 APPROVED
Criteria: SA
A flight control failure case normally leading to ALTN LAW will lead to DIRECT LAW.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
ABNORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-ABN P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
NORMAL PROCEDURES
GLG A319-112 FLEET APP-LGDN-NORM P 1/2
AFM A 25 JAN 11
PREFLIGHT CHECK
Ident.: APP-LGDN-NORM-00007076.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The L/G DOWN VMO/MMO switch located in the avionic bay on 188VU must be set on L/G DOWN
position.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-NORM P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
PERFORMANCE
GLG A319-112 FLEET APP-LGDN-PERF P 1/2
AFM A 25 JAN 11
PERFORMANCE
Ident.: APP-LGDN-PERF-00007354.0002001 / 23 NOV 09 APPROVED
Criteria: SA
For takeoff, en route net flight path and go-around performance determination the Performance
Engineer's Programs/AFM_OCTO approved FM module at the latest approved revision given must
be used. Refer to PERF-OCTO Performance Database.
Select the LANDING GEARS EXTENDED case in the SPECIAL CASES field of the input data for
AFM performance calculation.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-PERF P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
APPENDICES AND SUPPLEMENTS
GLG A319-112 FLEET APP-LGDN-APP P 1/2
AFM A 25 JAN 11
APPENDICES AND SUPPLEMENTS
Ident.: APP-LGDN-APP-00009236.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The combination with the following supplement is not allowed:
‐ Extended Operations ETOPS (if applicable)
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
APPENDICES AND SUPPLEMENTS
Intentionally left blank
GLG A319-112 FLEET APP-LGDN-APP P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
GENERAL
GLG A319-112 FLEET APP-INTX-GEN P 1/2
AFM A 25 JAN 11
GENERAL
Ident.: APP-INTX-GEN-00007085.0007001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
This supplement is applicable to dispatch the aircraft in intermix configuration.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
GENERAL
Intentionally left blank
GLG A319-112 FLEET APP-INTX-GEN P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
LIMITATIONS
GLG A319-112 FLEET APP-INTX-LIM P 1/2
AFM A 25 JAN 11
LIMITATIONS
Ident.: APP-INTX-LIM-00009744.0006001 / 03 AUG 10 APPROVED
Criteria: 319-112
MAIN ENGINES
Any combination of two engines among the following engine types may be installed:
‐ CFM 56-5B6/P
‐ CFM 56-5B6/3
‐ CFM 56-5B6/2P
‐ CFM 56-5B6/P with "TI HPC Kit".
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET APP-INTX-LIM P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
ABNORMAL PROCEDURES
GLG A319-112 FLEET APP-INTX-ABN P 1/2
AFM A 14 DEC 13
ENG RELIGHT IN FLIGHT IN CASE OF SAC/DAC INTERMIX
Ident.: APP-INTX-ABN-00007089.0001001 / 02 DEC 13 APPROVED
Criteria: (319-112 or 320-214 or 321-111 or 321-211 or 321-212)
The DAC engine relight envelope is more restrictive than the SAC engine or SAC-TI relight
envelope. Therefore, in the case of an engine intermix, the flight crew must use the DAC engine
relight envelope below:
In Flight Engine Relight Envelope
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
ABNORMAL PROCEDURES
GLG A319-112 FLEET APP-INTX-ABN P 2/2
AFM B 14 DEC 13
ENG RELIGHT IN FLIGHT IN CASE OF SAC-TI INTERMIX
Ident.: APP-INTX-ABN-00009652.0001001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
For SAC-TI engine, the maximum altitude for the engine relight envelope is reduced, compared to
the SAC engine. Therefore, in the case of an engine intermix, the flight crew must use the following
engine relight envelope:
In Flight Engine Relight Envelope
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
NORMAL PROCEDURES
GLG A319-112 FLEET APP-INTX-NORM P 1/2
AFM A 25 JAN 11
TAKEOFF PROCEDURE
Ident.: APP-INTX-NORM-00007088.0002001 / 23 NOV 09 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or 321-211 or
321-212 or 321-213)
If takeoff is performed in engine intermix configuration, It is mandatory to wait for a stabilized 50 % of
N1 on both engines with brakes on before selecting FLX/TOGA.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET APP-INTX-NORM P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
GENERAL
GLG A319-112 FLEET APP-HAO-GEN P 1/2
AFM A 22 SEP 15
GENERAL
Ident.: APP-HAO-GEN-00007111.0001001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or 320-232 or 320-233 or
321-200) and (25615 or 34540))
This supplement is applicable to operate the aircraft to and from airports with a pressure altitude
above 9 200 ft.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
GENERAL
Intentionally left blank
GLG A319-112 FLEET APP-HAO-GEN P 2/2
AFM 22 SEP 15
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
LIMITATIONS
GLG A319-112 FLEET APP-HAO-LIM P 1/2
AFM A 12 SEP 17
ENVIRONMENTAL ENVELOPE
Ident.: APP-HAO-LIM-00007112.0093001 / 11 AUG 17 APPROVED
Criteria: ((319-111 or 319-112) and (25615 and 30748))
The environmental envelope is modified as shown herebelow to extend the TO and LDG limit to the
pressure altitude of 14 100 ft.
ENVIRONMENTAL ENVELOPE
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET APP-HAO-LIM P 2/2
AFM 12 SEP 17
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
NORMAL PROCEDURES
GLG A319-112 FLEET APP-HAO-NORM P 1/2
AFM A 22 SEP 15
NORMAL PROCEDURES
Ident.: APP-HAO-NORM-00007122.0006001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or 320-215 or 320-216 or
320-232 or 320-233 or 321-200) and 25615)
In cruise toward airport at or above 9 200 ft:
If CAB ALT unduly increases beyond 8 000 ft:
Manually set landing elevation to 8 000 ft.
At top of descent:
Set HlGH ALT LDG to ON.
Set landing elevation to AUTO.
For approach and landing:
If performance requires:
Approach can be performed with:
‐ both packs supplied by APU below 17 000 ft or
‐ one single pack supplied by APU bleed below 20 000 ft
On ground operation:
Keep HlGH ALT LDG set to ON for all ground operations.
For takeoff:
If performance requires:
Takeoff can be performed with:
‐ both packs supplied by APU up to 17 000 ft or
‐ one single pack supplied by APU bleed up to 20 000 ft
At top of climb:
When cabin altitude is below 12 000 ft and decreasing:
Set HlGH ALT LDG to OFF.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET APP-HAO-NORM P 2/2
AFM 22 SEP 15
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
PERFORMANCE
GLG A319-112 FLEET APP-HAO-PERF P 1/2
AFM A 22 SEP 15
PERFORMANCE
Ident.: APP-HAO-PERF-00007129.0002001 / 23 NOV 09 APPROVED
Criteria: ((318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 319-131 or 319-132 or 319-133 or 320-214 or 320-215 or 320-216 or
320-232 or 320-233 or 321-200) and 25615)
The performance data given in performance and supplementary performance chapters of this AFM
remain applicable for takeoff and landing up to 14 100 ft.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET APP-HAO-PERF P 2/2
AFM 22 SEP 15
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
TAWS-GPWS
GLG A319-112 FLEET APP-TAWS P 1/2
AFM A to C → 16 MAR 15
GENERAL
Ident.: APP-TAWS-00007228.0001001 / 14 JAN 15 APPROVED
Criteria: (SA and (26526 or 28244 or 34637 or 39146))
This supplement is applicable to aircraft fitted with Terrain Awareness Warning System (TAWS)
T2CAS, or with TAWS T3CAS, or with Enhanced Ground Proximity Warning System (EGPWS).
A list of areas where no terrain data are available along the scheduled route should be made
available to the flight crew.
Approval of TAWS predictive functions of T2CAS or T3CAS, or of EGPWS enhanced function is
based on the assumption that TAWS databases (excluding Performance database) are compliant
with DO-200A DPAL2.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
LIMITATIONS
Ident.: APP-TAWS-00007229.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and (26526 or 28244))
Aircraft navigation is not to be predicated upon the use of the terrain display.
The terrain display is intended to serve as a situation awareness tool only, and may not provide the
accuracy on which to solely base terrain avoidance maneuvering.
The EGPWS database, display, and alerting algorithms currently do not account for man made
obstructions.
The EGPWS enhanced function should be inhibited (TERR pushbutton set to OFF on GPWS panel)
when the aircraft position is less than 15 NM from the airfield:
‐ For operations from/to runways not incorporated into the EGPWS database
‐ For specific approach procedures which have previously been identified as potentially producing
false terrain alerts.
NORMAL PROCEDURES
Ident.: APP-TAWS-00007231.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 28244)
The following procedures replace the GPWS procedures published in the NORMAL PROCEDURES
chapter of this AFM.
When a warning occurs:
Pull up using full back stick.
Apply takeoff thrust and climb until the warning ceases.
For enhanced function, in addition to climbing, a turning maneuver can be initiated after verifying
the aircraft position and if the crew concludes turning is the safest way of action.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
TAWS-GPWS
GLG A319-112 FLEET APP-TAWS P 2/2
AFM ← C 16 MAR 15
Note: The EGPWS does not take account of specific aircraft configuration and climb
performance and a "pull up" maneuver on its own, for certain situations, may not ensure
terrain clearance.
Warnings may be considered cautionary during daylight VMC conditions provided the cause of
the warning can be identified immediately.
When a caution occurs:
Adjust the flight path/configuration so that the caution alert ceases.
Climb and/or turn as necessary based on analysis of all available instruments and information.
During climb, descent, approach and go-around, when the FMS navigation accuracy check prevents
the crew from using NAV mode in a phase of flight, the EGPWS enhanced function must be switched
OFF through the TERR pushbutton located on the GPWS panel.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
NARROW RUNWAY
GLG A319-112 FLEET APP-NRWY P 1/2
AFM A to C 08 AUG 17
GENERAL
Ident.: APP-NRWY-00006985.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 30397)
This supplement is applicable to operations on runways with a width below 45 m.
This supplement does not constitute an operational approval. Such authorization must be obtained
by the operator from the appropriate authorities.
Unless amended in this supplement, all the chapters of this AFM remain applicable.
LIMITATIONS
Ident.: APP-NRWY-00006987.0001001 / 23 NOV 09 APPROVED
Criteria: (SA and 30397)
Minimum runway width: 30 m
Systems:
The dispatch from/to narrow runways is not allowed in case of:
‐ nosewheel steering inoperative
‐ one brake or more inoperative.
Autoland is not allowed.
PROCEDURES
Ident.: APP-NRWY-00007014.0001001 / 03 AUG 17 APPROVED
Criteria: ((A319 or A320 or A321) and 30397)
Diversion to a 45 m wide runway is recommended in case of:
‐ Rudder jam
‐ Rudder pedal jam
‐ Yaw damper fault
‐ Rudder Travel Limit system fault
‐ All failures leading to the loss of the nosewheel steering (HYD Green system loss, double
hydraulic failure, double BSCU fault, double LGCIU fault).
The following applies to narrow runways in terms of crosswind component:
‐ Maximum demonstrated crosswind for dry runways: 38 kt (gust included) for takeoff and landing
‐ Maximum demonstrated crosswind for wet runways: 33 kt (gust included) for takeoff and landing
‐ Maximum crosswind for contaminated runways: 10 kt (gust included) for takeoff and landing.
Operations on icy runways have not been demonstrated.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
NARROW RUNWAY
GLG A319-112 FLEET APP-NRWY P 2/2
AFM D 08 AUG 17
PERFORMANCE
Ident.: APP-NRWY-00006986.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and 30397)
For performance determination, the Performance Engineer's Programs AFM_OCTO approved FM
module at the latest approved revision must be used.
Refer to PERF-OCTO Performance Database.
Enter the runway width in the RUNWAY WIDTH field of the input data for AFM performance
calculation.
For runways with a width below 40 m, the VMCG must be increased by:
Runway width 30 m 35 m 40 m
ΔVMCG (kt) + 2.5 + 1.5 + 0
and linear interpolation in between.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
OPERATIONS ON WET GROOVED/PFC RUNWAYS
GLG A319-112 FLEET APP-PFC P 1/2
AFM A to B 25 JAN 11
GENERAL
Ident.: APP-PFC-00007028.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
The nominal runway surface for performance calculation on wet runway is smooth.
The takeoff performance improvements on wet grooved or Porous Friction Course (PFC) runways
are covered by modification 35075.
The landing performance improvements on wet grooved/PFC runways are covered by modification
37457.
PERFORMANCE
Ident.: APP-PFC-00007029.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
The takeoff performance (Accelerate Stop Distance, Complete Takeoff) on wet grooved/PFC runway
given in the approved databases of the PERFORMANCE chapter must not be used for aircraft not
fitted with modification 35075.
The landing performance (Landing Distance) on wet grooved/PFC runway given in the approved
databases of the PERFORMANCE chapter must not be used for aircraft not fitted with modification
37457.
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
OPERATIONS ON WET GROOVED/PFC RUNWAYS
Intentionally left blank
GLG A319-112 FLEET APP-PFC P 2/2
AFM 25 JAN 11
MASTER CONFIGURATION
DEVIATION LIST
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 1/8
AFM 12 DEC 17
MCDL-GEN GENERAL
MCDL-GEN-INTR Introduction
Introduction...............................................................................................................................................................A
MCDL-GEN-LIM Limitations
Limitations................................................................................................................................................................ A
MCDL-GEN-PERF Performance
Performance Determination Method........................................................................................................................A
Performance Penalties published in the Airplane Flight Manual MCDL Chapter....................................................B
Performance Penalties calculated with AFM_OCTO Software............................................................................... C
MCDL-21 AIR CONDITIONING
MCDL-21-01 Ram Air Inlet Flap
Ram Air Inlet Flap................................................................................................................................................... A
Illustration Ram Air Inlet Flap..................................................................................................................................B
MCDL-21-03 Ram Air Inlet Leading Edge
Ram Air Inlet Leading Edge....................................................................................................................................A
Illustration Ram Air Inlet Leading Edge.................................................................................................................. B
MCDL-23 COMMUNICATION
MCDL-23-01 Static Discharger
Static Discharger......................................................................................................................................................A
Illustration Static Discharger....................................................................................................................................B
MCDL-27 FLIGHT CONTROL
MCDL-27-01 Flap Track Fairing
Flap Track Fairing....................................................................................................................................................A
Illustration Flap track fairing.................................................................................................................................... B
MCDL-27-03 Slat Track Closing Plate
Slat Track Closing Plate..........................................................................................................................................A
Illustration Slat track closing plate...........................................................................................................................B
MCDL-27-05 Access Panel for Bearings at Elevator
Access Panel for Bearings at Elevator................................................................................................................... A
Illustration Access panel for bearings at elevator................................................................................................... B
MCDL-27-06 Flap Track Fairing Rear Top Cover and Tail Cone
Flap Track Fairing Rear Top Cover and Tail Cone................................................................................................ A
Illustration Flap track fairing rear top cover and tail cone.......................................................................................B
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 2/8
AFM 12 DEC 17
Continued from the previous page
MCDL-27-07 Rubber Seal under Slat
Rubber Seal under Slat...........................................................................................................................................A
Illustration Rubber seal under slat.......................................................................................................................... B
MCDL-27-08 Seal Between Inboard and Outboard Flap
Seal Between Inboard and Outboard Flap..............................................................................................................A
Illustration Seal Between Inboard and Outboard Flap............................................................................................ B
MCDL-27-09 Inboard Aileron Edge to Wing Seal
Inboard Aileron Edge to Wing Seal.........................................................................................................................A
Illustration Inboard Aileron to Wing Seal.................................................................................................................B
MCDL-27-10 Slat End Seal and Weather Seal
Slat End Seal and Weather Seal............................................................................................................................ A
Illustration Slat End Seal and Weather Seal...........................................................................................................B
MCDL-27-11 Slat Track Filler Block
Slat Track Filler Block............................................................................................................................................. A
Illustration Slat track filler block...............................................................................................................................B
MCDL-27-12 Slat Track Sealing Packer
Slat Track Sealing Packer.......................................................................................................................................A
Illustration Slat track sealing packer....................................................................................................................... B
MCDL-27-13 Inter-flap Cushion Seal
Inter-flap Cushion Seal............................................................................................................................................A
Illustration Inter-flap cushion seal............................................................................................................................B
MCDL-27-14 Flap Track Moveable Fairing Seal
Flap Track Moveable Fairing Seal.......................................................................................................................... A
Illustration Moveable flap track fairing seal............................................................................................................. B
MCDL-27-15 Flap Track Fixed Fairing Seal
Flap Track Fixed Fairing seal..................................................................................................................................A
Illustration Fixed flap track fairing seal....................................................................................................................B
MCDL-27-16 Flap Track Moveable Fairing Pivot Cover
Flap Track Moveable Fairing Pivot Cover...............................................................................................................A
Illustration Flap Track Moveable Fairing Pivot Cover............................................................................................. B
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 3/8
AFM 12 DEC 17
Continued from the previous page
MCDL-28 FUEL
MCDL-28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM
Refuel/Defuel Coupling Cap 101 QM Or 41 QM.................................................................................................... A
Illustration Refuel/Defuel Coupling Cap 101 QM or 41 QM....................................................................................B
MCDL-28-02 Refuel Panel Door 192MB
Refuel Panel Door ..................................................................................................................................................A
Illustration Refuel Panel Door 192MB..................................................................................................................... B
MCDL-30 ICE AND RAIN PROTECTION
MCDL-30-01 Icing Indicator
Icing Indicator...........................................................................................................................................................A
Illustration Icing Indicator.........................................................................................................................................B
MCDL-32 LANDING GEAR
MCDL-32-03 Nose Wheel Hubcap
Nose Wheel Hubcap................................................................................................................................................A
Illustration Nose Wheel Hubcap..............................................................................................................................B
MCDL-32-04 Nose Fitting Towing
Nose Fitting Towing.................................................................................................................................................A
Illustration Nose Fitting Towing............................................................................................................................... B
MCDL-33 LIGHTS
MCDL-33-01 Wing/Engine Scan light Cover 3LX, 4LX
Wing/Engine Scan Light Cover 3LX, 4LX............................................................................................................... A
Illustration Wing/Engine Scan light Cover 3LX, 4LX...............................................................................................B
MCDL-33-02 Taxi Light Lamp 8LR
Taxi Light Lamp 8LR...............................................................................................................................................A
Illustration Taxi Light Lamp 8LR............................................................................................................................. B
MCDL-33-03 Rear Navigation Light Lens 15LA
Rear Navigation Light Lens 15LA........................................................................................................................... A
Illustration Rear Navigation Light Lens 15LA..........................................................................................................B
MCDL-33-04 Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light Cover
Upper 7LV and Lower 6LV Anti-collision (Beacon) Light Cover............................................................................. A
Illustration Upper and Lower Anti-Collision ( Beacon) Light Cover.........................................................................B
Continued on the following page
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GLG A319-112 FLEET MCDL-PLP-TOC P 4/8
AFM 12 DEC 17
Continued from the previous page
MCDL-33-05 Logo Light Lens (Cover) 3LY, 4LY
Logo Light Lens (Cover) 3LY, 4LY ........................................................................................................................A
Illustration Logo Light Lens (Cover) 3LY, 4LY........................................................................................................ B
MCDL-33-07 Landing Light Lens 7LB, 8LB
Landing Light Lens 7LB, 8LB..................................................................................................................................A
Illustration Landing Light Lens 7LB, 8LB................................................................................................................ B
MCDL-33-08 Turn OFF Light Lamp 3LC1, 3LC2
Turn OFF Light Lamp 3LC1, 3LC2......................................................................................................................... A
Illustration Turn OFF Light Lamp 3LC1, 3LC2........................................................................................................B
MCDL-33-09 Takeoff Light Lamp 7LR
Takeoff light lamp 7LR............................................................................................................................................ A
Illustration Takeoff Light Lamp 7LR........................................................................................................................ B
MCDL-49 APU
MCDL-49-01 APU Overpressure Release Door
APU Overpressure Release Door........................................................................................................................... A
Illustration APU Overpressure Release Door..........................................................................................................B
MCDL-51 STRUCTURE
MCDL-51-02 Passenger Door Scuff Plate
Passenger Door Scuff Plate....................................................................................................................................A
Illustration Passenger Door Scuff Plate.................................................................................................................. B
MCDL-51-04 Fairing Aft Safety Stay Point 311 AL
Fairing Aft Safety Stay Point 311 AL...................................................................................................................... A
Illustration Fairing Aft Safety Stay Point 311AL...................................................................................................... B
MCDL-52 DOORS
MCDL-52-01 Toilet Servicing and Drainage Door
Toilet Servicing and Drainage Door 172 AR...........................................................................................................A
Illustration Toilet Servicing and Drainage Door ..................................................................................................... B
MCDL-52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB
Access Door To Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB.......................................................... A
Illustration Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB...........................................B
Continued on the following page
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PRELIMINARY PAGES
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GLG A319-112 FLEET MCDL-PLP-TOC P 5/8
AFM 12 DEC 17
Continued from the previous page
MCDL-52-03 Access Door to Potable Water Filling and Drainage
Access Door To Potable Water Filling And Drainage 133 AL - 171 AL..................................................................A
Access Door To Potable Water Filling And Drainage 133 AL - 171 AL - 192 NB...................................................B
Illustration Access Door to Potable Water Filling and Drainage............................................................................. C
Illustration Access Door to Potable Water Filling and Drainage............................................................................. D
MCDL-52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB
Access Door To Opening Control Of Landing Gear Doors On Ground 195 BB - 196 BB...................................... A
Illustration Access door to opening control of landing gear doors on ground 195 BB - 196 BB..............................B
MCDL-52-05 Access Door to Air Conditioning Ground Supply 191 CB
Access Door To Air Conditioning Ground Supply 191 CB......................................................................................A
Illustration Access door to air conditionning ground supply 191 CB.......................................................................B
MCDL-52-07 External Power Ground Connection Access Door Assy 121 AL
External Power Ground Connection Access Door Assy 121 AL.............................................................................A
Illustration External Power Ground Connection Access Door Assy 121 AL........................................................... B
MCDL-52-08 Access Door of Cargo Opening System 134 AR - 154 AR
Access Door Of Cargo Opening System 134 AR - 154 AR................................................................................... A
Illustration Access Door of Cargo Opening System 134 AR - 154 AR................................................................... B
MCDL-52-09 Nose Landing Gear Main Door (713, 714)
Nose Landing Gear Main Door (713, 714)............................................................................................................. A
Illustration Nose Landing Gear Main Door (713, 714)............................................................................................ B
MCDL-52-10 Nose Landing Gear Aft Door (715, 716)
Nose Landing Gear Aft Door (715, 716).................................................................................................................A
Illustration Nose Landing Gear Aft Door (715, 716)............................................................................................... B
MCDL-52-11 Nose Landing Gear Leg Door (712)
Nose Landing Gear Leg Door (712)....................................................................................................................... A
Illustration Nose Landing Gear Leg Door (712)...................................................................................................... B
MCDL-52-12 Main Landing Gear Door (732, 742) (flight with gear up)
Main Landing Gear Door (732, 742) (flight with gear up).......................................................................................A
Illustration Main Landing Gear Door (732, 742)......................................................................................................B
MCDL-52-13 Main Landing Gear Door (733, 743) (flight with gear up)
Main Landing Gear Door (733, 743) (flight with gear up).......................................................................................A
Illustration Main Landing Gear Door (733, 743)......................................................................................................B
Continued on the following page
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PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 6/8
AFM 12 DEC 17
Continued from the previous page
MCDL-52-14 Main Landing Gear Door (732, 742) (flight with gear down)
Main Landing Gear Door (732, 742) (Flight with gear down)................................................................................. A
Illustration Main Landing Gear Door (732, 742)......................................................................................................B
MCDL-52-15 Main Landing Gear Door (733, 743) (Flight with gear down)
Main Landing Gear Door (733, 743) (Flight with gear down)................................................................................. A
Illustration Main Landing Gear Door (733, 743)......................................................................................................B
MCDL-52-16 Main Landing Gear Door (734, 744) (Flight with gear down)
Main Landing Gear Door (734, 744) (Flight with gear down)................................................................................. A
Illustration Main Landing Gear Door (734, 744)......................................................................................................B
MCDL-52-18 Main Landing Gear Door : Seal on Secondary Hinged Fairing
Main Landing Gear Door : Seal On Secondary Hinged Fairing..............................................................................A
Illustration Main Landing Gear Door : Seal on Secondary Hinged Fairing............................................................. B
MCDL-52-19 Pax Door Upper Cover Plate
Pax Door Upper Cover Plate.................................................................................................................................. A
Illustration Pax Door Upper Cover Plate.................................................................................................................B
MCDL-52-20 Access Door to HP Air Ground Connector 191 DB
Access Door To HP Air Ground Connector 191 DB...............................................................................................A
Illustration Access Door to HP Air Ground Connector 191 DB...............................................................................B
MCDL-52-21 Blue Hydraulic Access Door 197 FB
Blue Hydraulic Access Door 197 FB.......................................................................................................................A
Illustration Blue Hydraulic Access Door 197 FB..................................................................................................... B
MCDL-52-22 Forward Cargo Door Access Cover Panel 825 AR
Forward Cargo Door Access Cover Panel 825 AR................................................................................................ A
Illustration Forward Cargo Door Access Cover Panel 825 AR............................................................................... B
MCDL-52-23 Aft Cargo Door Access Cover Panel 826 AR
Aft Cargo Door Access Cover Panel 826 AR......................................................................................................... A
Illustration Aft Cargo Door Access Cover Panel 826 AR........................................................................................B
MCDL-53 FUSELAGE
MCDL-53-01 Belly Fairing Vent Louver Vane
Belly Fairing Vent Louver Vane.............................................................................................................................. A
Illustration Belly Fairing Vent Louver Vane............................................................................................................. B
Continued on the following page
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PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 7/8
AFM 12 DEC 17
Continued from the previous page
MCDL-53-03 Root Fillet Fairing
Root Fillet Fairing.................................................................................................................................................... A
Illustration Root Fillet Fairing...................................................................................................................................B
MCDL-54 NACELLE / PYLON
MCDL-54-01 Nacelle Strake
Nacelle Strake..........................................................................................................................................................A
Illustration Nacelle Strake........................................................................................................................................B
MCDL-54-03 Pylon Pressure Relief Door 413(423) BL - 414(424) BR
Pylon Pressure Relief Door 413(423) BL - 414(424) BR........................................................................................A
Illustration Pylon Pressure Relief Door 413(423) BL - 414(424) BR.......................................................................B
MCDL-54-04 Pylon Access Door 415(425) AL - 415(425) AR
Pylon Access Door 415(425) AL - 415(425) AR.....................................................................................................A
Illustration Pylon Access Door 415(425) AL - 415(425) AR....................................................................................B
MCDL-54-05 Pylon Fairing Seal
Pylon Fairing Seal................................................................................................................................................... A
Pylon Fairing seal....................................................................................................................................................B
Illustration Pylon Fairing Seal..................................................................................................................................C
Illustration Pylon Fairing Seal..................................................................................................................................D
MCDL-54-06 Aerodynamic Seal
Aerodynamic Seal....................................................................................................................................................A
Illustration Aerodynamic Seal.................................................................................................................................. B
MCDL-57 WINGS
MCDL-57-01 Wing Tip Fence
Wing Tip Fence....................................................................................................................................................... A
Illustration Wing Tip Fence......................................................................................................................................B
MCDL-57-02 Belly Fairing Sliding Panel
Belly Fairing Sliding Panel...................................................................................................................................... A
Illustration Belly Fairing Sliding Panel.....................................................................................................................B
MCDL-57-03 Outboard Flaps Rubbing Strip
Outboard Flap Rubbing Strip Items 10, 15, 20, 40.................................................................................................A
Illustration Outboard Flap Rubbing Strip ................................................................................................................B
Continued on the following page
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PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET MCDL-PLP-TOC P 8/8
AFM 12 DEC 17
Continued from the previous page
MCDL-57-04 Inboard Flap Rubbing Strip
Inboard Flap Rubbing Strip items 1, 5, 10, 30........................................................................................................A
Illustration Inboard Flap Rubbing Strip .................................................................................................................. B
MCDL-57-06 Outer Flap Blade Seal
Outer Flap Blade Seal.............................................................................................................................................A
Illustration Outer Flap Blade Seal........................................................................................................................... B
MCDL-71 POWER PLANT
MCDL-71-01 Frangible Drain Mast
Frangible Drain Mast............................................................................................................................................... A
Illustration Frangible Drain Mast..............................................................................................................................B
MCDL-71-09 Fan Cowl Hold Open Rod
Fan Cowl Hold Open Rod.......................................................................................................................................A
Illustration Fan Cowl Hold Open Rod..................................................................................................................... B
MCDL-78 EXHAUST
MCDL-78-01 Duct Opening Actuator
Duct Opening Actuator............................................................................................................................................ A
Illustration Duct Opening Actuator...........................................................................................................................B
MCDL-78-09 Thrust Reverser 11 and 1 O'clock Struts
Thrust Reverser 11 and 1 O'clock Struts................................................................................................................A
Illustration Thrust Reverser 11 and 1 O'clock Struts.............................................................................................. B
MCDL-78-11 Thrust Reverser Lockout Fairing
Thrust Reverser Lockout Fairing.............................................................................................................................A
Illustration of the Thrust Reverser Lockout Fairing................................................................................................. B
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PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
GLG A319-112 FLEET MCDL-PLP-SOH P 1/2
AFM 12 DEC 17
Localization
Title
Toc
Index
ID Reason
MCDL-27-01
Flap Track Fairing
A1Addition of a note to allow item combination.
MCDL-27-03
Slat Track Closing Plate
A1Addition of a note to allow item combination.
MCDL-27-08
Seal Between Inboard and Outboard
Flap
A1Addition of a note to allow item combination.
MCDL-27-16
Flap Track Moveable Fairing Pivot
Cover
A1Addition of a note to allow item combination.
MCDL-28-01
Refuel/Defuel Coupling Cap 101 QM
Or 41 QM
A1Addition of a note to allow item combination.
MCDL-28-02
Refuel Panel Door
A1Addition of a note to allow item combination.
Addition of a note to allow item combination.MCDL-33-02
Taxi Light Lamp 8LR
A1
Removal of the high speed tape content as Operator must refer to
AMM task.
Addition of a note to allow item combination.MCDL-33-07
Landing Light Lens 7LB, 8LB
A1
Removal of the high speed tape content as Operator must refer to
AMM task.
MCDL-52-05
Access Door To Air Conditioning
Ground Supply 191 CB
A1Addition of a note to allow item combination.
MCDL-52-21
Blue Hydraulic Access Door 197 FB
A1Addition of a note to allow item combination.
MCDL-57-01
Wing Tip Fence
A1Addition of a note to allow item combination.
MCDL-57-01
Wing Tip Fence
A2Addition of a note to allow item combination.
MCDL-57-02
Belly Fairing Sliding Panel
A1Addition of a note to allow item combination.
MCDL-57-06
Outer Flap Blade Seal
A1Addition of a note to allow item combination.
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PRELIMINARY PAGES
SUMMARY OF HIGHLIGHTS
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GLG A319-112 FLEET MCDL-PLP-SOH P 2/2
AFM 12 DEC 17
A319
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GENERAL
INTRODUCTION
GLG A319-112 FLEET MCDL-GEN-INTR P 1/2
AFM A 10 OCT 17
INTRODUCTION
Ident.: MCDL-GEN-INTR-00006202.0001001 / 02 OCT 17 APPROVED
Criteria: SA
Operation of the aircraft without certain secondary airframe and engine parts is possible as indicated
in this Master Configuration Deviation List. Any part not included in this list must be considered as
necessary.
It is important to repair the aircraft at the first airport where repairs or replacements may reasonably
be made, since additional malfunctions may require the airplane to be taken out of service.
Letter (m) associated to an item indicates that maintenance action is necessary to permit flight with
these parts missing.
It is the Operator's responsibility to:
‐ Define the task sharing between the flight and maintenance crews
‐ Ensure that all maintenance procedures are performed.
When items require high-speed tape, the MCDL dispatch conditions are assessed considering that
the tape is in the correct position and in good condition. The Operator must use an appropriate
process to ensure that the dispatch conditions are satisfied. The Operator must define this process in
accordance with its specific operations.
Note: Unless otherwise specified in the MCDL item or the relevant AMM task, a visual inspection
of the high-speed tape must be made at a regular interval that must not exceed 3 calendar
days.
The MCDL maintenance procedures are published in the AMM. The MCDL item number may be
used to find the associated task in the AMM via the dedicated function of AirN@v.
Note: 1. The sign “-” in “Quantity installed” column indicates that the quantity is variable.
2. The illustrations included in this Master Configuration Deviation List are given only
for information to facilitate location of missing items and must not be considered as
approved data.
3. Items numbering is used for item identification only. As a consequence it may appear
some gaps in the item numbering sequence of a given aircraft. In such a case,
completeness of the MCDL may be checked by referring to the LEDU.
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GENERAL
INTRODUCTION
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GLG A319-112 FLEET MCDL-GEN-INTR P 2/2
AFM 10 OCT 17
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GENERAL
LIMITATIONS
GLG A319-112 FLEET MCDL-GEN-LIM P 1/2
AFM A 25 JAN 11
LIMITATIONS
Ident.: MCDL-GEN-LIM-00006203.0001001 / 23 NOV 09 APPROVED
Criteria: SA
No more than one part of one system may be missing except if otherwise specified. Parts of different
systems may be simultaneously missing, unless otherwise specified in this list.
When missing part introduces additional limitation(s), this limitation is indicated in the dispatch
condition of the item of this list. This limitation comes in addition to the ones of the LIMITATIONS
chapter of this AFM. This limitation must be clearly indicated by a placard on the pilote's instrument
panel.
When an MCDL dispatch condition refers to the MMEL, the minimum number of equipment required
for dispatch is the most limiting of the two documents.
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GENERAL
LIMITATIONS
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GLG A319-112 FLEET MCDL-GEN-LIM P 2/2
AFM 25 JAN 11
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MASTER CONFIGURATION DEVIATION LIST
GENERAL
PERFORMANCE
GLG A319-112 FLEET MCDL-GEN-PERF P 1/2
AFM A to B 16 MAR 15
PERFORMANCE DETERMINATION METHOD
Ident.: MCDL-GEN-PERF-00006204.0001001 / 23 NOV 09 APPROVED
Criteria: SA
There are two approved ways of determining the performance impact of CDL items missing:
‐ Using MCDL chapter of the AFM, or
‐ Using AFM_OCTO software.
The MCDL performance penalties associated to the missing items when published in this chapter
are envelope penalties. More accurate penalties can be determined by using AFM_OCTO software.
According to the operations, operators can select the most adequate method.
If no performance data are available in AFM_OCTO for a given item listed in this MCDL chapter, the
penalties published in this MCDL chapter must be used.
PERFORMANCE PENALTIES PUBLISHED IN THE
AIRPLANE FLIGHT MANUAL MCDL CHAPTER
Ident.: MCDL-GEN-PERF-00006205.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Performance penalties are cumulative unless specific penalties for particular combinations of missing
items are indicated.
These takeoff, en route and landing penalties apply to the most limiting corresponding weight.
If performance penalties are not indicated for removed items, no more than three of such items can
be missing without taking further penalty. If more than three of such items are missing together, the
following performance penalties are applicable per additional missing item:
‐ Takeoff and approach climb performance limiting weights are reduced by 50 kg (110 lb)
‐ En route performance limiting weight is reduced by 60 kg (132 lb) (i.e. corresponding to a 60 ft
decrease of en-route net ceiling).
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GENERAL
PERFORMANCE
GLG A319-112 FLEET MCDL-GEN-PERF P 2/2
AFM C 16 MAR 15
PERFORMANCE PENALTIES CALCULATED WITH AFM_OCTO SOFTWARE
Ident.: MCDL-GEN-PERF-00006206.0001001 / 14 JAN 15 APPROVED
Criteria: SA
The takeoff, approach climb and en route performance with MCDL items missing can be determined
by selecting the missing items in the “CDL item...” menu of the AFM_OCTO interface, using the
database given in PERFORMANCE chapter (Refer to PERF-OCTO Performance Database) of
this AFM associated to the CDLA320F.cdl file at issue 1 or higher using AFM_OCTO approved FM
module at the revision 31 or higher.
Items for which no performance penalty is indicated in this MCDL chapter are referenced as
negligible items. Select the number of negligible items in the “CDL item...” menu to determine
performance impact when four or more of such items are missing.
CAUTION The most limiting performance between the one computed with items missing and
the one computed without item missing must be used.
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MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
RAM AIR INLET FLAP
GLG A319-112 FLEET MCDL-21-01 P 1/2
AFM A 25 JAN 11
21-01 Ram Air Inlet Flap
Ident.: MCDL-21-01-00006207.0002001 / 23 NOV 09 APPROVED
Criteria: (SA and ((26363 and A319) or (26363 and A320) or (26363 and A321) or A318))
21-01 Quantity installed
RAM AIR INLET FLAP 2
All may be missing.
Note: System performance in heating mode will be decreased.
•Performance:
The following performance penalties are applicable per missing flap:
‐ Takeoff and approach climb performance limiting weights are reduced by 190 kg
(418 lb)
‐ En route performance limiting weight is reduced by 216 kg (476 lb)
‐ Fuel consumption is increased by 0.53 %.
Refer to MCDL-21-01 Illustration Ram Air Inlet Flap
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MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
RAM AIR INLET FLAP
GLG A319-112 FLEET MCDL-21-01 P 2/2
AFM B 25 JAN 11
ILLUSTRATION RAM AIR INLET FLAP
Ident.: MCDL-21-01-00006213.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions: Refer to 21-01 Ram Air Inlet Flap
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
RAM AIR INLET LEADING EDGE
GLG A319-112 FLEET MCDL-21-03 P 1/2
AFM A 25 JAN 11
21-03 Ram Air Inlet Leading Edge
Ident.: MCDL-21-03-00006216.0001001 / 23 NOV 09 APPROVED
Criteria: SA
21-03 Quantity installed
RAM AIR INLET LEADING EDGE 2
One may be missing provided the associated pack is turned off (Refer to MMEL/MI-21-52 Air
Conditioning Pack).
Refer to MCDL-21-03 Illustration Ram Air Inlet Leading Edge
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
RAM AIR INLET LEADING EDGE
GLG A319-112 FLEET MCDL-21-03 P 2/2
AFM B 25 JAN 11
ILLUSTRATION RAM AIR INLET LEADING EDGE
Ident.: MCDL-21-03-00006219.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 21-03 Ram Air Inlet Leading Edge
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MASTER CONFIGURATION DEVIATION LIST
COMMUNICATION
STATIC DISCHARGER
GLG A319-112 FLEET MCDL-23-01 P 1/2
AFM A 09 JUL 14
23-01 Static Discharger
Ident.: MCDL-23-01-00006220.0001001 / 02 DEC 13 APPROVED
Criteria: SA
23-01 Quantity installed
STATIC DISCHARGER –
20 % of static dischargers may be missing or inoperative on each the following areas:
‐ RIGHT wing
‐ LEFT wing
‐ Vertical stabilizer (including rudder)
‐ RIGHT horizontal stabilizer (including elevator)
‐ LEFT horizontal stabilizer (including elevator).
Note: 1. If a static discharger is missing or inoperative on a flap track fairing, the VHF and
HF sound quality may be slightly degraded.
2. When combined with the case of dispatch with a wing tip fence missing, 20 % of
the remaining static dischargers of the affected wing are allowed to be inoperative
or missing (Refer to 57-01 Wing Tip Fence).
Refer to MCDL-23-01 Illustration Static Discharger
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MASTER CONFIGURATION DEVIATION LIST
COMMUNICATION
STATIC DISCHARGER
GLG A319-112 FLEET MCDL-23-01 P 2/2
AFM B 09 JUL 14
ILLUSTRATION STATIC DISCHARGER
Ident.: MCDL-23-01-00006221.0001001 / 12 JUN 14 FOR INFORMATION ONLY
Criteria: SA
Note: The engine pylons static dischargers may be uninstalled per Service Bulletin 23-1299. The
aircraft configuration regarding the SB 23-1299 defines the number of static dischargers
installed.
For dispatch conditions:Refer to 23-01 Static Discharger
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FAIRING
GLG A319-112 FLEET MCDL-27-01 P 1/2
AFM A 12 DEC 17
27-01 Flap Track Fairing
Ident.: MCDL-27-01-00006235.0001001 / 29 NOV 17 APPROVED
Criteria: (A319 or A320)
1
27-01 Quantity installed
FLAP TRACK FAIRING 6
(m) Refer to AMM Task 57-55-00-040-001
One fairing may be partly or completely missing.
Note: 1. When the forward part of the fairing is missing, the aft part must be removed.
2. When the aft part of the fairing is missing, the forward part may remain installed.
3. May be combined with MCDL item 27-08 (Refer to 27-08 Seal Between Inboard
and Outboard Flap).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 1 180 kg
(2 601 lb)
‐ En route performance limiting weight is reduced by 1 620 kg (3 571 lb)
‐ Fuel consumption is increased by 3.14 %.
Refer to MCDL-27-01 Illustration Flap Track Fairing
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FAIRING
GLG A319-112 FLEET MCDL-27-01 P 2/2
AFM B 12 DEC 17
ILLUSTRATION FLAP TRACK FAIRING
Ident.: MCDL-27-01-00006236.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-01 Flap Track Fairing
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK CLOSING PLATE
GLG A319-112 FLEET MCDL-27-03 P 1/2
AFM A 12 DEC 17
27-03 Slat Track Closing Plate
Ident.: MCDL-27-03-00006239.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
27-03 Quantity installed
SLAT TRACK CLOSING PLATE 24
Two may be missing.
Note: May be combined with MCDL item 27-16 (Refer to 27-16 Flap Track Moveable
Fairing Pivot Cover).
Refer to MCDL-27-03 Illustration Slat Track Closing Plate
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MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK CLOSING PLATE
GLG A319-112 FLEET MCDL-27-03 P 2/2
AFM B 12 DEC 17
ILLUSTRATION SLAT TRACK CLOSING PLATE
Ident.: MCDL-27-03-00006240.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions: Refer to 27-03 Slat Track Closing Plate
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MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
ACCESS PANEL FOR BEARINGS AT ELEVATOR
GLG A319-112 FLEET MCDL-27-05 P 1/2
AFM A 25 JAN 11
27-05 Access Panel for Bearings at Elevator
Ident.: MCDL-27-05-00006243.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-05 Quantity installed
ACCESS PANEL FOR BEARINGS AT ELEVATOR 8
Two may be missing.
Refer to MCDL-27-05 Illustration Access Panel for Bearings at Elevator
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AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
ACCESS PANEL FOR BEARINGS AT ELEVATOR
GLG A319-112 FLEET MCDL-27-05 P 2/2
AFM B 25 JAN 11
ILLUSTRATION ACCESS PANEL FOR BEARINGS AT ELEVATOR
Ident.: MCDL-27-05-00006244.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-05 Access Panel for Bearings at Elevator
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
GLG A319-112 FLEET MCDL-27-06 P 1/2
AFM A 14 DEC 13
27-06 Flap Track Fairing Rear Top Cover and Tail Cone
Ident.: MCDL-27-06-00006245.0001001 / 02 DEC 13 APPROVED
Criteria: SA
27-06 Quantity installed
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE –
(m) Refer to AMM Task 57-55-00-040-002
Both may be missing on two flap track fairings.
Note: 1. When the tail cone is missing, the rear top cover may remain installed.
2. When the rear top cover is missing, the associated tail cone must be removed.
Refer to MCDL-27-06 Illustration Flap Track Fairing Rear Top Cover and Tail Cone
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
GLG A319-112 FLEET MCDL-27-06 P 2/2
AFM B 14 DEC 13
ILLUSTRATION FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
Ident.: MCDL-27-06-00006246.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-06 Flap Track Fairing Rear Top Cover and Tail Cone
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
RUBBER SEAL UNDER SLAT
GLG A319-112 FLEET MCDL-27-07 P 1/2
AFM A 14 DEC 13
27-07 Rubber Seal under Slat
Ident.: MCDL-27-07-00006247.0001001 / 02 DEC 13 APPROVED
Criteria: SA
27-07 Quantity installed
RUBBER SEAL UNDER SLAT –
(m) Refer to AMM Task 57-40-00-040-001
1 m (39.3 in) per slat may be missing.
Refer to MCDL-27-07 Illustration Rubber Seal under Slat
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
RUBBER SEAL UNDER SLAT
GLG A319-112 FLEET MCDL-27-07 P 2/2
AFM B 14 DEC 13
ILLUSTRATION RUBBER SEAL UNDER SLAT
Ident.: MCDL-27-07-00006248.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-07 Rubber Seal under Slat
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
GLG A319-112 FLEET MCDL-27-08 P 1/2
AFM A 12 DEC 17
27-08 Seal Between Inboard and Outboard Flap
Ident.: MCDL-27-08-00006250.0001001 / 29 NOV 17 APPROVED
Criteria: (A319 or A320 or A321)
1
27-08 Quantity installed
SEAL BETWEEN INBOARD AND OUTBOARD FLAP 6
Three may be missing.
Note: May be combined with MCDL items:
‐ 27-01 (Refer to 27-01 Flap Track Fairing)
‐ 27-13 (Refer to 27-13 Inter-flap Cushion Seal).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 63 kg (139 lb)
per missing seal
‐ En route performance limiting weight is reduced by 72 kg (159 lb) per missing seal
‐ If two or more seals are missing, fuel consumption is increased by 0.16 % per missing
seal.
Refer to MCDL-27-08 Illustration Seal between Inboard and Outboard Flap
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
GLG A319-112 FLEET MCDL-27-08 P 2/2
AFM B 12 DEC 17
ILLUSTRATION SEAL BETWEEN INBOARD AND OUTBOARD FLAP
Ident.: MCDL-27-08-00006251.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-08 Seal Between Inboard and Outboard Flap
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
INBOARD AILERON EDGE TO WING SEAL
GLG A319-112 FLEET MCDL-27-09 P 1/2
AFM A 25 JAN 11
27-09 Inboard Aileron Edge to Wing Seal
Ident.: MCDL-27-09-00006252.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-09 Quantity installed
INBOARD AILERON EDGE TO WING SEAL 4
One seal per aileron may be partially or completely missing provided that any loose or flapping
seal material is cut off.
Refer to MCDL-27-09 Illustration Inboard Aileron to Wing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
INBOARD AILERON EDGE TO WING SEAL
GLG A319-112 FLEET MCDL-27-09 P 2/2
AFM B 25 JAN 11
ILLUSTRATION INBOARD AILERON TO WING SEAL
Ident.: MCDL-27-09-00006253.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-09 Inboard Aileron Edge to Wing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT END SEAL AND WEATHER SEAL
GLG A319-112 FLEET MCDL-27-10 P 1/2
AFM A 03 MAY 16
27-10 Slat End Seal and Weather Seal
Ident.: MCDL-27-10-00006254.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-10 Quantity installed
SLAT END SEAL AND WEATHER SEAL 12
One seal per wing may be partially or completely missing provided any loose or flapping seal
material is cut off.
Refer to MCDL-27-10 Illustration Slat End Seal and Weather Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT END SEAL AND WEATHER SEAL
GLG A319-112 FLEET MCDL-27-10 P 2/2
AFM B 03 MAY 16
ILLUSTRATION SLAT END SEAL AND WEATHER SEAL
Ident.: MCDL-27-10-00006255.0001001 / 24 NOV 15 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-10 Slat End Seal and Weather Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK FILLER BLOCK
GLG A319-112 FLEET MCDL-27-11 P 1/2
AFM A 25 JAN 11
27-11 Slat Track Filler Block
Ident.: MCDL-27-11-00006256.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-11 Quantity installed
SLAT TRACK FILLER BLOCK 6
All may be missing.
Note: May be combined with MCDL item 27-12 (Refer to 27-12 Slat Track Sealing Packer).
Refer to MCDL-27-11 Illustration Slat Track Filler Block
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK FILLER BLOCK
GLG A319-112 FLEET MCDL-27-11 P 2/2
AFM B 25 JAN 11
ILLUSTRATION SLAT TRACK FILLER BLOCK
Ident.: MCDL-27-11-00006257.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-11 Slat Track Filler Block
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK SEALING PACKER
GLG A319-112 FLEET MCDL-27-12 P 1/2
AFM A 25 JAN 11
27-12 Slat Track Sealing Packer
Ident.: MCDL-27-12-00006258.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-12 Quantity installed
SLAT TRACK SEALING PACKER 4
All may be missing.
Note: May be combined with MCDL item 27-11 (Refer to 27-11 Slat Track Filler Block).
Refer to MCDL-27-12 Illustration Slat Track Sealing Packer
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
SLAT TRACK SEALING PACKER
GLG A319-112 FLEET MCDL-27-12 P 2/2
AFM B 25 JAN 11
ILLUSTRATION SLAT TRACK SEALING PACKER
Ident.: MCDL-27-12-00006259.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-12 Slat Track Sealing Packer
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
INTER-FLAP CUSHION SEAL
GLG A319-112 FLEET MCDL-27-13 P 1/2
AFM A 25 JAN 11
27-13 Inter-flap Cushion Seal
Ident.: MCDL-27-13-00006249.0001001 / 23 NOV 09 APPROVED
Criteria: SA
27-13 Quantity installed
INTER-FLAP CUSHION SEAL 4
One cushion seal may be missing per wing.
Refer to MCDL-27-13 Illustration Inter-Flap Cushion Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
INTER-FLAP CUSHION SEAL
GLG A319-112 FLEET MCDL-27-13 P 2/2
AFM B 25 JAN 11
ILLUSTRATION INTER-FLAP CUSHION SEAL
Ident.: MCDL-27-13-00006260.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-13 Inter-flap Cushion Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK MOVEABLE FAIRING SEAL
GLG A319-112 FLEET MCDL-27-14 P 1/2
AFM A 14 DEC 13
27-14 Flap Track Moveable Fairing Seal
Ident.: MCDL-27-14-00006261.0001001 / 02 DEC 13 APPROVED
Criteria: SA
27-14 Quantity installed
FLAP TRACK MOVEABLE FAIRING SEAL 12
(m) Refer to AMM Task 57-55-00-040-004
50 % of the seal length may be missing on each side of the flap track fairing for 100 flight
hours provided that a visual inspection is performed before each flight to ensure there is no
flapping seal on the aircraft.
Note: May be combined with MCDL item 27-15 (Refer to 27-15 Flap Track Fixed Fairing
Seal).
Refer to MCDL-27-14 Illustration Flap Track Moveable Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK MOVEABLE FAIRING SEAL
GLG A319-112 FLEET MCDL-27-14 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MOVEABLE FLAP TRACK FAIRING SEAL
Ident.: MCDL-27-14-00006262.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-14 Flap Track Moveable Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FIXED FAIRING SEAL
GLG A319-112 FLEET MCDL-27-15 P 1/2
AFM A 14 DEC 13
27-15 Flap Track Fixed Fairing seal
Ident.: MCDL-27-15-00006263.0001001 / 02 DEC 13 APPROVED
Criteria: (A318 or A319 or A320)
27-15 Quantity installed
FLAP TRACK FIXED FAIRING SEAL 18
(m) Refer to AMM Task 57-55-00-040-004
All may be missing for 100 flight hours provided that the hole is covered with high speed tape
and a visual inspection is performed before each flight.
Note: May be combined with MCDL item 27-14 (Refer to 27-14 Flap Track Moveable
Fairing Seal).
Refer to MCDL-27-15 Illustration Flap Track Fixed Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK FIXED FAIRING SEAL
GLG A319-112 FLEET MCDL-27-15 P 2/2
AFM B 14 DEC 13
ILLUSTRATION FIXED FLAP TRACK FAIRING SEAL
Ident.: MCDL-27-15-00006264.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 27-15 Flap Track Fixed Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
GLG A319-112 FLEET MCDL-27-16 P 1/2
AFM A 12 DEC 17
27-16 Flap Track Moveable Fairing Pivot Cover
Ident.: MCDL-27-16-00006265.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
27-16 Quantity installed
FLAP TRACK MOVEABLE FAIRING PIVOT COVER 12
(m) Refer to AMM Task 57-55-00-040-005
All may be missing provided that the hole is covered and a visual inspection is performed
daily.
Note: May be combined with MCDL item 27-03 (Refer to 27-03 Slat Track Closing Plate).
Refer to MCDL-27-16 Illustration Flap Track Moveable Fairing Pivot Cover
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
GLG A319-112 FLEET MCDL-27-16 P 2/2
AFM B 12 DEC 17
ILLUSTRATION FLAP TRACK MOVEABLE FAIRING PIVOT COVER
Ident.: MCDL-27-16-00006266.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 27-16 Flap Track Moveable Fairing Pivot Cover
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUEL
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
GLG A319-112 FLEET MCDL-28-01 P 1/2
AFM A 12 DEC 17
28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM
Ident.: MCDL-28-01-00006282.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
28-01 Quantity installed
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM –
(m) Refer to AMM Task 28-25-00-040-003
All may be missing provided seal integrity of coupling is positively confirmed (i.e. no fuel leak
reported).
Note: 1. If the coupling or O-ring is damaged and the cap cannot be fitted, dispatch is
permitted in accordance with this CDL item provided the cap is removed and
coupling integrity is verified.
2. If only the lanyard is missing, the removal of the cap is not necessary.
3. May be combined with MCDL item 28-02 (Refer to 28-02 Refuel Panel Door
192MB).
Refer to MCDL-28-01 Illustration Refuel/Defuel Coupling Cap 101 QM or 41 QM
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUEL
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
GLG A319-112 FLEET MCDL-28-01 P 2/2
AFM B 12 DEC 17
ILLUSTRATION REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
Ident.: MCDL-28-01-00006283.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUEL
REFUEL PANEL DOOR 192MB
GLG A319-112 FLEET MCDL-28-02 P 1/2
AFM A 12 DEC 17
28-02 Refuel Panel Door
Ident.: MCDL-28-02-00006285.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
28-02 Quantity installed
REFUEL PANEL DOOR 1
(m) Refer to AMM Task 52-42-00-040-001
Belly fairing mounted refuel panel door 192 MB may be missing (if installed).
Note: 1. If belly fairing mounted refuel panel door 192 MB is not installed, underwing
mounted refuel panel doors (622KB, 522KB) must not be missing.
2. May be combined with MCDL item 28-01 (Refer to 28-01 Refuel/Defuel Coupling
Cap 101 QM Or 41 QM).
Refer to MCDL-28-02 Illustration Refuel Panel Door 192MB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUEL
REFUEL PANEL DOOR 192MB
GLG A319-112 FLEET MCDL-28-02 P 2/2
AFM B 12 DEC 17
ILLUSTRATION REFUEL PANEL DOOR 192MB
Ident.: MCDL-28-02-00006286.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 28-02 Refuel Panel Door 192MB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
ICE AND RAIN PROTECTION
ICING INDICATOR
GLG A319-112 FLEET MCDL-30-01 P 1/2
AFM A 25 JAN 11
30-01 Icing Indicator
Ident.: MCDL-30-01-00006287.0001001 / 23 NOV 09 APPROVED
Criteria: SA
30-01 Quantity installed
ICING INDICATOR 1
May be missing.
•Procedures:
If icing conditions expected:
For icing conditions definition, Refer to LIM-GEN Icing Conditions Definition.
Turn on engine and wing anti-ice.
Refer to MCDL-30-01 Illustration Icing Indicator
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
ICE AND RAIN PROTECTION
ICING INDICATOR
GLG A319-112 FLEET MCDL-30-01 P 2/2
AFM B 25 JAN 11
ILLUSTRATION ICING INDICATOR
Ident.: MCDL-30-01-00006288.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 30-01 Icing Indicator
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
NOSE WHEEL HUBCAP
GLG A319-112 FLEET MCDL-32-03 P 1/2
AFM A 14 DEC 13
32-03 Nose Wheel Hubcap
Ident.: MCDL-32-03-00006297.0001001 / 02 DEC 13 APPROVED
Criteria: SA
32-03 Quantity installed
NOSE WHEEL HUBCAP 2
(m) Refer to AMM Task 32-41-00-040-001
One may be missing.
Refer to MCDL-32-03 Illustration Nose Wheel Hubcap
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
NOSE WHEEL HUBCAP
GLG A319-112 FLEET MCDL-32-03 P 2/2
AFM B 14 DEC 13
ILLUSTRATION NOSE WHEEL HUBCAP
Ident.: MCDL-32-03-00006298.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 32-03 Nose Wheel Hubcap
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
NOSE FITTING TOWING
GLG A319-112 FLEET MCDL-32-04 P 1/2
AFM A 14 DEC 13
32-04 Nose Fitting Towing
Ident.: MCDL-32-04-00006299.0001001 / 02 DEC 13 APPROVED
Criteria: SA
32-04 Quantity installed
NOSE FITTING TOWING 1
(m) Refer to AMM Task 32-21-00-040-001
May be missing.
Refer to MCDL-32-04 Illustration Nose Fitting Towing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
NOSE FITTING TOWING
GLG A319-112 FLEET MCDL-32-04 P 2/2
AFM B 14 DEC 13
ILLUSTRATION NOSE FITTING TOWING
Ident.: MCDL-32-04-00006300.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 32-04 Nose Fitting Towing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
GLG A319-112 FLEET MCDL-33-01 P 1/2
AFM A 14 DEC 13
33-01 Wing/Engine Scan Light Cover 3LX, 4LX
Ident.: MCDL-33-01-00006301.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-01 Quantity installed
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX 2
(m) Refer to AMM Task 33-49-00-040-001
One may be missing provided the hole is covered with high speed tape.
Note: If non transparent high speed tape is used, the affected light must be deactivated
(Refer to MMEL/MI-33-40 Wing Scan light).
Refer to MCDL-33-01 Illustration Wing/Engine Scan Light Cover 3LX, 4LX
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
GLG A319-112 FLEET MCDL-33-01 P 2/2
AFM B 14 DEC 13
ILLUSTRATION WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
Ident.: MCDL-33-01-00006302.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-01 Wing/Engine Scan light Cover 3LX, 4LX
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TAXI LIGHT LAMP 8LR
GLG A319-112 FLEET MCDL-33-02 P 1/2
AFM A 12 DEC 17
33-02 Taxi Light Lamp 8LR
Ident.: MCDL-33-02-00006303.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
33-02 Quantity installed
TAXI LIGHT LAMP 8LR 1
(m) Refer to AMM Task 33-46-00-040-001
May be missing provided the hole is covered and the affected light is deactivated (Refer to
MMEL/MI-33-40 Taxi and Takeoff light).
Note: May be combined with MCDL item 33-07 (Refer to 33-07 Landing Light Lens 7LB,
8LB) only for daylight operations.
Refer to MCDL-33-02 Illustration Taxi Light Lamp 8LR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TAXI LIGHT LAMP 8LR
GLG A319-112 FLEET MCDL-33-02 P 2/2
AFM B 12 DEC 17
ILLUSTRATION TAXI LIGHT LAMP 8LR
Ident.: MCDL-33-02-00006304.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-02 Taxi Light Lamp 8LR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
REAR NAVIGATION LIGHT LENS 15LA
GLG A319-112 FLEET MCDL-33-03 P 1/2
AFM A 14 DEC 13
33-03 Rear Navigation Light Lens 15LA
Ident.: MCDL-33-03-00006305.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-03 Quantity installed
REAR NAVIGATION LIGHT LENS 15LA 1
(m) Refer to AMM Task 33-41-00-040-002
May be missing for 10 flight cycles provided visual inspection is performed, before the first
flight of the day only, to check that there is no structural buckling.
Refer to MCDL-33-03 Illustration Rear Navigation Light Lens 15LA
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
REAR NAVIGATION LIGHT LENS 15LA
GLG A319-112 FLEET MCDL-33-03 P 2/2
AFM B 14 DEC 13
ILLUSTRATION REAR NAVIGATION LIGHT LENS 15LA
Ident.: MCDL-33-03-00006306.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-03 Rear Navigation Light Lens 15LA
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON) LIGHT COVER
GLG A319-112 FLEET MCDL-33-04 P 1/2
AFM A 14 DEC 13
33-04 Upper 7LV and Lower 6LV Anti-collision (Beacon) Light Cover
Ident.: MCDL-33-04-00006307.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-04 Quantity installed
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON)
LIGHT COVER
2
(m) Refer to AMM Task 33-48-00-040-001
All may be missing provided the lamp is covered with high speed tape and affected light is
deactivated (Refer to MMEL/MI-33-40 Beacon light).
•Performance:
If upper and lower light covers are missing, the following performance penalties are
applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 80 kg (177 lb)
‐ En route performance limiting weight is reduced by 90 kg (199 lb)
‐ Fuel consumption is increased by 0.22 %.
Refer to MCDL-33-04 Illustration Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light Cover
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON) LIGHT COVER
GLG A319-112 FLEET MCDL-33-04 P 2/2
AFM B 14 DEC 13
ILLUSTRATION UPPER AND LOWER ANTI-COLLISION ( BEACON) LIGHT COVER
Ident.: MCDL-33-04-00006308.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-04 Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light
Cover
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
LOGO LIGHT LENS (COVER) 3LY, 4LY
GLG A319-112 FLEET MCDL-33-05 P 1/2
AFM A 14 DEC 13
33-05 Logo Light Lens (Cover) 3LY, 4LY
Ident.: MCDL-33-05-00006309.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-05 Quantity installed
LOGO LIGHT LENS (COVER) 3LY, 4LY 2
(m) Refer to AMM Task 33-47-00-040-001
All may be missing provided the hole is covered with high speed tape.
Note: If non transparent high speed tape is used, the affected light must be deactivated.
(Refer to MMEL/MI-33-40 Logo light).
Refer to MCDL-33-05 Illustration Logo Light Lens (Cover) 3LY, 4LY
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
LOGO LIGHT LENS (COVER) 3LY, 4LY
GLG A319-112 FLEET MCDL-33-05 P 2/2
AFM B 14 DEC 13
ILLUSTRATION LOGO LIGHT LENS (COVER) 3LY, 4LY
Ident.: MCDL-33-05-00006310.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-05 Logo Light Lens (Cover) 3LY, 4LY
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
LANDING LIGHT LENS 7LB, 8LB
GLG A319-112 FLEET MCDL-33-07 P 1/2
AFM A 12 DEC 17
33-07 Landing Light Lens 7LB, 8LB
Ident.: MCDL-33-07-00006321.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
33-07 Quantity installed
LANDING LIGHT LENS 7LB, 8LB 2
(m) Refer to AMM Task 33-42-00-040-001
One may be missing provided the associated light is retracted and deactivated and the hole is
covered (Refer to MMEL/MI-33-40 Landing light).
Note: May be combined with MCDL item 33-02 (Refer to 33-02 Taxi Light Lamp 8LR) only
for daylight operations.
Refer to MCDL-33-07 Illustration Landing Light Lens 7LB, 8LB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
LANDING LIGHT LENS 7LB, 8LB
GLG A319-112 FLEET MCDL-33-07 P 2/2
AFM B 12 DEC 17
ILLUSTRATION LANDING LIGHT LENS 7LB, 8LB
Ident.: MCDL-33-07-00006322.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-07 Landing Light Lens 7LB, 8LB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TURN OFF LIGHT LAMP 3LC1, 3LC2
GLG A319-112 FLEET MCDL-33-08 P 1/2
AFM A 14 DEC 13
33-08 Turn OFF Light Lamp 3LC1, 3LC2
Ident.: MCDL-33-08-00006324.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-08 Quantity installed
TURN OFF LIGHT LAMP 3LC1, 3LC2 2
(m) Refer to AMM Task 33-43-00-040-002
All may be missing provided the hole is covered with high speed tape and the affected light is
deactivated (Refer to MMEL/MI-33-40 Runway Turnoff light).
Refer to MCDL-33-08 Illustration Turn OFF Light Lamp 3LC1, 3LC2
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TURN OFF LIGHT LAMP 3LC1, 3LC2
GLG A319-112 FLEET MCDL-33-08 P 2/2
AFM B 14 DEC 13
ILLUSTRATION TURN OFF LIGHT LAMP 3LC1, 3LC2
Ident.: MCDL-33-08-00006325.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-08 Turn OFF Light Lamp 3LC1, 3LC2
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TAKEOFF LIGHT LAMP 7LR
GLG A319-112 FLEET MCDL-33-09 P 1/2
AFM A 14 DEC 13
33-09 Takeoff light lamp 7LR
Ident.: MCDL-33-09-00006327.0001001 / 02 DEC 13 APPROVED
Criteria: SA
33-09 Quantity installed
TAKEOFF LIGHT LAMP 7LR 1
(m) Refer to AMM Task 33-46-00-040-002
May be missing provided the hole is covered with high speed tape and the affected light is
deactivated (Refer to MMEL/MI-33-40 Taxi and Takeoff light).
Refer to MCDL-33-09 Illustration Takeoff Light Lamp 7LR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
TAKEOFF LIGHT LAMP 7LR
GLG A319-112 FLEET MCDL-33-09 P 2/2
AFM B 14 DEC 13
ILLUSTRATION TAKEOFF LIGHT LAMP 7LR
Ident.: MCDL-33-09-00006328.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 33-09 Takeoff Light Lamp 7LR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
APU
APU OVERPRESSURE RELEASE DOOR
GLG A319-112 FLEET MCDL-49-01 P 1/2
AFM A 25 JAN 11
49-01 APU Overpressure Release Door
Ident.: MCDL-49-01-00006329.0001001 / 23 NOV 09 APPROVED
Criteria: SA
49-01 Quantity installed
APU OVERPRESSURE RELEASE DOOR 1
May be missing provided APU is not used in flight and on ground.
•Limitations:
Flights for which APU is mandatory are not allowed.
Refer to MCDL-49-01 Illustration APU Overpressure Release Door
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
APU
APU OVERPRESSURE RELEASE DOOR
GLG A319-112 FLEET MCDL-49-01 P 2/2
AFM B 25 JAN 11
ILLUSTRATION APU OVERPRESSURE RELEASE DOOR
Ident.: MCDL-49-01-00006330.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 49-01 APU Overpressure Release Door
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
PASSENGER DOOR SCUFF PLATE
GLG A319-112 FLEET MCDL-51-02 P 1/2
AFM A 25 JAN 11
51-02 Passenger Door Scuff Plate
Ident.: MCDL-51-02-00006333.0001001 / 23 NOV 09 APPROVED
Criteria: SA
51-02 Quantity installed
PASSENGER DOOR SCUFF PLATE –
All may be missing.
Refer to MCDL-51-02 Illustration Passenger Door Scuff Plate
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
PASSENGER DOOR SCUFF PLATE
GLG A319-112 FLEET MCDL-51-02 P 2/2
AFM B 25 JAN 11
ILLUSTRATION PASSENGER DOOR SCUFF PLATE
Ident.: MCDL-51-02-00006334.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 51-02 Passenger Door Scuff Plate
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
FAIRING AFT SAFETY STAY POINT 311 AL
GLG A319-112 FLEET MCDL-51-04 P 1/2
AFM A 25 JAN 11
51-04 Fairing Aft Safety Stay Point 311 AL
Ident.: MCDL-51-04-00006338.0001001 / 23 NOV 09 APPROVED
Criteria: SA
51-04 Quantity installed
FAIRING AFT SAFETY STAY POINT 311 AL 1
May be missing.
Refer to MCDL-51-04 Illustration Fairing Aft Safety Stay Point 311AL
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
FAIRING AFT SAFETY STAY POINT 311 AL
GLG A319-112 FLEET MCDL-51-04 P 2/2
AFM B 25 JAN 11
ILLUSTRATION FAIRING AFT SAFETY STAY POINT 311AL
Ident.: MCDL-51-04-00006339.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 51-04 Fairing Aft Safety Stay Point 311 AL
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
TOILET SERVICING AND DRAINAGE DOOR
GLG A319-112 FLEET MCDL-52-01 P 1/2
AFM A 07 FEB 17
52-01 Toilet Servicing and Drainage Door 172 AR
Ident.: MCDL-52-01-00006441.0003001 / 23 JAN 17 APPROVED
Criteria: ((A319 or A320 or A321) and 20109)
52-01 Quantity installed
TOILET SERVICING AND DRAINAGE DOOR 172 AR 1
(m) Refer to AMM Task 52-42-00-040-002
May be missing.
Note: 1. Following the deactivation procedures of the toilet servicing and draining door,
the toilet system remains operative. Ensure toilets are not used on ground due to
possible ongoing servicing operations.
2. May be combined with MCDL items:
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB -
197 EB - 198 CB)
‐ 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors
on Ground 195 BB - 196 BB)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 63 kg (139 lb)
‐ En route performance limiting weight is reduced by 72 kg (159 lb).
Refer to MCDL-52-01 Illustration Toilet Servicing and Drainage Door
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
TOILET SERVICING AND DRAINAGE DOOR
GLG A319-112 FLEET MCDL-52-01 P 2/2
AFM B 07 FEB 17
ILLUSTRATION TOILET SERVICING AND DRAINAGE DOOR
Ident.: MCDL-52-01-00006442.0002001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (SA and 20109)
for dispatch conditions:Refer to 52-01 Toilet Servicing and Drainage Door
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO HYDRAULIC GROUND
CONNECTORS 197 CB - 197 EB - 198 CB
GLG A319-112 FLEET MCDL-52-02 P 1/2
AFM A 11 JUL 17
52-02 Access Door To Hydraulic Ground
Connectors 197 CB - 197 EB - 198 CB
Ident.: MCDL-52-02-00006447.0001001 / 16 JUN 17 APPROVED
Criteria: (A319 or A320 or A321)
52-02 Quantity installed
ACCESS DOOR TO HYDRAULIC GROUND CONNECTORS
197 CB - 197 EB - 198 CB
3
(m) Refer to AMM Task 52-42-00-040-802
One may be missing.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 63 kg (139 lb)
‐ En route performance limiting weight is reduced by 72 kg (159 lb).
Refer to MCDL-52-02 Illustration Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198
CB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO HYDRAULIC GROUND
CONNECTORS 197 CB - 197 EB - 198 CB
GLG A319-112 FLEET MCDL-52-02 P 2/2
AFM B 11 JUL 17
ILLUSTRATION ACCESS DOOR TO HYDRAULIC
GROUND CONNECTORS 197 CB - 197 EB - 198 CB
Ident.: MCDL-52-02-00006449.0001001 / 24 NOV 15 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
GLG A319-112 FLEET MCDL-52-03 P 1/4
AFM A to B → 30 JUL 15
52-03 Access Door To Potable Water Filling And Drainage 133 AL - 171 AL
Ident.: TDU / MCDL-52-03-00016655.0001001 / 06 JUL 15 APPROVED
Criteria: (A319 or A321)
Impacted DU: 00006452 Access Door to Potable Water Filling and Drainage
Belongs to TR564 Issue 1
52-03 Quantity installed
ACCESS DOOR TO POTABLE WATER FILLING AND
DRAINAGE 133 AL - 171 AL
2
One may be missing.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
Refer to MCDL-52-03 Illustration Access Door to Potable Water Filling and Drainage
52-03 Access Door To Potable Water Filling
And Drainage 133 AL - 171 AL - 192 NB
Ident.: MCDL-52-03-00006452.0001001 / 14 JAN 15 APPROVED
Criteria: (A319 or A320 or A321)
Impacted by TDU: 00016655 Access Door to Potable Water Filling and Drainage
52-03 Quantity installed
ACCESS DOOR TO POTABLE WATER FILLING AND
DRAINAGE 133 AL - 171 AL - 192 NB
3
One may be missing.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
Continued on the following page
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
GLG A319-112 FLEET MCDL-52-03 P 2/4
AFM ← B to C 30 JUL 15
Continued from the previous page Access Door To Potable Water Filling And Drainage 133 AL - 171 AL - 192 NB
Refer to MCDL-52-03 Illustration Access Door to Potable Water Filling and Drainage
ILLUSTRATION ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Ident.: TDU / MCDL-52-03-00016656.0001001 / 06 JUL 15 APPROVED
Criteria: (A319 or A321)
Impacted DU: 00006453 Illustration Access Door to Potable Water Filling and Drainage
Belongs to TR564 Issue 1
For dispatch conditions: Refer to 52-03 Access Door to Potable Water Filling and Drainage.
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
GLG A319-112 FLEET MCDL-52-03 P 3/4
AFM D 30 JUL 15
ILLUSTRATION ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Ident.: MCDL-52-03-00006453.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (A319 or A320 or A321)
Impacted by TDU: 00016656 Illustration Access Door to Potable Water Filling and Drainage
For dispatch conditions:Refer to 52-03 Access Door to Potable Water Filling and Drainage
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Intentionally left blank
GLG A319-112 FLEET MCDL-52-03 P 4/4
AFM 30 JUL 15
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO OPENING CONTROL OF LANDING
GEAR DOORS ON GROUND 195 BB - 196 BB
GLG A319-112 FLEET MCDL-52-04 P 1/2
AFM A 16 MAR 15
52-04 Access Door To Opening Control Of Landing
Gear Doors On Ground 195 BB - 196 BB
Ident.: MCDL-52-04-00006455.0001001 / 14 JAN 15 APPROVED
Criteria: (A319 or A320 or A321)
52-04 Quantity installed
ACCESS DOOR TO OPENING CONTROL OF LANDING
GEAR DOORS ON GROUND 195 BB - 196 BB
2
One may be missing for five flight cycles.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB)
‐ 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
•Limitations:
Flight in forecasted thunderstorm condition is not allowed.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 63 kg (139 lb)
‐ En route performance limiting weight is reduced by 72 kg (159 lb).
Refer to MCDL-52-04 Illustration Access Door to Opening Control of Landing Gear Doors on Ground
195 BB - 196 BB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO OPENING CONTROL OF LANDING
GEAR DOORS ON GROUND 195 BB - 196 BB
GLG A319-112 FLEET MCDL-52-04 P 2/2
AFM B 16 MAR 15
ILLUSTRATION ACCESS DOOR TO OPENING CONTROL
OF LANDING GEAR DOORS ON GROUND 195 BB - 196 BB
Ident.: MCDL-52-04-00006456.0001001 / 03 AUG 10 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB
GLG A319-112 FLEET MCDL-52-05 P 1/2
AFM A 12 DEC 17
52-05 Access Door To Air Conditioning Ground Supply 191 CB
Ident.: MCDL-52-05-00006457.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
52-05 Quantity installed
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY
191 CB
1
May be missing.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB)
‐ 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB)
‐ 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB)
‐ 52-21 (Refer to 52-21 Blue Hydraulic Access Door 197 FB).
Refer to MCDL-52-05 Illustration Access Door to Air Conditioning Ground Supply 191 CB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB
GLG A319-112 FLEET MCDL-52-05 P 2/2
AFM B 12 DEC 17
ILLUSTRATION ACCESS DOOR TO AIR CONDITIONNING GROUND SUPPLY 191 CB
Ident.: MCDL-52-05-00006458.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
EXTERNAL POWER GROUND
CONNECTION ACCESS DOOR ASSY 121 AL
GLG A319-112 FLEET MCDL-52-07 P 1/2
AFM A 10 OCT 17
52-07 External Power Ground Connection Access Door Assy 121 AL
Ident.: MCDL-52-07-00006461.0001001 / 02 OCT 17 APPROVED
Criteria: SA
52-07 Quantity installed
EXTERNAL POWER GROUND CONNECTION ACCESS
DOOR ASSY 121 AL
1
(m) Refer to AMM Task 52-42-00-040-003
May be missing for five flight cycles provided the hole is covered and a visual inspection is
performed before each flight.
•Limitations:
Flight in forecasted thunderstorm condition is not allowed.
Refer to MCDL-52-07 Illustration External Power Ground Connection Access Door Assy 121 AL
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
EXTERNAL POWER GROUND
CONNECTION ACCESS DOOR ASSY 121 AL
GLG A319-112 FLEET MCDL-52-07 P 2/2
AFM B 10 OCT 17
ILLUSTRATION EXTERNAL POWER GROUND CONNECTION ACCESS DOOR ASSY 121 AL
Ident.: MCDL-52-07-00006462.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-07 External Power Ground Connection Access Door Assy 121
AL
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
GLG A319-112 FLEET MCDL-52-08 P 1/2
AFM A 25 JAN 11
52-08 Access Door Of Cargo Opening System 134 AR - 154 AR
Ident.: MCDL-52-08-00006463.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
52-08 Quantity installed
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154
AR
2
All may be missing.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 79 kg (175 lb)
per missing access door
‐ En-route performance limiting weight is reduced by 108 kg (239 lb) per missing access
door
‐ Fuel consumption is increased by 0.27 % per missing access door.
Refer to MCDL-52-08 Illustration Access Door of Cargo Opening System 134 AR - 154 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
GLG A319-112 FLEET MCDL-52-08 P 2/2
AFM B 25 JAN 11
ILLUSTRATION ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
Ident.: MCDL-52-08-00006464.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-08 Access Door of Cargo Opening System 134 AR - 154 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR MAIN DOOR (713, 714)
GLG A319-112 FLEET MCDL-52-09 P 1/2
AFM A 14 DEC 13
52-09 Nose Landing Gear Main Door (713, 714)
Ident.: MCDL-52-09-00006465.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320)
52-09 Quantity installed
NOSE LANDING GEAR MAIN DOOR (713, 714) 2
(m) Refer to AMM Task 32-22-00-040-001
May be missing provided both main doors (713, 714) are removed and both aft doors (715,
716) (Refer to 52-10 Nose Landing Gear Aft Door (715, 716)) are removed.
Note: May be combined with MCDL item 52-11 (Refer to 52-11 Nose Landing Gear Leg
Door (712))
Disregard the alert L/G DOORS NOT CLOSED displayed on the ECAM.
•Limitations:
Passengers transportation is not allowed.
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Maximum speed: 220 kt IAS/ M 0.5
•Performance:
Note: Reference performance for penalties computations are performance with landing
gear down.
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 918 kg
(2 024 lb)
‐ En-route performance limiting weight is reduced by 1 000 kg (2 205 lb)
‐ Fuel consumption is increased by 2 %.
Refer to MCDL-52-09 Illustration Nose Landing Gear Main Door (713, 714)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR MAIN DOOR (713, 714)
GLG A319-112 FLEET MCDL-52-09 P 2/2
AFM B 14 DEC 13
ILLUSTRATION NOSE LANDING GEAR MAIN DOOR (713, 714)
Ident.: MCDL-52-09-00006466.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-09 Nose Landing Gear Main Door (713, 714)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR AFT DOOR (715, 716)
GLG A319-112 FLEET MCDL-52-10 P 1/2
AFM A 14 DEC 13
52-10 Nose Landing Gear Aft Door (715, 716)
Ident.: MCDL-52-10-00006467.0001001 / 02 DEC 13 APPROVED
Criteria: SA
52-10 Quantity installed
NOSE LANDING GEAR AFT DOOR (715, 716) 2
(m) Refer to AMM Task 32-22-00-040-002
All may be missing.
Note: May be combined with MCDL item 52-11 (Refer to 52-11 Nose Landing Gear Leg
Door (712))
•Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
•Performance:
Note: Reference performance for penalties computations are performance with landing
gear down.
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 79 kg (175 lb)
‐ En-route performance limiting weight is reduced by 100 kg (221 lb)
‐ Fuel consumption is increased by 0.25 %.
When combined with MCDL item 52-09 (Refer to 52-09 Nose Landing Gear Main Door
(713, 714)), the performance penalties published in 52-09 are applicable.
Refer to MCDL-52-10 Illustration Nose Landing Gear Aft Door (715, 716)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR AFT DOOR (715, 716)
GLG A319-112 FLEET MCDL-52-10 P 2/2
AFM B 14 DEC 13
ILLUSTRATION NOSE LANDING GEAR AFT DOOR (715, 716)
Ident.: MCDL-52-10-00006468.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-10 Nose Landing Gear Aft Door (715, 716)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR LEG DOOR (712)
GLG A319-112 FLEET MCDL-52-11 P 1/2
AFM A 14 DEC 13
52-11 Nose Landing Gear Leg Door (712)
Ident.: MCDL-52-11-00006471.0001001 / 02 DEC 13 APPROVED
Criteria: SA
52-11 Quantity installed
NOSE LANDING GEAR LEG DOOR (712) 1
(m) Refer to AMM Task 32-22-00-040-003
May be missing.
Note: May be combined with MCDL items 52-09 (Refer to 52-09 Nose Landing Gear Main
Door (713, 714)) and 52-10 (Refer to 52-10 Nose Landing Gear Aft Door (715, 716)).
•Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
Refer to MCDL-52-11 Illustration Nose Landing Gear Leg Door (712)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
NOSE LANDING GEAR LEG DOOR (712)
GLG A319-112 FLEET MCDL-52-11 P 2/2
AFM B 14 DEC 13
ILLUSTRATION NOSE LANDING GEAR LEG DOOR (712)
Ident.: MCDL-52-11-00006472.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-11 Nose Landing Gear Leg Door (712)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP)
GLG A319-112 FLEET MCDL-52-12 P 1/2
AFM A 14 DEC 13
52-12 Main Landing Gear Door (732, 742) (flight with gear up)
Ident.: MCDL-52-12-00006473.0001001 / 02 DEC 13 APPROVED
Criteria: (A318 or A319 or A320)
52-12 Quantity installed
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH
GEAR UP)
2
(m) Refer to AMM Task 32-12-00-040-005
One may be missing.
•Limitations:
Passengers transportation is not allowed.
Flight in forecasted icing conditions is not allowed.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 394 kg
(869 lb)
‐ En-route performance limiting weight is reduced by 540 kg (1 191 lb)
‐ Fuel consumption is increased by 1.22 %.
Refer to MCDL-52-12 Illustration Main Landing Gear Door (732, 742)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP)
GLG A319-112 FLEET MCDL-52-12 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MAIN LANDING GEAR DOOR (732, 742)
Ident.: MCDL-52-12-00006474.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-12 Main Landing Gear Door (732, 742) (flight with gear up)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP)
GLG A319-112 FLEET MCDL-52-13 P 1/2
AFM A 14 DEC 13
52-13 Main Landing Gear Door (733, 743) (flight with gear up)
Ident.: MCDL-52-13-00006487.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
52-13 Quantity installed
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH
GEAR UP)
2
(m) Refer to AMM Task 32-12-00-040-005
One may be missing.
•Limitations:
Passengers transportation is not allowed.
Flight in forecasted icing conditions is not allowed.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 111 kg
(245 lb)
‐ En-route performance limiting weight is reduced by 126 kg (278 lb)
‐ Fuel consumption is increased by 0.28 %.
Refer to MCDL-52-13 Illustration Main Landing Gear Door (733, 743)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP)
GLG A319-112 FLEET MCDL-52-13 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MAIN LANDING GEAR DOOR (733, 743)
Ident.: MCDL-52-13-00006488.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-13 Main Landing Gear Door (733, 743) (flight with gear up)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-14 P 1/2
AFM A 14 DEC 13
52-14 Main Landing Gear Door (732, 742) (Flight with gear down)
Ident.: MCDL-52-14-00006475.0001001 / 02 DEC 13 APPROVED
Criteria: (A318 or A319 or A320)
52-14 Quantity installed
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH
GEAR DOWN)
2
(m) Refer to AMM Task 32-12-00-040-001
One may be missing.
Disregard the alert L/G DOORS NOT CLOSED displayed on the ECAM.
•Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
•Performance:
Note: Reference performance for penalties computations are performance with landing
gear down.
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 394 kg
(869 lb)
‐ En-route performance limiting weight is reduced by 450 kg (993 lb)
‐ Fuel consumption is increased by 1.00 %.
Refer to MCDL-52-14 Illustration Main Landing Gear Door (732, 742)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-14 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MAIN LANDING GEAR DOOR (732, 742)
Ident.: MCDL-52-14-00006476.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-14 Main Landing Gear Door (732, 742) (flight with gear down)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-15 P 1/2
AFM A 14 DEC 13
52-15 Main Landing Gear Door (733, 743) (Flight with gear down)
Ident.: MCDL-52-15-00006489.0001001 / 02 DEC 13 APPROVED
Criteria: (A319 or A320 or A321)
52-15 Quantity installed
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH
GEAR DOWN)
2
(m) Refer to AMM Task 32-12-00-040-001
One may be missing.
Disregard the alert L/G DOORS NOT CLOSED displayed on the ECAM.
•Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
•Performance:
Note: Reference performance for penalties computations are performance with landing
gear down.
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 111 kg
(245 lb)
‐ En-route performance limiting weight is reduced by 200 kg (441 lb)
‐ Fuel consumption is increased by 0.30 %.
Refer to MCDL-52-15 Illustration Main Landing Gear Door (733, 743)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-15 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MAIN LANDING GEAR DOOR (733, 743)
Ident.: MCDL-52-15-00006490.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-15 Main Landing Gear Door (733, 743) (Flight with gear down)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-16 P 1/2
AFM A 14 DEC 13
52-16 Main Landing Gear Door (734, 744) (Flight with gear down)
Ident.: MCDL-52-16-00006491.0001001 / 02 DEC 13 APPROVED
Criteria: (A318 or A319 or A320)
52-16 Quantity installed
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH
GEAR DOWN)
2
(m) Refer to AMM Task 32-12-00-040-001
One may be missing.
Disregard the alert L/G DOORS NOT CLOSED displayed on the ECAM.
•Limitations:
Flight with landing gear down is required.
Refer to APP-LGDN-GEN General
•Performance:
Note: Reference performance for penalties computations are performance with landing
gear down.
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 623 kg
(1 374 lb)
‐ En-route performance limiting weight is reduced by 700 kg (1 544 lb)
‐ Fuel consumption is increased by 1.50 %.
Refer to MCDL-52-16 Illustration Main Landing Gear Door (734, 744)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN)
GLG A319-112 FLEET MCDL-52-16 P 2/2
AFM B 14 DEC 13
ILLUSTRATION MAIN LANDING GEAR DOOR (734, 744)
Ident.: MCDL-52-16-00006492.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
for dispatch conditions:Refer to 52-16 Main Landing Gear Door (734, 744) (Flight with gear down)
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
GLG A319-112 FLEET MCDL-52-18 P 1/2
AFM A 25 JAN 11
52-18 Main Landing Gear Door : Seal On Secondary Hinged Fairing
Ident.: MCDL-52-18-00006479.0001001 / 23 NOV 09 APPROVED
Criteria: SA
52-18 Quantity installed
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY
HINGED FAIRING
6
All may be missing.
•Performance:
If three or more seals are missing, the following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 24 kg (53 lb)
per missing seal
‐ En-route performance limiting weight is reduced by 27 kg (60 lb) per missing seal
‐ Fuel consumption is increased by 0.07 % per missing seal.
Refer to MCDL-52-18 Illustration Main Landing Gear Door : Seal on Secondary Hinged Fairing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
GLG A319-112 FLEET MCDL-52-18 P 2/2
AFM B 25 JAN 11
ILLUSTRATION MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
Ident.: MCDL-52-18-00006480.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-18 Main Landing Gear Door : Seal on Secondary Hinged Fairing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
PAX DOOR UPPER COVER PLATE
GLG A319-112 FLEET MCDL-52-19 P 1/2
AFM A 25 JAN 11
52-19 Pax Door Upper Cover Plate
Ident.: MCDL-52-19-00006481.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
52-19 Quantity installed
PAX DOOR UPPER COVER PLATE 4
All may be missing.
Note: The affected door must be considered as inoperative (Refer to MMEL/MI-52-10
Cabin Door).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 66 kg (146 lb)
per missing plate
‐ En-route performance limiting weight is reduced by 90 kg (199 lb) per missing plate
‐ Fuel consumption is increased by 0.23 % per missing plate.
Refer to MCDL-52-19 Illustration Pax Door Upper Cover Plate
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
PAX DOOR UPPER COVER PLATE
GLG A319-112 FLEET MCDL-52-19 P 2/2
AFM B 25 JAN 11
ILLUSTRATION PAX DOOR UPPER COVER PLATE
Ident.: MCDL-52-19-00006482.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-19 Pax Door Upper Cover Plate
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
GLG A319-112 FLEET MCDL-52-20 P 1/2
AFM A 16 MAR 15
52-20 Access Door To HP Air Ground Connector 191 DB
Ident.: MCDL-52-20-00006483.0001001 / 14 JAN 15 APPROVED
Criteria: SA
52-20 Quantity installed
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB 1
May be missing.
Note: May be combined with MCDL items:
‐ 52-01 (Refer to 52-01 Toilet Servicing and Drainage Door)
‐ 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB)
‐ 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
‐ 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB)
‐ 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
Refer to MCDL-52-20 Illustration Access Door to HP Air Ground Connector 191 DB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
GLG A319-112 FLEET MCDL-52-20 P 2/2
AFM B 16 MAR 15
ILLUSTRATION ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
Ident.: MCDL-52-20-00006484.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-20 Access Door to HP Air Ground Connector 191 DB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
BLUE HYDRAULIC ACCESS DOOR 197 FB
GLG A319-112 FLEET MCDL-52-21 P 1/2
AFM A 12 DEC 17
52-21 Blue Hydraulic Access Door 197 FB
Ident.: MCDL-52-21-00007449.0001001 / 29 NOV 17 APPROVED
Criteria: SA
1
52-21 Quantity installed
BLUE HYDRAULIC ACCESS DOOR 197 FB 1
(m) Refer to AMM Task 52-41-00-040-001
May be missing.
Note: May be combined with MCDL item 52-05 (Refer to 52-05 Access Door to Air
Conditioning Ground Supply 191 CB).
Refer to MCDL-52-21 Illustration Blue Hydraulic Access Door 197 FB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
BLUE HYDRAULIC ACCESS DOOR 197 FB
GLG A319-112 FLEET MCDL-52-21 P 2/2
AFM B 12 DEC 17
ILLUSTRATION BLUE HYDRAULIC ACCESS DOOR 197 FB
Ident.: MCDL-52-21-00007450.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-21 Blue Hydraulic Access Door 197 FB
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
GLG A319-112 FLEET MCDL-52-22 P 1/2
AFM A 14 DEC 13
52-22 Forward Cargo Door Access Cover Panel 825 AR
Ident.: MCDL-52-22-00007451.0001001 / 02 DEC 13 APPROVED
Criteria: SA
52-22 Quantity installed
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR 1
(m) Refer to AMM Task 52-31-00-040-004
May be missing provided all latching hooks are checked latched and locked before each flight.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 234 kg
(516 lb)
‐ En-route performance limiting weight is reduced by 266 kg (587 lb)
‐ Fuel consumption is increased by 0.64 %.
Refer to MCDL-52-22 Illustration Forward Cargo Door Access Cover Panel 825 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
GLG A319-112 FLEET MCDL-52-22 P 2/2
AFM B 14 DEC 13
ILLUSTRATION FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
Ident.: MCDL-52-22-00007452.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 52-22 Forward Cargo Door Access Cover Panel 825 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
GLG A319-112 FLEET MCDL-52-23 P 1/2
AFM A 01 SEP 16
52-23 Aft Cargo Door Access Cover Panel 826 AR
Ident.: MCDL-52-23-00007453.0001001 / 02 DEC 13 APPROVED
Criteria: SA
52-23 Quantity installed
AFT CARGO DOOR ACCESS COVER PANEL 826 AR 1
(m) Refer to AMM Task 52-32-00-040-004
May be missing provided all latching hooks are checked latched and locked before each flight.
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 190 kg
(419 lb)
‐ En-route performance limiting weight is reduced by 216 kg (477 lb)
‐ Fuel consumption is increased by 0.53 %.
Refer to MCDL-52-23 Illustration Aft Cargo Door Access Cover Panel 826 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
DOORS
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
GLG A319-112 FLEET MCDL-52-23 P 2/2
AFM B 01 SEP 16
ILLUSTRATION AFT CARGO DOOR ACCESS COVER PANEL 826 AR
Ident.: MCDL-52-23-00007454.0002001 / 17 AUG 16 FOR INFORMATION ONLY
Criteria: A319
For dispatch conditions: Refer to 52-23 Aft Cargo Door Access Cover Panel 826 AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
BELLY FAIRING VENT LOUVER VANE
GLG A319-112 FLEET MCDL-53-01 P 1/2
AFM A 16 MAR 15
53-01 Belly Fairing Vent Louver Vane
Ident.: MCDL-53-01-00006512.0001001 / 14 JAN 15 APPROVED
Criteria: SA
53-01 Quantity installed
BELLY FAIRING VENT LOUVER VANE –
(m) Refer to AMM Task 53-35-00-040-802
Three may be missing per vent louver.
Note: Vane with a crack length higher than 50 % must be removed before next flight.
Refer to MCDL-53-01 Illustration Belly Fairing Vent Louver Vane
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
BELLY FAIRING VENT LOUVER VANE
GLG A319-112 FLEET MCDL-53-01 P 2/2
AFM B 16 MAR 15
ILLUSTRATION BELLY FAIRING VENT LOUVER VANE
Ident.: MCDL-53-01-00006513.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 53-01 Belly Fairing Vent Louver Vane
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
ROOT FILLET FAIRING
GLG A319-112 FLEET MCDL-53-03 P 1/2
AFM A 14 DEC 13
53-03 Root Fillet Fairing
Ident.: MCDL-53-03-00011063.0005001 / 02 DEC 13 APPROVED
Criteria: A319
53-03 Quantity installed
ROOT FILLET FAIRING 2
(m) Refer to AMM Task 53-35-00-040-001
All may be missing.
Note: Must not be combined with MCDL item 54-01 (Refer to 54-01 Nacelle Strake)
or MCDL item 54-03 (Refer to 54-03 Pylon Pressure Relief Door 413(423) BL -
414(424) BR).
•Performance:
The following performance penalty is applicable:
‐ Takeoff performance limiting weight is reduced by 1 800 kg (3 969 lb).
Note: The above performance penalty is not applicable if the flight crew can check V2
greater than 1.15 VS1G.
Refer to MCDL-53-03 Illustration Root Fillet Fairing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
ROOT FILLET FAIRING
GLG A319-112 FLEET MCDL-53-03 P 2/2
AFM B 14 DEC 13
ILLUSTRATION ROOT FILLET FAIRING
Ident.: MCDL-53-03-00011064.0001001 / 03 AUG 10 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 53-03 Root Fillet Fairing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
NACELLE STRAKE
GLG A319-112 FLEET MCDL-54-01 P 1/2
AFM A 16 MAR 15
54-01 Nacelle Strake
Ident.: MCDL-54-01-00006516.0005001 / 14 JAN 15 APPROVED
Criteria: A319
54-01 Quantity installed
NACELLE STRAKE 4
(m) Refer to AMM Task
All may be missing.
Note: Must not be combined with MCDL item 53-03 (Refer to 53-03 Root Fillet Fairing).
•Procedures:
Approach speed: VAPP + 3 kt.
Landing distance: multiply by 1.05.
•Performance:
The following performance penalties are applicable:
‐ If no internal strakes and one or both external strakes are missing, takeoff performance
limiting weight is reduced by 4 800 kg (10 583 lb)
‐ If one or both internal strakes are missing (with or without external strakes missing),
takeoff performance limiting weight is reduced by 6 400 kg (14 110 lb)
‐ Increase V2 and VR by 1 kt.
Note: The performance penalties are not applicable if the flight crew can check V2
greater than 1.18 VS1G.
Refer to MCDL-54-01 Illustration Nacelle Strake
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
NACELLE STRAKE
GLG A319-112 FLEET MCDL-54-01 P 2/2
AFM B 16 MAR 15
ILLUSTRATION NACELLE STRAKE
Ident.: MCDL-54-01-00006517.0002001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (A318 or A319 or A321)
For dispatch conditions:Refer to 54-01 Nacelle Strake
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
GLG A319-112 FLEET MCDL-54-03 P 1/2
AFM A 14 DEC 13
54-03 Pylon Pressure Relief Door 413(423) BL - 414(424) BR
Ident.: MCDL-54-03-00006540.0003001 / 02 DEC 13 APPROVED
Criteria: A319
54-03 Quantity installed
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424)
BR
4
(m) Refer to AMM Task 54-52-00-040-001
All may be missing for 5 flight cycles only.
Note: 1. If one door is missing on a pylon, the other door on the same pylon must be
removed.
2. Must not be combined with MCDL item 53-03 (Refer to 53-03 Root Fillet Fairing).
•Limitations:
Maximum cruise speed: M 0.78.
•Procedures:
Approach speed: VAPP + 4 kt.
Landing distance: multiply by 1.07.
•Performance:
The following performance penalties are applicable:
‐ Takeoff performance limiting weight is reduced by 3 840 kg (8 466 lb)
‐ Increase V2 and VR by 1 kt
Note: The above performance penalty is not applicable if the flight crew can check
V2 greater than 1.16 VS1G.
‐ If two or more doors are missing, en route performance limiting weight is reduced by
40 kg (89 lb) per missing door
‐ If three or more doors are missing, fuel consumption is increased by 0.09 % per missing
door.
Refer to MCDL-54-03 Illustration Pylon Pressure Relief Door 413(423) BL - 414(424) BR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
GLG A319-112 FLEET MCDL-54-03 P 2/2
AFM B 14 DEC 13
ILLUSTRATION PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
Ident.: MCDL-54-03-00006541.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 54-03 Pylon Pressure Relief Door 413(423) BL - 414(424) BR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
GLG A319-112 FLEET MCDL-54-04 P 1/2
AFM A 25 JAN 11
54-04 Pylon Access Door 415(425) AL - 415(425) AR
Ident.: MCDL-54-04-00006543.0001001 / 23 NOV 09 APPROVED
Criteria: SA
54-04 Quantity installed
PYLON ACCESS DOOR 415(425) AL - 415(425) AR –
All may be missing for 5 flight cycles provided the hole is covered with high speed tape.
•Limitations:
Flight in forecasted thunderstorm conditions is not allowed.
Refer to MCDL-54-04 Illustration Pylon Access Door 415(425) AL - 415(425) AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
GLG A319-112 FLEET MCDL-54-04 P 2/2
AFM B 25 JAN 11
ILLUSTRATION PYLON ACCESS DOOR 415(425) AL - 415(425) AR
Ident.: MCDL-54-04-00006544.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 54-04 Pylon Access Door 415(425) AL - 415(425) AR
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON FAIRING SEAL
GLG A319-112 FLEET MCDL-54-05 P 1/4
AFM A to B 19 NOV 14
54-05 Pylon Fairing Seal
Ident.: TDU / MCDL-54-05-00015527.0001001 / 29 OCT 14 APPROVED
Criteria: SA
Impacted DU: 00006545 Pylon Fairing Seal
Belongs to TR423 Issue 1
54-05 Quantity installed
PYLON FAIRING SEAL 6
One may be missing per pylon.
Refer to MCDL-54-05 Illustration Pylon Fairing Seal
54-05 Pylon Fairing seal
Ident.: MCDL-54-05-00006545.0001001 / 23 NOV 09 APPROVED
Criteria: SA
Impacted by TDU: 00015527 Pylon Fairing Seal
54-05 Quantity installed
PYLON FAIRING SEAL 4
One may be missing per pylon.
Refer to MCDL-54-05 Illustration Pylon Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON FAIRING SEAL
GLG A319-112 FLEET MCDL-54-05 P 2/4
AFM C 19 NOV 14
ILLUSTRATION PYLON FAIRING SEAL
Ident.: TDU / MCDL-54-05-00015528.0001001 / 29 OCT 14 APPROVED
Criteria: SA
Impacted DU: 00006546 Illustration Pylon Fairing Seal
Belongs to TR423 Issue 1
For dispatch conditions:Refer to 54-05 Pylon Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON FAIRING SEAL
GLG A319-112 FLEET MCDL-54-05 P 3/4
AFM D 19 NOV 14
ILLUSTRATION PYLON FAIRING SEAL
Ident.: MCDL-54-05-00006546.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
Impacted by TDU: 00015528 Illustration Pylon Fairing Seal
For dispatch conditions:Refer to 54-05 Pylon Fairing Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
PYLON FAIRING SEAL
Intentionally left blank
GLG A319-112 FLEET MCDL-54-05 P 4/4
AFM 19 NOV 14
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
AERODYNAMIC SEAL
GLG A319-112 FLEET MCDL-54-06 P 1/2
AFM A 14 DEC 13
54-06 Aerodynamic Seal
Ident.: MCDL-54-06-00006547.0001001 / 02 DEC 13 APPROVED
Criteria: SA
54-06 Quantity installed
AERODYNAMIC SEAL 2
(m) Refer to AMM Task 54-53-00-040-001
All may be missing.
Refer to MCDL-54-06 Illustration Aerodynamic Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
AERODYNAMIC SEAL
GLG A319-112 FLEET MCDL-54-06 P 2/2
AFM B 14 DEC 13
ILLUSTRATION AERODYNAMIC SEAL
Ident.: MCDL-54-06-00006548.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 54-06 Aerodynamic Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
WING TIP FENCE
GLG A319-112 FLEET MCDL-57-01 P 1/2
AFM A 12 DEC 17
57-01 Wing Tip Fence
Ident.: MCDL-57-01-00006549.0001001 / 29 NOV 17 APPROVED
Criteria: A319
1a)
57-01 Quantity installed
WING TIP FENCE 2
(m) Refer to AMM Task 57-31-00-040-001
One lower part of a wing tip fence may be missing provided the broken part is removed and
holes are covered.
Note: May be combined with MCDL item 57-05 (Refer to MCDL-57-05 Vortex Generator).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 4 480 kg
(9 877 lb)
‐ En-route performance limiting weight is reduced by 378 kg (834 lb)
‐ Fuel consumption is increased by 0.88 %.
– or –
2b)
57-01 Quantity installed
WING TIP FENCE 2
(m) Refer to AMM Task 57-31-00-040-001
One complete wing tip fence may be missing provided exposed interior structure is covered,
protective material is inspected before each flight and replaced if necessary.
Note: May be combined with MCDL item 57-05 (Refer to MCDL-57-05 Vortex Generator).
•Performance:
The following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 10 080 kg
(22 223 lb)
‐ En-route performance limiting weight is reduced by 756 kg (1 667 lb)
‐ Fuel consumption is increased by 1.69 %.
Refer to MCDL-57-01 Illustration Wing Tip Fence
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
WING TIP FENCE
GLG A319-112 FLEET MCDL-57-01 P 2/2
AFM B 12 DEC 17
ILLUSTRATION WING TIP FENCE
Ident.: MCDL-57-01-00006550.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: SA
For dispatch conditions:Refer to 57-01 Wing Tip Fence
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
BELLY FAIRING SLIDING PANEL
GLG A319-112 FLEET MCDL-57-02 P 1/2
AFM A 12 DEC 17
57-02 Belly Fairing Sliding Panel
Ident.: MCDL-57-02-00006551.0002001 / 29 NOV 17 APPROVED
Criteria: (SA and 26495)
1
57-02 Quantity installed
BELLY FAIRING SLIDING PANEL 2
All may be missing.
Note: May be combined with MCDL item 57-06 (Refer to MCDL-57-06 Outer Flap Blade
Seal).
•Performance:
If two panels are missing, the following performance penalties are applicable:
‐ Takeoff and approach climb performance limiting weights are reduced by 96 kg (212 lb)
‐ En route performance limiting weight is reduced by 108 kg (238 lb)
‐ Fuel consumption is increased by 0.28 %.
Refer to MCDL-57-02 Illustration Belly Fairing Sliding Panel
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
BELLY FAIRING SLIDING PANEL
GLG A319-112 FLEET MCDL-57-02 P 2/2
AFM B 12 DEC 17
ILLUSTRATION BELLY FAIRING SLIDING PANEL
Ident.: MCDL-57-02-00006552.0002001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (SA and 26495)
For dispatch conditions:Refer to 57-02 Belly Fairing Sliding Panel
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
OUTBOARD FLAPS RUBBING STRIP
GLG A319-112 FLEET MCDL-57-03 P 1/2
AFM A 25 JAN 11
57-03 Outboard Flap Rubbing Strip Items 10, 15, 20, 40
Ident.: MCDL-57-03-00006564.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
57-03 Quantity installed
OUTBOARD FLAP RUBBING STRIP ITEMS 10, 15, 20, 40 12
All may be missing.
Refer to MCDL-57-03 Illustration Outboard Flap Rubbing Strip
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
OUTBOARD FLAPS RUBBING STRIP
GLG A319-112 FLEET MCDL-57-03 P 2/2
AFM B 25 JAN 11
ILLUSTRATION OUTBOARD FLAP RUBBING STRIP
Ident.: MCDL-57-03-00006565.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 57-03 Outboard Flap Rubbing Strip
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
INBOARD FLAP RUBBING STRIP
GLG A319-112 FLEET MCDL-57-04 P 1/2
AFM A 14 DEC 13
57-04 Inboard Flap Rubbing Strip items 1, 5, 10, 30
Ident.: MCDL-57-04-00006567.0001001 / 23 NOV 09 APPROVED
Criteria: (A318 or A319 or A320)
57-04 Quantity installed
INBOARD FLAP RUBBING STRIP ITEMS 1, 5, 10, 30 8
All may be missing.
Refer to MCDL-57-04 Illustration Inboard Flap Rubbing Strip
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
INBOARD FLAP RUBBING STRIP
GLG A319-112 FLEET MCDL-57-04 P 2/2
AFM B 14 DEC 13
ILLUSTRATION INBOARD FLAP RUBBING STRIP
Ident.: MCDL-57-04-00006568.0001001 / 02 DEC 13 FOR INFORMATION ONLY
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 57-04 Inboard Flap Rubbing Strip
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
OUTER FLAP BLADE SEAL
GLG A319-112 FLEET MCDL-57-06 P 1/2
AFM A 12 DEC 17
57-06 Outer Flap Blade Seal
Ident.: MCDL-57-06-00021897.0001001 / 29 NOV 17 APPROVED
Criteria: (A318 or A319 or A320 or A321)
1
57-06 Quantity installed
OUTER FLAP BLADE SEAL 2
All may be missing.
Note: May be combined with MCDL item 57-02 (Refer to 57-02 Belly Fairing Sliding Panel).
Refer to MCDL-57-06 Illustration Outer Flap Blade Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
WINGS
OUTER FLAP BLADE SEAL
GLG A319-112 FLEET MCDL-57-06 P 2/2
AFM B 12 DEC 17
ILLUSTRATION OUTER FLAP BLADE SEAL
Ident.: MCDL-57-06-00021942.0001001 / 07 SEP 17 FOR INFORMATION ONLY
Criteria: (A318 or A319 or A320)
Belongs to CP116 Issue 1
For dispatch conditions: Refer to 57-06 Outer Flap Blade Seal
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
FRANGIBLE DRAIN MAST
GLG A319-112 FLEET MCDL-71-01 P 1/2
AFM A 14 DEC 13
71-01 Frangible Drain Mast
Ident.: MCDL-71-01-00006569.0001001 / 02 DEC 13 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-115 or 320-111 or 320-214 or 320-215 or 320-216 or 321-111 or 321-112 or
321-211 or 321-212 or 321-213)
71-01 Quantity installed
FRANGIBLE DRAIN MAST 2
(m) Refer to AMM Task 71-71-42-040-045
All may be missing.
Refer to MCDL-71-01 Illustration Frangible Drain Mast
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
FRANGIBLE DRAIN MAST
GLG A319-112 FLEET MCDL-71-01 P 2/2
AFM B 14 DEC 13
ILLUSTRATION FRANGIBLE DRAIN MAST
Ident.: MCDL-71-01-00006570.0001001 / 23 NOV 09 FOR INFORMATION ONLY
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
For dispatch conditions:Refer to 71-01 Frangible Drain Mast
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
FAN COWL HOLD OPEN ROD
GLG A319-112 FLEET MCDL-71-09 P 1/2
AFM A 01 DEC 16
71-09 Fan Cowl Hold Open Rod
Ident.: MCDL-71-09-00006587.0002001 / 02 DEC 13 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
71-09 Quantity installed
FAN COWL HOLD OPEN ROD 8
(m) Refer to AMM Task
All may be missing.
Refer to MCDL-71-09 Illustration Fan Cowl Hold Open Rod
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
FAN COWL HOLD OPEN ROD
GLG A319-112 FLEET MCDL-71-09 P 2/2
AFM B 01 DEC 16
ILLUSTRATION FAN COWL HOLD OPEN ROD
Ident.: MCDL-71-09-00006588.0003001 / 09 NOV 16 FOR INFORMATION ONLY
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
For dispatch conditions:Refer to 71-09 Fan Cowl Hold Open Rod
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
DUCT OPENING ACTUATOR
GLG A319-112 FLEET MCDL-78-01 P 1/2
AFM A 14 APR 15
78-01 Duct Opening Actuator
Ident.: TDU / MCDL-78-01-00016031.0001001 / 20 MAR 15 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Impacted DU: NONE
Belongs to TR499 Issue 1
78-01 Quantity installed
DUCT OPENING ACTUATOR 4
(m) Refer to AMM Task
All may be missing.
Refer to MCDL-78-01 Illustration Duct Opening Actuator
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
DUCT OPENING ACTUATOR
GLG A319-112 FLEET MCDL-78-01 P 2/2
AFM B 14 APR 15
ILLUSTRATION DUCT OPENING ACTUATOR
Ident.: TDU / MCDL-78-01-00016033.0001001 / 20 MAR 15 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
Impacted DU: NONE
Belongs to TR499 Issue 1
For dispatch conditions:Refer to MCDL-78-01 Duct Opening Actuator
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
GLG A319-112 FLEET MCDL-78-09 P 1/2
AFM A 14 DEC 13
78-09 Thrust Reverser 11 and 1 O'clock Struts
Ident.: MCDL-78-09-00006596.0001001 / 02 DEC 13 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
78-09 Quantity installed
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS 4
(m) Refer to AMM Task 78-32-11-040-001
All may be missing.
Note: The affected thrust reverser must be considered inoperative (Refer to
MMEL/MI-78-30 Thrust Reverser).
Refer to MCDL-78-09 Illustration Thrust Reverser 11 and 1 O'clock Struts
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
GLG A319-112 FLEET MCDL-78-09 P 2/2
AFM B 14 DEC 13
ILLUSTRATION THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
Ident.: MCDL-78-09-00006597.0001001 / 02 DEC 13 FOR INFORMATION ONLY
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-111 or 320-211 or 320-212 or 320-214 or
320-215 or 320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
For dispatch conditions:Refer to 78-09 Thrust Reverser 11 and 1 O'clock Struts
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
THRUST REVERSER LOCKOUT FAIRING
GLG A319-112 FLEET MCDL-78-11 P 1/2
AFM A 16 MAR 15
78-11 Thrust Reverser Lockout Fairing
Ident.: MCDL-78-11-00014886.0001001 / 14 JAN 15 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
78-11 Quantity installed
THRUST REVERSER LOCKOUT FAIRING 8
(m) Refer to AMM Task 78-30-00-040-804
All may be missing.
•Performance:
The following performance penalties are applicable:
‐ Takeoff performance limiting weight is reduced by 365 kg (805 lb) per missing item
‐ Approach climb limiting weight is reduced by 260 kg (574 lb) per missing item
‐ If two or more Thrust Reverser lockout fairings are missing, en route performance
limiting weight is reduced by 45 kg (99 lb) per missing item
‐ If two or more Thrust Reverser lockout fairings are missing, fuel consumption is
increased by 0.11% per missing item
Refer to MCDL-78-11 Illustration of the Thrust Reverser Lockout Fairing
A319
AIRPLANE FLIGHT MANUAL
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
THRUST REVERSER LOCKOUT FAIRING
GLG A319-112 FLEET MCDL-78-11 P 2/2
AFM B 16 MAR 15
ILLUSTRATION OF THE THRUST REVERSER LOCKOUT FAIRING
Ident.: MCDL-78-11-00014887.0001001 / 02 DEC 13 APPROVED
Criteria: (318-111 or 318-112 or 319-111 or 319-112 or 319-113 or 319-114 or 319-115 or 320-211 or 320-212 or 320-214 or 320-215 or
320-216 or 321-111 or 321-112 or 321-211 or 321-212 or 321-213)
SUPPLEMENTARY
PERFORMANCE
Intentionally left blank
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
PRELIMINARY PAGES
TABLE OF CONTENTS
GLG A319-112 FLEET SPERF-PLP-TOC P 1/2
AFM 12 DEC 17
SPERF-CONT CONTAMINATED RUNWAY
SPERF-CONT-GEN GENERAL
General.....................................................................................................................................................................A
SPERF-CONT-LIM LIMITATIONS
Limitations................................................................................................................................................................ A
SPERF-CONT-PERF PERFORMANCE
Introduction...............................................................................................................................................................A
Aircraft Configuration............................................................................................................................................... B
Takeoff and Landing Performance..........................................................................................................................C
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
PRELIMINARY PAGES
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET SPERF-PLP-TOC P 2/2
AFM 12 DEC 17
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
GENERAL
GLG A319-112 FLEET SPERF-CONT-GEN P 1/2
AFM A 25 JAN 11
GENERAL
Ident.: SPERF-CONT-GEN-00009415.0001001 / 23 NOV 09 APPROVED
Criteria: SA
This chapter of the AFM gives the performance information for operations on contaminated runways
and the conditions used for their establishment.
Any actual condition different from those listed in this chapter may lead to different performance.
Refer to SPERF-CONT-PERF Aircraft Configuration.
This chapter of the AFM is approved by EASA according to JAR 25 contaminated runway
performance requirements.
This chapter is not required by FAR 25 and is provided for guidance only for those aircraft certificated
according to this requirement.
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
GENERAL
Intentionally left blank
GLG A319-112 FLEET SPERF-CONT-GEN P 2/2
AFM 25 JAN 11
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
LIMITATIONS
GLG A319-112 FLEET SPERF-CONT-LIM P 1/2
AFM A 08 APR 11
LIMITATIONS
Ident.: SPERF-CONT-LIM-00009416.0001001 / 04 APR 11 APPROVED
Criteria: SA
Reduced thrust takeoff is not allowed on contaminated runways.
Takeoff on very low braking friction surface (icy runway) is not recommended.
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET SPERF-CONT-LIM P 2/2
AFM 08 APR 11
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
PERFORMANCE
GLG A319-112 FLEET SPERF-CONT-PERF P 1/2
AFM A to C 12 DEC 17
INTRODUCTION
Ident.: SPERF-CONT-PERF-00009417.0001001 / 23 NOV 09 APPROVED
Criteria: SA
The considered atmosphere is the international standard atmosphere.
Performance are related to VS1G.
Wind speed is measured at the height of 10 m.
AIRCRAFT CONFIGURATION
Ident.: SPERF-CONT-PERF-00009441.0001001 / 07 NOV 17 APPROVED
Criteria: SA
TAKEOFF ON CONTAMINATED RUNWAY
The takeoff performance has been established for slats/flaps configuration 1, 2 and 3 on runways
contaminated by:
‐ 6 mm and 13 mm of water
‐ 6 mm and 13 mm of slush
‐ 10 mm and 100 mm of dry snow
‐ 5 mm, 15 mm, and 30 mm of wet snow
‐ Compacted snow
‐ Icy
Ground spoilers are armed.
Accelerate Stop Distance (ASD) determination is made with or without thrust reversers and
considering the use of ground spoilers and wheel brakes with anti-skid on.
LANDING DISTANCE ON VERY LOW BRAKING FRICTION SURFACE
Advisory landing distance on very low braking friction surface such as icy runway has been
established for slats/flaps configuration 3 and FULL.
Ground spoilers are armed.
Landing distance determination is made with or without thrust reversers and considering the use of
ground spoilers and wheel brakes with anti-skid on.
TAKEOFF AND LANDING PERFORMANCE
Ident.: SPERF-CONT-PERF-00009429.0001001 / 23 NOV 09 APPROVED
Criteria: SA
For takeoff and landing performance determination on contaminated runways, the Performance
Engineer's Programs/AFM_OCTO approved FM module at the latest approved revision must be
used. Refer to PERF-OCTO Performance Database.
A319
AIRPLANE FLIGHT MANUAL
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
PERFORMANCE
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GLG A319-112 FLEET SPERF-CONT-PERF P 2/2
AFM 12 DEC 17
