AFM M2K 005 AIRCRAFT FLIGHT MANUAL 319 112 2K
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TRANSMITTAL LETTER
A319
AIRPLANE FLIGHT MANUAL
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
GLG A319-112 FLEET
AFM
TRL P 1/2
12 DEC 17
TRANSMITTAL LETTER
A319
AIRPLANE FLIGHT MANUAL
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GLG A319-112 FLEET
AFM
TRL P 2/2
12 DEC 17
FILING INSTRUCTIONS
A319
AIRPLANE FLIGHT MANUAL
Please incorporate this revision as follow:
Localization
Subsection Title
PLP-LESS
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
PLP-LEDU
LIST OF EFFECTIVE DOCUMENTARY UNITS
PLP-LAR
LIST OF APPROVAL REFERENCES
APPRO-PLP-TOC
TABLE OF CONTENTS
APPRO-PLP-SOH
SUMMARY OF HIGHLIGHTS
PERF-PLP-TOC
TABLE OF CONTENTS
PERF-PLP-SOH
SUMMARY OF HIGHLIGHTS
PERF-OCTO
PERFORMANCE DATABASE
MCDL-PLP-TOC
TABLE OF CONTENTS
MCDL-PLP-SOH
SUMMARY OF HIGHLIGHTS
MCDL-27-01
Flap Track Fairing
MCDL-27-03
Slat Track Closing Plate
MCDL-27-08
Seal Between Inboard and Outboard Flap
MCDL-27-16
Flap Track Moveable Fairing Pivot Cover
MCDL-28-01
Refuel/Defuel Coupling Cap 101 QM Or 41 QM
MCDL-28-02
Refuel Panel Door 192MB
MCDL-33-02
Taxi Light Lamp 8LR
MCDL-33-07
Landing Light Lens 7LB, 8LB
MCDL-52-05
Access Door to Air Conditioning Ground Supply 191 CB
GLG A319-112 FLEET
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Rev. Date
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12 DEC 17
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12 DEC 17
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Continued on the following page
FI P 1/2
12 DEC 17
FILING INSTRUCTIONS
A319
AIRPLANE FLIGHT MANUAL
Localization
Subsection Title
MCDL-52-21
Blue Hydraulic Access Door 197 FB
MCDL-57-01
Wing Tip Fence
MCDL-57-02
Belly Fairing Sliding Panel
MCDL-57-06
Outer Flap Blade Seal
SPERF-PLP-TOC
TABLE OF CONTENTS
SPERF-CONT-PERF
PERFORMANCE
GLG A319-112 FLEET
AFM
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Rev. Date
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12 DEC 17
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12 DEC 17
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12 DEC 17
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PRELIMINARY PAGES
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PRELIMINARY PAGES
TABLE OF CONTENTS
A319
AIRPLANE FLIGHT MANUAL
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
GLG A319-112 FLEET
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07 MAR 17
PRELIMINARY PAGES
TABLE OF CONTENTS
A319
AIRPLANE FLIGHT MANUAL
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07 MAR 17
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
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Localization
Subsection Title
Rev. Date
APPRO-TR
GEN-INTR
GEN-DESC
GEN-DEF
GEN-ABB
GEN-UNIT
GEN-VIEW
LIM-GEN
LIM-WGHT
LIM-SPD
LIM-OPS
LIM-09
LIM-21
LIM-22-FMS
LIM-22-FGS
LIM-24
LIM-28
LIM-29
LIM-32
LIM-34
LIM-46
LIM-49
LIM-70
EMER-GEN
EMER-21
EMER-24
EMER-26
EMER-27
EMER-29
EMER-32
EMER-34
EMER-70
EMER-90
ABN-GEN
ABN-OEI-TO
ABN-OEI-LDG
ABN-21
ABN-22-AUTOFLT
ABN-22-CATII
TEMPORARY REVISIONS
14 NOV 17
INTRODUCTION
07 FEB 17
AFM DESCRIPTION
07 FEB 17
WORDING DEFINITIONS
16 MAR 15
ABBREVIATIONS
16 MAR 15
UNITS
25 JAN 11
3-VIEW DRAWING
08 APR 11
GENERAL
14 DEC 13
WEIGHTS AND LOADING
25 JAN 11
AIRSPEEDS
25 JAN 11
OPERATIONAL PARAMETERS
25 JAN 11
TOWING AND TAXIING
30 JUL 15
AIR COND/PRESS/VENT
25 JAN 11
Flight Management System
14 APR 17
Flight Guidance System
10 OCT 17
ELECTRICAL POWER
25 JAN 11
FUEL
12 SEP 17
HYDRAULIC
25 JAN 11
LANDING GEAR
25 JAN 11
NAVIGATION
14 NOV 17
INFORMATION SYSTEMS
25 JAN 11
AUXILIARY POWER UNIT
25 JAN 11
POWER PLANT
13 JUN 17
GENERAL
08 AUG 17
AIR COND/PRESS/VENT
14 DEC 13
ELECTRICAL POWER
14 DEC 13
FIRE/SMOKE
16 MAR 15
FLIGHT CONTROLS
14 DEC 13
HYDRAULIC
14 DEC 13
LANDING GEAR
25 AUG 15
NAVIGATION
06 JAN 15
POWER PLANT
25 JAN 11
MISCELLANEOUS
12 SEP 17
GENERAL
08 AUG 17
TAKEOFF
16 MAR 15
APPROACH AND LANDING
14 DEC 13
AIR COND/PRESS/VENT
05 DEC 11
AUTO FLIGHT SYSTEM
13 JUN 17
FAILURES OR WARNINGS DURING A CAT II APPROACH WITH
25 JAN 11
OR WITHOUT AUTOMATIC LANDING
Continued on the following page
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PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
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ABN-22-CATIIIDH
ABN-22-CATIIInoDH
R
ABN-24
ABN-27
ABN-28
ABN-29
ABN-30
ABN-31
ABN-32
ABN-34
ABN-36
ABN-52
ABN-70
ABN-90
NORM-GEN
NORM-PFLT
NORM-TO
NORM-FLT
NORM-LDG
NORM-22-CONF
NORM-22-NPA
NORM-22-PA
NORM-28
NORM-30
NORM-34
NORM-49
PERF-GEN
PERF-CAL-TO
PERF-CAL-CRU
PERF-CAL-LDG
PERF-TO
PERF-FLT
PERF-LDG
PERF-OCTO
PERF-ENG
PERF-FLEX
APP-NOI
GLG A319-112 FLEET
AFM
Subsection Title
Rev. Date
FAILURES OR WARNINGS DURING A CAT III APPROACH
25 JAN 11
WITH DH
FAILURES OR WARNINGS DURING A CAT III APPROACH
14 DEC 13
WITH NO DH
ELECTRICAL POWER
10 SEP 14
FLIGHT CONTROLS
08 AUG 17
FUEL
10 SEP 14
HYDRAULIC
14 DEC 13
ICE AND RAIN PROTECTION
16 MAR 15
INDICATING/RECORDING SYSTEM
14 DEC 13
LANDING GEAR
10 SEP 14
NAVIGATION
11 JUL 17
PNEUMATIC
10 SEP 14
DOORS
08 APR 11
POWER PLANT
22 SEP 15
MISCELLANEOUS
08 APR 11
GENERAL
16 MAR 15
PREFLIGHT CHECKS
10 OCT 17
TAKEOFF
16 MAR 15
FLIGHT
07 MAR 17
APPROACH AND LANDING
25 JAN 11
Demonstrated System Configuration
13 JUN 17
Non Precision Approach
14 DEC 13
Precision Approach
16 MAR 15
FUEL
25 JAN 11
ICE AND RAIN PROTECTION
25 JAN 11
NAVIGATION
13 JUN 17
AUXILIARY POWER UNIT
25 JAN 11
GENERAL
25 JAN 11
TAKEOFF
25 JAN 11
CRUISE (Clean Configuration)
25 JAN 11
LANDING
25 JAN 11
TAKEOFF PERFORMANCE
08 APR 11
IN FLIGHT PERFORMANCE
08 APR 11
LANDING PERFORMANCE
14 DEC 13
PERFORMANCE DATABASE
12 DEC 17
ENGINE MANAGEMENT
25 JAN 11
REDUCED THRUST TAKEOFF
25 JAN 11
EXTERNAL NOISE
25 JAN 11
Continued on the following page
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PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
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Subsection Title
Rev. Date
APP-TCAS
APP-INOP
APP-LGDN-GEN
APP-LGDN-LIM
APP-LGDN-EMER
APP-LGDN-ABN
APP-LGDN-NORM
APP-LGDN-PERF
APP-LGDN-APP
APP-INTX-GEN
APP-INTX-LIM
APP-INTX-ABN
APP-INTX-NORM
APP-HAO-GEN
APP-HAO-LIM
APP-HAO-NORM
APP-HAO-PERF
APP-TAWS
APP-NRWY
APP-PFC
MCDL-GEN-INTR
MCDL-GEN-LIM
MCDL-GEN-PERF
MCDL-21-01
MCDL-21-03
MCDL-23-01
MCDL-27-01
MCDL-27-03
MCDL-27-05
MCDL-27-06
MCDL-27-07
MCDL-27-08
MCDL-27-09
MCDL-27-10
MCDL-27-11
MCDL-27-12
MCDL-27-13
MCDL-27-14
MCDL-27-15
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
12 JAN 17
DISPATCH WITH INOPERATIVE ITEMS
25 JAN 11
GENERAL
25 JAN 11
LIMITATIONS
25 JAN 11
EMERGENCY PROCEDURES
25 JAN 11
ABNORMAL PROCEDURES
25 JAN 11
NORMAL PROCEDURES
25 JAN 11
PERFORMANCE
25 JAN 11
APPENDICES AND SUPPLEMENTS
25 JAN 11
GENERAL
25 JAN 11
LIMITATIONS
25 JAN 11
ABNORMAL PROCEDURES
14 DEC 13
NORMAL PROCEDURES
25 JAN 11
GENERAL
22 SEP 15
LIMITATIONS
12 SEP 17
NORMAL PROCEDURES
22 SEP 15
PERFORMANCE
22 SEP 15
TAWS-GPWS
16 MAR 15
NARROW RUNWAY
08 AUG 17
OPERATIONS ON WET GROOVED/PFC RUNWAYS
25 JAN 11
Introduction
10 OCT 17
Limitations
25 JAN 11
Performance
16 MAR 15
Ram Air Inlet Flap
25 JAN 11
Ram Air Inlet Leading Edge
25 JAN 11
Static Discharger
09 JUL 14
Flap Track Fairing
12 DEC 17
Slat Track Closing Plate
12 DEC 17
Access Panel for Bearings at Elevator
25 JAN 11
Flap Track Fairing Rear Top Cover and Tail Cone
14 DEC 13
Rubber Seal under Slat
14 DEC 13
Seal Between Inboard and Outboard Flap
12 DEC 17
Inboard Aileron Edge to Wing Seal
25 JAN 11
Slat End Seal and Weather Seal
03 MAY 16
Slat Track Filler Block
25 JAN 11
Slat Track Sealing Packer
25 JAN 11
Inter-flap Cushion Seal
25 JAN 11
Flap Track Moveable Fairing Seal
14 DEC 13
Flap Track Fixed Fairing Seal
14 DEC 13
Continued on the following page
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R
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PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
R
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R
R
R
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Localization
MCDL-27-16
MCDL-28-01
MCDL-28-02
MCDL-30-01
MCDL-32-03
MCDL-32-04
MCDL-33-01
MCDL-33-02
MCDL-33-03
MCDL-33-04
MCDL-33-05
MCDL-33-07
MCDL-33-08
MCDL-33-09
MCDL-49-01
MCDL-51-02
MCDL-51-04
MCDL-52-01
MCDL-52-02
MCDL-52-03
MCDL-52-04
R
R
MCDL-52-05
MCDL-52-07
MCDL-52-08
MCDL-52-09
MCDL-52-10
MCDL-52-11
MCDL-52-12
MCDL-52-13
MCDL-52-14
MCDL-52-15
MCDL-52-16
MCDL-52-18
MCDL-52-19
MCDL-52-20
MCDL-52-21
MCDL-52-22
GLG A319-112 FLEET
AFM
Subsection Title
Rev. Date
Flap Track Moveable Fairing Pivot Cover
12 DEC 17
Refuel/Defuel Coupling Cap 101 QM Or 41 QM
12 DEC 17
Refuel Panel Door 192MB
12 DEC 17
Icing Indicator
25 JAN 11
Nose Wheel Hubcap
14 DEC 13
Nose Fitting Towing
14 DEC 13
Wing/Engine Scan light Cover 3LX, 4LX
14 DEC 13
Taxi Light Lamp 8LR
12 DEC 17
Rear Navigation Light Lens 15LA
14 DEC 13
Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light Cover
14 DEC 13
Logo Light Lens (Cover) 3LY, 4LY
14 DEC 13
Landing Light Lens 7LB, 8LB
12 DEC 17
Turn OFF Light Lamp 3LC1, 3LC2
14 DEC 13
Takeoff Light Lamp 7LR
14 DEC 13
APU Overpressure Release Door
25 JAN 11
Passenger Door Scuff Plate
25 JAN 11
Fairing Aft Safety Stay Point 311 AL
25 JAN 11
Toilet Servicing and Drainage Door
07 FEB 17
Access Door to Hydraulic Ground Connectors 197 CB - 197
11 JUL 17
EB - 198 CB
Access Door to Potable Water Filling and Drainage
30 JUL 15
Access Door to Opening Control of Landing Gear Doors on
16 MAR 15
Ground 195 BB - 196 BB
Access Door to Air Conditioning Ground Supply 191 CB
12 DEC 17
External Power Ground Connection Access Door Assy 121 AL
10 OCT 17
Access Door of Cargo Opening System 134 AR - 154 AR
25 JAN 11
Nose Landing Gear Main Door (713, 714)
14 DEC 13
Nose Landing Gear Aft Door (715, 716)
14 DEC 13
Nose Landing Gear Leg Door (712)
14 DEC 13
Main Landing Gear Door (732, 742) (flight with gear up)
14 DEC 13
Main Landing Gear Door (733, 743) (flight with gear up)
14 DEC 13
Main Landing Gear Door (732, 742) (flight with gear down)
14 DEC 13
Main Landing Gear Door (733, 743) (Flight with gear down)
14 DEC 13
Main Landing Gear Door (734, 744) (Flight with gear down)
14 DEC 13
Main Landing Gear Door : Seal on Secondary Hinged Fairing
25 JAN 11
Pax Door Upper Cover Plate
25 JAN 11
Access Door to HP Air Ground Connector 191 DB
16 MAR 15
Blue Hydraulic Access Door 197 FB
12 DEC 17
Forward Cargo Door Access Cover Panel 825 AR
14 DEC 13
Continued on the following page
PLP-LESS P 4/6
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
R
R
R
R
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Localization
MCDL-52-23
MCDL-53-01
MCDL-53-03
MCDL-54-01
MCDL-54-03
MCDL-54-04
MCDL-54-05
MCDL-54-06
MCDL-57-01
MCDL-57-02
MCDL-57-03
MCDL-57-04
MCDL-57-06
MCDL-71-01
MCDL-71-09
MCDL-78-01
MCDL-78-09
MCDL-78-11
SPERF-CONT-GEN
SPERF-CONT-LIM
SPERF-CONT-PERF
Subsection Title
Aft Cargo Door Access Cover Panel 826 AR
Belly Fairing Vent Louver Vane
Root Fillet Fairing
Nacelle Strake
Pylon Pressure Relief Door 413(423) BL - 414(424) BR
Pylon Access Door 415(425) AL - 415(425) AR
Pylon Fairing Seal
Aerodynamic Seal
Wing Tip Fence
Belly Fairing Sliding Panel
Outboard Flaps Rubbing Strip
Inboard Flap Rubbing Strip
Outer Flap Blade Seal
Frangible Drain Mast
Fan Cowl Hold Open Rod
Duct Opening Actuator
Thrust Reverser 11 and 1 O'clock Struts
Thrust Reverser Lockout Fairing
GENERAL
LIMITATIONS
PERFORMANCE
Rev. Date
01 SEP 16
16 MAR 15
14 DEC 13
16 MAR 15
14 DEC 13
25 JAN 11
19 NOV 14
14 DEC 13
12 DEC 17
12 DEC 17
25 JAN 11
14 DEC 13
12 DEC 17
14 DEC 13
01 DEC 16
14 APR 15
14 DEC 13
16 MAR 15
25 JAN 11
08 APR 11
12 DEC 17
(1) Evolution code : N=New, R=Revised, E=Effectivity, M=Moved
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AIRPLANE FLIGHT MANUAL
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(1)
M
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Localization
PLP-LEDU
(2)
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DU Title
DU identification
DU date
List of Effective Documentary Units
12 DEC 17
Approved by Airbus under the authority of DOA ref.
EASA. 21J.031
Heading Approbation A319-112
00007334.0006001
09 APR 96
Approved by
APPRO-HEAD
Approval reference: .
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
00009728.0001001
21 OCT 09
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
Impacted DU: NONE
APPRO-TR
x (TR 2.05.00/47) - Non Precision
00009667.0001001
23 NOV 09
Approaches with OEI
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)
00009670.0001001
23 NOV 09
Flight Testing
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
00014157.0003001
04 NOV 15
ADIRU
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
Continued on the following page
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PLP-LEDU P 1/58
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PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
DU date
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
00016021.0003001
20 MAR 15
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
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
00016654.0001001
06 JUL 15
Water Filling and Drainage
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 2/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 3/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
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(1)
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DU Title
DU identification
DU date
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 4/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 5/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 6/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
00009711.0009001
04 NOV 15
ADIRU
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 7/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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(1)
M
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T
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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
00007359.0001001
23 NOV 09
(RVSM)
Approval reference: 10060714
Approved by EASA
Criteria: (SA and (25861 or 25910 or 25952 or 31039 or 31528))
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 8/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
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(1)
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T
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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
00015177.0001001
14 JUL 17
IN CASE OF IN-FLIGHT FAILURE
Approval reference: 10062618
Approved by EASA
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 9/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
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(1)
M
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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
00006884.0003001
02 DEC 13
GENERATORS FAILED)
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 10/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
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T
Continued from the previous page
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
00007039.0011001
23 NOV 09
FLAME OUT)
Approval reference: 10060714
Approved by EASA
Criteria: (319-111 or 319-112 or 319-115)
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 11/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
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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
00021836.0002001
11 AUG 17
Failure)
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 12/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
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(2)
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Continued from the previous page
DU Title
DU identification
DU date
LANDING DISTANCE DETERMINATION
00015178.0001001
14 JUL 17
IN CASE OF IN-FLIGHT FAILURE
Approval reference: 10062618
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-OEI-TO
ENGINE FAILURE BEFORE V1
00007100.0001001
23 NOV 09
(REJECTED TAKEOFF)
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
00007103.0001001
23 NOV 09
CLIMB OUT
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
00007105.0001001
23 NOV 09
INTERMEDIATE APPROACH
CONFIGURATION)
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
ABN-GEN
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A319
AIRPLANE FLIGHT MANUAL
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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
00009795.0001001
23 NOV 09
(CAT II)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII
Failure Leading to Slats/Flaps less than
00009315.0001001
23 NOV 09
FLAPS 3 (CAT II)
Approval reference: 10060714
Approved by EASA
Continued on the following page
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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DU Title
DU identification
DU date
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII
Antiskid System and/or Nosewheel
00009338.0001001
23 NOV 09
Steering Failure (CAT II)
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
00009349.0001001
23 NOV 09
(CAT II)
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
00009351.0001001
23 NOV 09
one PFD and one ND (CAT II)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATII
Amber "CHECK HDG" Flag on two PFDs
00009352.0001001
23 NOV 09
and on two NDs (CAT II)
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 00009353.0001001
23 NOV 09
(CAT II)
Approval reference: 10060714
Approved by EASA
Continued on the following page
GLG A319-112 FLEET
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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(1)
M
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(2)
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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
00009356.0001001
23 NOV 09
(CAT II)
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
00009360.0001001
23 NOV 09
deg (CAT II)
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 16/58
12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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DU Title
DU identification
DU date
Multiples Failures or Warnings (CAT III
00009366.0001001
23 NOV 09
with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Failure Leading to Slats/Flaps less than
00009383.0001001
23 NOV 09
CONF 3 (CAT III with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Nosewheel Steering Failure (CAT III with
00009382.0001001
23 NOV 09
DH)
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
00009377.0001001
23 NOV 09
DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Amber "CHECK ATT" Flag on two PFDs
00009386.0001001
23 NOV 09
(CAT III with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
ABN-22-CATIIIDH
GLG A319-112 FLEET
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A319
AIRPLANE FLIGHT MANUAL
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DU Title
DU identification
DU date
Red "ATT" Flag on one PFD (CAT III with
00009385.0001001
23 NOV 09
DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Amber "CHECK HDG" Flag on two PFDs
00009376.0001001
23 NOV 09
and two NDs (CAT III with DH)
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 00009375.0001001
23 NOV 09
(CAT III with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Red "SPD" Flag on one PFD (CAT III
00009374.0001001
23 NOV 09
with DH)
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
00009372.0001001
23 NOV 09
A/THR Loss) (CAT III with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
Total Loss of A/THR ("CAT 3" Decreases
00009384.0001001
23 NOV 09
to "CAT 2") (CAT III with DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIIDH
LOC or G/S Excessive Deviation on PFD
00009371.0001001
23 NOV 09
(CAT III with DH)
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
ABN-22-CATIIIDH
GLG A319-112 FLEET
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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Continued from the previous page
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
00009368.0001001
23 NOV 09
deg (CAT III with DH)
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
00009393.0001001
23 NOV 09
DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
Failure Leading to Slats/Flaps less than
00009394.0001001
23 NOV 09
CONF 3 (CAT III no DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
Nosewheel Steering Failure (CAT III no
00009395.0001001
23 NOV 09
DH)
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
GLG A319-112 FLEET
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12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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(1)
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Continued from the previous page
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
00009399.0001001
23 NOV 09
DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
Amber "CHECK ATT" Flag on two PFDs
00009400.0001001
23 NOV 09
(CAT III no DH)
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
00009401.0001001
23 NOV 09
DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
Amber "CHECK HDG" Flag on two PFDs
00009402.0001001
23 NOV 09
and two NDs (CAT III no DH)
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 00009403.0001001
23 NOV 09
(CAT III no DH)
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
00009404.0001001
23 NOV 09
DH)
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
GLG A319-112 FLEET
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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(1)
M
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T
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DU Title
DU identification
DU date
Capability Decrease (Except if due to
00009406.0001001
23 NOV 09
A/THR Loss) (CAT III no DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
Total Loss of A/THR ("CAT 3" Decreases
00009407.0001001
23 NOV 09
to "CAT 2") (CAT III no DH)
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-22-CATIIInoDH
LOC or G/S Excessive Deviation on PFD
00009408.0001001
23 NOV 09
(CAT III no DH)
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
00009411.0001001
23 NOV 09
deg (CAT III no DH)
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
ABN-22-CATIIInoDH
GLG A319-112 FLEET
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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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
GLG A319-112 FLEET
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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
APPROVED
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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
00006879.0005001
02 DEC 13
LANDING DISTANCE MULTIPLICATION
FACTOR
Approval reference: 10060714
Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
ABN-27
PERFORMANCE LIMITATION FOR
00007110.0003001
03 AUG 10
LANDING IN CLEAN CONFIGURATION
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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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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A319
AIRPLANE FLIGHT MANUAL
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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
00007201.0001001
23 NOV 09
OUTER) TK HI TEMP
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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A319
AIRPLANE FLIGHT MANUAL
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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
00007178.0001001
23 NOV 09
FAULT
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)
00009388.0002001
23 NOV 09
(F/O + STBY) PITOT HEAT FAULT
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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A319
AIRPLANE FLIGHT MANUAL
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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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A319
AIRPLANE FLIGHT MANUAL
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DU Title
ABN-34
NAV IR DISAGREE
Approval reference: 10060714
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34
NAV - ADR 1+2 FAULT
Approval reference: SA01D17016179
Criteria: SA
Applicable to: MSN 1882, 2078
ABN-34
NAV - ADR 1+3 FAULT
Approval reference: SA01D17016179
Criteria: (SA and 37871)
Applicable to: MSN 1882, 2078
ABN-34
NAV - ADR 2+3 FAULT
Approval reference: SA01D17016179
DU identification
00007214.0001001
Approved by EASA
DU date
23 NOV 09
00007186.0001001
15 MAY 17
Approved by Airbus under the authority of DOA ref.
EASA.21J.031
00007187.0002001
15 MAY 17
Approved by Airbus under the authority of DOA ref.
EASA.21J.031
00009566.0002001
15 MAY 17
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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12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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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
00009732.0001001
21 OCT 09
on ground
Approval reference: 10027686
Approved by EASA
Continued on the following page
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A319
AIRPLANE FLIGHT MANUAL
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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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A319
AIRPLANE FLIGHT MANUAL
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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
00007183.0001001
23 NOV 09
ENGINES OPERATIVE
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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12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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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12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
00009469.0001001
23 NOV 09
Approach
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 00009472.0003001
23 NOV 09
Initiation
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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12 DEC 17
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DU Title
DU identification
DU date
CAT II and CAT III Approach and/or
00009482.0001001
23 NOV 09
Automatic Landing
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
00009476.0001001
14 JAN 15
III Approach and Landing
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
00007081.0001001
23 NOV 09
(GPWS)
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
00009175.0002001
23 NOV 09
(RVSM)
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
00009761.0001001
23 NOV 09
System
Approval reference: 10060714
Approved by EASA
Criteria: (SA and 22249)
Applicable to: MSN 1882, 2078
Continued on the following page
NORM-22-PA
GLG A319-112 FLEET
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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
00007267.0001001
03 AUG 10
Takeoff and Landing
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 35/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
00006996.0001001
23 NOV 09
Definition
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 36/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
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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
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 37/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
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T
Continued from the previous page
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
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 38/58
12 DEC 17
PRELIMINARY PAGES
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A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
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T
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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
00007089.0001001
02 DEC 13
SAC/DAC intermix
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
00009652.0001001
23 NOV 09
SAC-TI intermix
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
GLG A319-112 FLEET
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12 DEC 17
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DU Title
Applicable to: MSN 1882, 2078
APP-HAO-LIM
Environmental Envelope
Approval reference: D01FM1703037
DU identification
DU date
00007112.0093001
11 AUG 17
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 40/58
12 DEC 17
PRELIMINARY PAGES
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A319
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APP-NRWY
Performance
Approval reference: 10060714
Criteria: (SA and 30397)
Applicable to: MSN 1882, 2078
APP-PFC
General
Approval reference: 10060714
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
APP-PFC
Performance
Approval reference: 10060714
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
MCDL-GEN-INTR
Introduction
Approval reference: SA03D17033085
Continued from the previous page
DU Title
DU identification
DU date
00006986.0002001
Approved by EASA
23 NOV 09
00007028.0001001
Approved by EASA
23 NOV 09
00007029.0001001
Approved by EASA
23 NOV 09
00006202.0001001
02 OCT 17
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
00006205.0001001
23 NOV 09
Airplane Flight Manual MCDL Chapter
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-GEN-PERF
Performance Penalties calculated with
00006206.0001001
14 JAN 15
AFM_OCTO Software
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
GLG A319-112 FLEET
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PLP-LEDU P 41/58
12 DEC 17
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A319
AIRPLANE FLIGHT MANUAL
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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
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
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
00006244.0001001
23 NOV 09
elevator
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-27-06
Flap Track Fairing Rear Top Cover and
00006245.0001001
02 DEC 13
Tail Cone
Approval reference: 10060714
Approved by EASA
Criteria: SA
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 42/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
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(2)
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DU Title
DU identification
DU date
Applicable to: MSN 1882, 2078
MCDL-27-06
Illustration Flap track fairing rear top
00006246.0001001
23 NOV 09
cover and tail cone
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
MCDL-27-08
Seal Between Inboard and Outboard
00006250.0001001
29 NOV 17
Flap
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
00006251.0001001
23 NOV 09
Outboard Flap
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
00006255.0001001
24 NOV 15
Seal
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 43/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
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(2)
T
Continued from the previous page
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
00006262.0001001
23 NOV 09
seal
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
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
00006266.0001001
23 NOV 09
Pivot Cover
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 44/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
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(2)
T
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DU Title
DU identification
DU date
Refuel/Defuel Coupling Cap 101 QM Or
00006282.0001001
29 NOV 17
41 QM
Approval reference: 10063916
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-28-01
Illustration Refuel/Defuel Coupling Cap
00006283.0001001
23 NOV 09
101 QM or 41 QM
Criteria: SA
Applicable to: MSN 1882, 2078
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
MCDL-28-01
GLG A319-112 FLEET
AFM
PLP-LEDU P 45/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
R
Localization
MCDL-33-01
(2)
T
Continued from the previous page
DU Title
Illustration Wing/Engine Scan light
Cover 3LX, 4LX
DU identification
00006302.0001001
DU date
23 NOV 09
Criteria: SA
Applicable to: MSN 1882, 2078
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
00006306.0001001
23 NOV 09
15LA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-04
Upper 7LV and Lower 6LV Anti-collision
00006307.0001001
02 DEC 13
(Beacon) Light Cover
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-33-04
Illustration Upper and Lower
00006308.0001001
23 NOV 09
Anti-Collision ( Beacon) Light Cover
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, 00006310.0001001
23 NOV 09
4LY
Criteria: SA
Applicable to: MSN 1882, 2078
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 46/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
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,
00006325.0001001
23 NOV 09
3LC2
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
00006330.0001001
23 NOV 09
Door
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
00006339.0001001
23 NOV 09
311AL
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 47/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
DU date
Toilet Servicing and Drainage Door 172
00006441.0003001
23 JAN 17
AR
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
00006442.0002001
23 NOV 09
Drainage Door
Criteria: (SA and 20109)
Applicable to: MSN 1882, 2078
MCDL-52-02
Access Door To Hydraulic Ground
00006447.0001001
16 JUN 17
Connectors 197 CB - 197 EB - 198 CB
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
00006449.0001001
24 NOV 15
Ground Connectors 197 CB - 197 EB 198 CB
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-03
x Access Door To Potable Water Filling
00016655.0001001
06 JUL 15
And Drainage 133 AL - 171 AL
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
00006452.0001001
14 JAN 15
And Drainage 133 AL - 171 AL - 192 NB
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
00016656.0001001
06 JUL 15
Water Filling and Drainage
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
MCDL-52-01
GLG A319-112 FLEET
AFM
PLP-LEDU P 48/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
DU date
Illustration Access Door to Potable
00006453.0001001
23 NOV 09
Water Filling and Drainage
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
00006455.0001001
14 JAN 15
Landing Gear Doors On Ground 195 BB
- 196 BB
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
00006456.0001001
03 AUG 10
control of landing gear doors on ground
195 BB - 196 BB
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-05
Access Door To Air Conditioning
00006457.0001001
29 NOV 17
Ground Supply 191 CB
Approval reference: 10063916
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-05
Illustration Access door to air
00006458.0001001
23 NOV 09
conditionning ground supply 191 CB
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-07
External Power Ground Connection
00006461.0001001
02 OCT 17
Access Door Assy 121 AL
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
00006462.0001001
23 NOV 09
Connection Access Door Assy 121 AL
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-08
Access Door Of Cargo Opening System
00006463.0001001
23 NOV 09
134 AR - 154 AR
Approval reference: 10060714
Approved by EASA
Criteria: (A318 or A319 or A320)
Applicable to: MSN 1882, 2078
Continued on the following page
MCDL-52-03
GLG A319-112 FLEET
AFM
PLP-LEDU P 49/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
MCDL-52-08
(2)
T
Continued from the previous page
DU Title
Illustration Access Door of Cargo
Opening System 134 AR - 154 AR
DU identification
00006464.0001001
DU date
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
00006466.0001001
23 NOV 09
Door (713, 714)
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
00006468.0001001
23 NOV 09
(715, 716)
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
00006472.0001001
23 NOV 09
(712)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-12
Main Landing Gear Door (732, 742)
00006473.0001001
02 DEC 13
(flight with gear up)
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
00006474.0001001
23 NOV 09
(732, 742)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-13
Main Landing Gear Door (733, 743)
00006487.0001001
02 DEC 13
(flight with gear up)
Approval reference: 10060714
Approved by EASA
Criteria: (A319 or A320 or A321)
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 50/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
DU date
Applicable to: MSN 1882, 2078
MCDL-52-13
Illustration Main Landing Gear Door
00006488.0001001
23 NOV 09
(733, 743)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-14
Main Landing Gear Door (732, 742)
00006475.0001001
02 DEC 13
(Flight with gear down)
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
00006476.0001001
23 NOV 09
(732, 742)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-15
Main Landing Gear Door (733, 743)
00006489.0001001
02 DEC 13
(Flight with gear down)
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
00006490.0001001
23 NOV 09
(733, 743)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-16
Main Landing Gear Door (734, 744)
00006491.0001001
02 DEC 13
(Flight with gear down)
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
00006492.0001001
23 NOV 09
(734, 744)
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-18
Main Landing Gear Door : Seal On
00006479.0001001
23 NOV 09
Secondary Hinged Fairing
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-18
Illustration Main Landing Gear Door :
00006480.0001001
23 NOV 09
Seal on Secondary Hinged Fairing
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 51/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
Localization
(2)
T
Continued from the previous page
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
00006483.0001001
14 JAN 15
Connector 191 DB
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-20
Illustration Access Door to HP Air
00006484.0001001
23 NOV 09
Ground Connector 191 DB
Criteria: SA
Applicable to: MSN 1882, 2078
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
00007450.0001001
23 NOV 09
197 FB
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-22
Forward Cargo Door Access Cover
00007451.0001001
02 DEC 13
Panel 825 AR
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-22
Illustration Forward Cargo Door Access
00007452.0001001
23 NOV 09
Cover Panel 825 AR
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-23
Aft Cargo Door Access Cover Panel 826
00007453.0001001
02 DEC 13
AR
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-52-23
Illustration Aft Cargo Door Access
00007454.0002001
17 AUG 16
Cover Panel 826 AR
Criteria: A319
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 52/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
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
00006513.0001001
23 NOV 09
Vane
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
00006540.0003001
02 DEC 13
- 414(424) BR
Approval reference: 10060714
Approved by EASA
Criteria: A319
Applicable to: MSN 1882, 2078
MCDL-54-03
Illustration Pylon Pressure Relief Door
00006541.0001001
23 NOV 09
413(423) BL - 414(424) BR
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-04
Pylon Access Door 415(425) AL 00006543.0001001
23 NOV 09
415(425) AR
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
MCDL-54-04
Illustration Pylon Access Door 415(425)
00006544.0001001
23 NOV 09
AL - 415(425) AR
Criteria: SA
Applicable to: MSN 1882, 2078
Continued on the following page
GLG A319-112 FLEET
AFM
PLP-LEDU P 53/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
R
Localization
(2)
T
Continued from the previous page
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
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
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 54/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
DU date
Outboard Flap Rubbing Strip Items 10,
00006564.0001001
23 NOV 09
15, 20, 40
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,
00006567.0001001
23 NOV 09
10, 30
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
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
MCDL-57-03
GLG A319-112 FLEET
AFM
PLP-LEDU P 55/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
Localization
(2)
T
Continued from the previous page
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
00006597.0001001
02 DEC 13
O'clock Struts
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
00014887.0001001
02 DEC 13
Lockout Fairing
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
GLG A319-112 FLEET
AFM
PLP-LEDU P 56/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
R
Localization
(2)
T
Continued from the previous page
DU Title
DU identification
SPERF-CONT-PERF
Introduction
00009417.0001001
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
SPERF-CONT-PERF
Aircraft Configuration
00009441.0001001
Approval reference: 10063632
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
SPERF-CONT-PERF
Takeoff and Landing Performance
00009429.0001001
Approval reference: 10060714
Approved by EASA
Criteria: SA
Applicable to: MSN 1882, 2078
DU date
23 NOV 09
07 NOV 17
23 NOV 09
(1) Evolution code : N=New, R=Revised, E=Effectivity
(2) Temporary information
GLG A319-112 FLEET
AFM
PLP-LEDU P 57/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE DOCUMENTARY UNITS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PLP-LEDU P 58/58
12 DEC 17
PRELIMINARY PAGES
LIST OF EFFECTIVE TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
TR identification TR approval
date
TR1 issue 1
23 NOV 09
Approval reference: 10027986
Criteria: SA
Applicable to: MSN 1882, 2078
TR6 issue 1
23 NOV 09
TR Title
(TR 2.05.00/47) - Non Precision Approaches
with OEI
Approved by EASA
Deleted by
Mod 37665 for A318/A320
or Mod 153286 for A321
(TR 2.05.00/67) - Ram Air Turbine (RAT) Flight
Mod 28413 or Mod
Testing
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
GLG A319-112 FLEET
AFM
PLP-LETR P 1/2
14 NOV 17
PRELIMINARY PAGES
LIST OF EFFECTIVE TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
APPROVED
(1)
M
TR identification TR approval
date
TR Title
Continued from the previous page
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
GLG A319-112 FLEET
AFM
PLP-LETR P 2/2
14 NOV 17
PRELIMINARY PAGES
LIST OF APPROVAL REFERENCES
A319
AIRPLANE FLIGHT MANUAL
Approval Date
Approval Reference
29 NOV 17
10 NOV 17
10063916
SA03D17036154
07 NOV 17
02 OCT 17
10063632
SA03D17033085
07 SEP 17
D03D17028536
11 AUG 17
D01FM1703037
11 AUG 17
D01FM1703948
03 AUG 17
14 JUL 17
16 JUN 17
10062810
10062618
SA52FM1703062
15 MAY 17
SA01D17016179
11 MAY 17
28 MAR 17
10061833
SA22FM1701636
13 MAR 17
14 FEB 17
10061213
FM1700589
23 JAN 17
SA52D17001991
16 JAN 17
16 JAN 17
10060714
10060714
GLG A319-112 FLEET
AFM
Approved By
EASA
Airbus under the authority
of DOA ref. EASA.21J.031
EASA
Airbus under the authority
of DOA ref. EASA.21J.031
Airbus under the authority
of DOA ref. EASA.21J.031
Airbus under the authority
of DOA ref. EASA.21J.031
Airbus under the authority
of DOA ref. EASA.21J.031
EASA
EASA
Airbus under the authority
of DOA ref. EASA.21J.031
Airbus under the authority
of DOA ref. EASA.21J.031
EASA
Airbus under the authority
of DOA ref. EASA.21J.031
EASA
Airbus under the authority
of DOA ref. EASA.21J.031
Airbus under the authority
of DOA ref. EASA.21J.031
EASA
EASA
PLP-LAR P 1/2
12 DEC 17
PRELIMINARY PAGES
LIST OF APPROVAL REFERENCES
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PLP-LAR P 2/2
12 DEC 17
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
CRITERION
Linked SB
20024
Applicable to: MSN 1882, 2078
20067
Incorp. Date
Title
14 DEC 10
FUEL- INSTALL A CENTRE TANK SYSTEM-
14 DEC 10
Applicable to: MSN 1882, 2078
20069
FIRE PROTECTION - FWD CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM -
14 DEC 10
Applicable to: MSN 1882, 2078
20109
FIRE PROTECTION - AFT CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM -
14 DEC 10
Applicable to: MSN 1882, 2078
21566
WATER/WASTE- INSTALL VACUUM TOILET SYSTEM
-
14 DEC 10
ICE AND RAIN PROTECTION - MODIFY AIR BLEED
SYSTEM TO PROVIDE LOW TEMPERATURE
WARNING-
14 DEC 10
AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION
14 DEC 10
Applicable to: MSN 1882, 2078
24414
HYDRAULIC POWER - AUXILIARY HYDRAULIC
POWER - INTRODUCE A321 RAM AIR TURBINE
14 DEC 10
Applicable to: MSN 1882, 2078
25294
AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU)
DELETE "EXPEDITE" FUNCTION FROM FCU
14 DEC 10
Applicable to: MSN 1882, 2078
25328
NAVIGATION - ADIRS - INSTALL HONEYWELL ADIRS
CAPABLE OF A319 A/C
14 DEC 10
Applicable to: MSN 1882, 2078
25615
GENERAL - DESIGN WEIGHTS - INCREASED
MAXIMUM TAKE-OFF WEIGHT (MTOW) TO 70.0 T
22 SEP 15
CERTIFICATION - GENERAL - CERTIFICATION FOR
HIGH ALTITUDE AIRPORT OPERATION
14 DEC 10
POWER PLANT-GENERAL-INTRODUCE CFM56-5B/P
14 DEC 10
NAVIGATION-REDUCED VERTICAL SEPARATION
MINIMUM (RVSM) (CERTIFICATION APPLICABLE ON
A319/A320 ONLY)
14 DEC 10
A.P.U.-POWER PLANT-INTRODUCE ALLIED SIGNAL
APU 131-9(A)
Applicable to: MSN 1882, 2078
22249
Applicable to: MSN 1882, 2078
22803
Applicable to: MSN 1882, 2078
25800
Applicable to: MSN 1882, 2078
25861
Applicable to: MSN 1882, 2078
25888
Applicable to: MSN 1882, 2078
GLG A319-112 FLEET
AFM
Continued on the following page
PLP-LOM P 1/4
08 AUG 17
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
Continued from the previous page
CRITERION
26001
Linked SB
Incorp. Date
Title
14 DEC 10
Applicable to: MSN 1882, 2078
26363
NAVIGATION-ADIRS-INTRODUCE HONEYWELL 4
MCU P/N AC09
14 DEC 10
Applicable to: MSN 1882, 2078
26495
AIR CONDITIONING-AIR COOLING SYSTEMINTRODUCE MODIFIED RAM AIR OUTLET
14 DEC 10
Applicable to: MSN 1882, 2078
26526
WINGS-INBOARD FLAP-MODIFY SLIDING PANEL
DRIVING MECHANISM
14 DEC 10
Applicable to: MSN 1882, 2078
26999
NAVIGATION - GPWS - ACTIVATE ENHANCED
FUNCTIONS OF THE EGPWS
14 DEC 10
Applicable to: MSN 1882, 2078
27522
NAVIGATION - MMR - INSTALL COLLINS MMR
PROVIDING ILS AND GPS FUNCTION
14 DEC 10
Applicable to: MSN 1882, 2078
27753
INFORMATION SYSTEM - AIR TRAFFIC AND
INFORMATION SYSTEM (ATIMS) - INSTALL ATSU
COMPUTER FOR ACARS
14 DEC 10
Applicable to: MSN 1882, 2078
27772
NAVIGATION - TCAS - INSTALL COLLINS TCAS
TTR921 WITH COLLINS ATC TPR901
14 DEC 10
Applicable to: MSN 1882, 2078
28244
ENGINES-CFM56-5B-FAN FRAME ASSY- INTRODUCE
QC1 PANEL KIT (ACOUSTIC TREATMENT)
14 DEC 10
Applicable to: MSN 1882, 2078
28479
NAVIGATION-GPWS-INTRODUCE EGPWS P/N
206-206 AND INHIBIT AUTOMATIC DEACTIVATION
ENHANCED FUNCTIONS
14 DEC 10
Applicable to: MSN 1882, 2078
28916
INDICATING RECORDING SYSTEM-FWCINTRODUCE FWC STANDARD H2/E3P
14 DEC 10
Applicable to: MSN 1882, 2078
30397
INDICATING RECORDING SYSTEM-FWS INTRODUCE
FWC STANDARD H1PE3P
21 MAR 12
Applicable to: MSN 1882, 2078
30660
CERTIFICATION DOCUMENTS - GENERAL - CERTIFY
AIRCRAFT FOR OPERATION ON RUNWAYS LESS
THAN 45M WIDTH
14 DEC 10
INDICATING/RECORDING SYSTEMS - FWC - INSTALL
FWC STANDARD H2E4
Applicable to: MSN 1882, 2078
GLG A319-112 FLEET
AFM
Continued on the following page
PLP-LOM P 2/4
08 AUG 17
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
Continued from the previous page
CRITERION
30748
Linked SB
Incorp. Date
Title
14 DEC 10
Applicable to: MSN 1882, 2078
30941
GENERAL-FLIGHT ENVIRONMENTAL ENVELOPEEXTENSION TO 12100 M (39800 FT)
14 DEC 10
Applicable to: MSN 1882, 2078
31276
NAVIGATION-ADIRU-INSTALL HONEYWELL ADIR U 4
MCU AD11 (NEW HARD)
14 DEC 10
Applicable to: MSN 1882, 2078
31283
ELECTRICAL POWER - GENERAL - INSTALL A
COMMERCIAL SHEDDING PUSH-BUTTON SWITCH IN
COCKPIT
14 DEC 10
Applicable to: MSN 1882, 2078
31528
INDICATING RECORDING SYSTEM-FWCINTRODUCE FWC STANDARD H2 F1
14 DEC 10
Applicable to: MSN 1882, 2078
31896
NAVIGATION-ADIRU-RESTORE RVSM 3 CIRCUIT
CAPABILITIES (SERIAL SOLUTION)
14 DEC 10
Applicable to: MSN 1882, 2078
32619
AUTOFLIGHT-FMGC-INSTALL FMGC CFM
C13042AA01 (EQUIPPED WITH FMS2) HONEYWELL
14 DEC 10
Applicable to: MSN 1882, 2078
33239
ENGINE FUEL AND CONTROL - FADEC SYSTEM
INTRODUCE NEW FADEC SOFTWARE "5BK" ON SAC
CFM56-5B ENGINES
14 DEC 10
Applicable to: MSN 1882, 2078
35220
ENGINE FUEL AND CONTROL - FADEC SYSTEM INSTALL "5BL" STANDARD ECU SOFTWARE FOR
CFM56-5B ENGINES (A318 CAPABLE)
05 DEC 11
Applicable to: MSN 1882, 2078
37871
INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2F3
05 DEC 11
Applicable to: MSN 1882, 2078
150110
INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F5
05 DEC 11
Applicable to: MSN 1882, 2078
151269
AUTO FLIGHT- FLIGHT MANAGEMENT SYSTEMACTIVATE BARO RADIO SETTING FUNCTION
11 APR 14
INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD H2-F6
Applicable to: MSN 1882, 2078
GLG A319-112 FLEET
AFM
Continued on the following page
PLP-LOM P 3/4
08 AUG 17
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A319
AIRPLANE FLIGHT MANUAL
(1)
M
Continued from the previous page
CRITERION
152830
Linked SB
Incorp. Date
Title
03 NOV 16
Applicable to: MSN 1882, 2078
153741
NAVIGATION-TRAFFIC COLLISION AVOIDANCE
SYSTEM (TCAS) - INSTALL TCAS COLLINS TTR-921
CHANGE 7.1
11 APR 14
Applicable to: MSN 1882, 2078
154473
INDICATING RECORDING SYSTEMS-FWCINTRODUCE FWC STANDARD H2-F7
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
GLG A319-112 FLEET
AFM
PLP-LOM P 4/4
08 AUG 17
APPROVAL DATA
Intentionally left blank
APPROVAL DATA
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
APPRO-PLP-TOC P 1/2
12 DEC 17
APPROVAL DATA
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET
AFM
APPRO-PLP-TOC P 2/2
12 DEC 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR500 Issue 1
ABN - ENG STALL
APPROVED
Ident.: TDU / APPRO-TR-00016179.0001001 / 03 SEP 15
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
GLG A319-112 FLEET
AFM
ABN-70-00016178.0001001/03 SEP 15
A
APPRO-TR P 1/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR562 Issue 1
UNRELIABLE AIRSPEED
APPROVED
Ident.: TDU / APPRO-TR-00009810.0003001 / 11 FEB 16
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
GLG A319-112 FLEET
AFM
ABN-34-00009811.0003001/11 FEB 16
B
APPRO-TR P 2/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR34 Issue 1
(TR 4.02.00/41) - ENG COMPRESSOR VANE/ENG STALL ON GROUND
APPROVED
Ident.: TDU / APPRO-TR-00009728.0001001 / 21 OCT 09
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
GLG A319-112 FLEET
AFM
ABN-70-00009732.0001001/21 OCT 09
C
APPRO-TR P 3/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR1 Issue 1
(TR 2.05.00/47) - NON PRECISION APPROACHES WITH OEI
APPROVED
Ident.: TDU / APPRO-TR-00009667.0001001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
LIM-22-FMS-00009620.0001001/23 NOV 09
D
APPRO-TR P 4/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR6 Issue 1
(TR 2.05.00/67) - RAM AIR TURBINE (RAT) FLIGHT TESTING
Ident.: TDU / APPRO-TR-00009670.0001001 / 23 NOV 09
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Impacted DU: NONE
APPROVED
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
GLG A319-112 FLEET
AFM
LIM-29-00009631.0001001/23 NOV 09
E
APPRO-TR P 5/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR188 Issue 2
AUTOLAND DATABASES WITH HONEYWELL ADIRU
APPROVED
Ident.: TDU / APPRO-TR-00014157.0003001 / 04 NOV 15
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
GLG A319-112 FLEET
AFM
LIM-22-FGS-00009711.0009001/04 NOV 15
F
APPRO-TR P 6/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR423 Issue 1
MCDL 54-05 PYLON FAIRING SEAL
APPROVED
Ident.: TDU / APPRO-TR-00015738.0001001 / 29 OCT 14
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-54-05-00015527.0001001/29 OCT 14
GLG A319-112 FLEET
AFM
MCDL-54-05-00015528.0001001/29 OCT 14
G
APPRO-TR P 7/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR499 Issue 1
MCDL 78-01 DUCT OPENING ACTUATOR FOR CFM ENGINE
APPROVED
Ident.: TDU / APPRO-TR-00016021.0003001 / 20 MAR 15
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-78-01-00016031.0001001/20 MAR 15
GLG A319-112 FLEET
AFM
MCDL-78-01-00016033.0001001/20 MAR 15
H
APPRO-TR P 8/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR502 Issue 1
ABNORMAL V ALPHA PROT
APPROVED
Ident.: TDU / APPRO-TR-00016062.0001001 / 05 DEC 14
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
GLG A319-112 FLEET
AFM
EMER-34-00016060.0001001/05 DEC 14
I
APPRO-TR P 9/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR566 Issue 1
EMER DESCENT
APPROVED
Ident.: TDU / APPRO-TR-00016716.0001001 / 07 OCT 15
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
GLG A319-112 FLEET
AFM
EMER-90-00016883.0001001/07 OCT 15
J
APPRO-TR P 10/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR556 Issue 1
TOWBARLESS OPERATIONS
APPROVED
Ident.: TDU / APPRO-TR-00016598.0001001 / 09 JUL 15
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
GLG A319-112 FLEET
AFM
LIM-09-00016592.0001001/09 JUL 15
K
APPRO-TR P 11/12
14 NOV 17
APPROVAL DATA
TEMPORARY REVISIONS
A319
AIRPLANE FLIGHT MANUAL
TR564 Issue 1
MCDL 52-03 ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
APPROVED
Ident.: TDU / APPRO-TR-00016654.0001001 / 06 JUL 15
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-52-03-00016655.0001001/06 JUL 15
GLG A319-112 FLEET
AFM
MCDL-52-03-00016656.0001001/06 JUL 15
L
APPRO-TR P 12/12
14 NOV 17
GENERAL
Intentionally left blank
GENERAL
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
GEN-PLP-TOC P 1/2
07 FEB 17
GENERAL
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET
AFM
GEN-PLP-TOC P 2/2
07 FEB 17
GENERAL
INTRODUCTION
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: GEN-INTR-00007010.0001001 / 16 JAN 17
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.
GLG A319-112 FLEET
AFM
A
GEN-INTR P 1/2
07 FEB 17
GENERAL
INTRODUCTION
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
GEN-INTR P 2/2
07 FEB 17
GENERAL
AFM DESCRIPTION
A319
AIRPLANE FLIGHT MANUAL
APPROVED AFM FORMAT
APPROVED
Ident.: GEN-DESC-00015195.0001001 / 02 DEC 13
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
APPROVED
Ident.: GEN-DESC-00007013.0001001 / 23 NOV 09
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
APPROVED
Ident.: GEN-DESC-00007015.0001001 / 23 NOV 09
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)
GLG A319-112 FLEET
AFM
A to C →
GEN-DESC P 1/4
07 FEB 17
GENERAL
AFM DESCRIPTION
A319
AIRPLANE FLIGHT MANUAL
‐ Supplementary performance (contaminated runway)
‐ Regulatory differences (when applicable).
DOCUMENTARY UNIT (DU)
APPROVED
Ident.: GEN-DESC-00007016.0001001 / 16 JAN 17
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
APPROVED
Ident.: GEN-DESC-00007017.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
← C to E
GEN-DESC P 2/4
07 FEB 17
GENERAL
AFM DESCRIPTION
A319
AIRPLANE FLIGHT MANUAL
APPROVAL INFORMATION
APPROVED
Ident.: GEN-DESC-00020434.0001001 / 16 JAN 17
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
APPROVED
Ident.: GEN-DESC-00007366.0001001 / 16 JAN 17
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)
APPROVED
Ident.: GEN-DESC-00007018.0001001 / 16 JAN 17
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).
GLG A319-112 FLEET
AFM
F to H →
GEN-DESC P 3/4
07 FEB 17
GENERAL
AFM DESCRIPTION
A319
AIRPLANE FLIGHT MANUAL
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).
GLG A319-112 FLEET
AFM
←H
GEN-DESC P 4/4
07 FEB 17
GENERAL
WORDING DEFINITIONS
A319
AIRPLANE FLIGHT MANUAL
WARNING DEFINITION
APPROVED
Ident.: GEN-DEF-00007020.0001001 / 23 NOV 09
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
APPROVED
Ident.: GEN-DEF-00007021.0001001 / 23 NOV 09
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
APPROVED
Ident.: GEN-DEF-00006982.0001001 / 23 NOV 09
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
APPROVED
Ident.: GEN-DEF-00007322.0001001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
A to D
GEN-DEF P 1/2
16 MAR 15
GENERAL
WORDING DEFINITIONS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
GEN-DEF P 2/2
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
ABBREVIATIONS
APPROVED
Ident.: GEN-ABB-00006976.0001001 / 14 JAN 15
Criteria: SA
A
Abbreviation
A/C
AC
ACD
ACJ
ACL
ACM
ACT
ADIRU
ADR
ADS-B
ADS-C
AEO
AFM
AGL
AIME
ALD
AMC
AMJ
AMM
AOA
AOC
AP
APU
AR
ARINC
ASD
ASDA
ASI
ATA
ATC
ATS
ATSA-AIRB
ATSA-ITP
ATSA-VSA
Term
Aircraft
Advisory Circular
Alternative Current
Airworthiness Compliance Document
Advisory Circular-Joint
ATC Clearance
ATC Communication Management
Additional Center Tank
Air Data Inertial Reference Unit
Air Data Reference
Automatic Dependent Surveillance-Broadcast
Automatic Dependent Surveillance-Contract
All Engines Operative
Airplane Flight Manual
Above Ground Level
Autonomous Integrity Monitoring Extrapolation
Actual Landing Distance
ATC Microphone Check
Acceptable Means of Compliance
Advisory Material-Joint
Aircraft Maintenance Manual
Angle of Attack
Airlines Operational Control
Autopilot
Auxiliary Power Unit
Authorization Required
Aeronautical Radio INC
Accelerate Stop Distance
Accelerate Stop Distance Available
Air Speed Indicator
Air Transport Association
Air Traffic Control
Air Traffic Service
Air Traffic Situational Awareness - Airborne
Air Traffic Situational Awareness - In Trail Procedures
Air Traffic Situational Awareness - Visual Separation on Approach
GLG A319-112 FLEET
AFM
A→
Continued on the following page
GEN-ABB P 1/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
ATSAW
ATSU
AWO
Term
Airborne Traffic Situational Awareness
Air Traffic Service Unit
All Weather Operations
Continued from the previous page
B
Abbreviation
BC
BSCU
Term
Back Course
Braking and Steering Control Unit
C
Abbreviation
C/B
CAA
CAP
CAS
CCOM
CDL
CDLS
CFR
CG
CIS
CJ
CLD
CM
CML
CMP
CONF
CPDLC
CS
CSMG
CVR
CWY
Term
Circuit Breaker
Civil Aviation Authority
Civil Aviation Publication
Calibrated Airspeed
Cabin Crew Operating Manual
Configuration Deviation List
Cockpit Door Locking System
Code of Federal Regulations
Center of Gravity
Commonwealth of Independent States
Corporate Jet
Certified Landing Distance
Context Management
Consumable Material List
Configuration, Maintenance and Procedures
Configuration
Controller Pilot Datalink Communication
Certification Specifications
Constant Speed Motor Generator
Cockpit Voice Recorder
Clearway
D
Abbreviation
DA
DAC
D-ATIS
DC
DCL
Term
Decision Altitude
Dual Annular Combustor
Digital Automatic Terminal Information Service
Direct Current
Departure Clearance
GLG A319-112 FLEET
AFM
←A→
Continued on the following page
GEN-ABB P 2/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
DGAC
DH
DLIC
DMC
DME
DNA
DO
DU
Term
Direction Générale de l'Aviation Civile
Decision Height
Data Link Initiation Capability
Display Management Computer
Distance Measuring Equipment
Dirección National de Aeronavegabilidad
Document Order (RTCA)
Display Unit
Documentary Unit
Continued from the previous page
E
Abbreviation
EASA
ECAM
ED
EDTO
EFB
EFIS
EGPWS
EGT
EHS
EIS
ELAC
ELT
EMER
ENG
EPR
ESS
ETOPS
EWD
Term
European Aviation Safety Agency
Electronic Centralized Aircraft Monitoring Computer
EUROCAE Document
Extended Diversion Time Operations
Electronic Flight Bag
Electronic Flight Instrument System
Enhanced Ground Proximity Warning System
Exhaust Gas Temperature
Enhanced Surveillance
Electronic Instrument System
Elevator Aileron Computer
Electronic Locator Transmitter
Emergency
Engine
Engine Pressure Ratio
Essential
Extended range operations for two engine aeroplanes (EASA)
Extended operations (FAA)
Engine Warning Display
F
Abbreviation
F
F/CTL
F-PLN
FAA
FAC
FADEC
Term
Fuel
Flight Controls
Flight Plan
Federal Aviation Administration
Flight Augmentation Computer
Full Authority Digital Engine Control System
GLG A319-112 FLEET
AFM
←A→
Continued on the following page
GEN-ABB P 3/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
FAF
FANS
FAP
FAR
FCDC
FCOM
FCU
FD
FI
FLS
FLX
FM
FMA
FMGC
FMGS
FMS
FOB
FPA
FPV
FQI
FU
FWC
Term
Final Approach Fix
Future Air Navigation System
Final Approach Point
Federal Aviation Regulations
Flight Control Data Concentrator
Flight Crew Operating Manual
Flight Control Unit
Flight Director
Filling Instructions
FMS Landing System
Flex
Flight Management
Flight Mode Annunciator
Flight Management and Guidance Computer
Flight Management and Guidance System
Flight Management System
Fuel on Board
Flight Path Angle
Flight Path Vector
Fuel Quantity Indication
Fuel Used
Flight Warning Computer
Continued from the previous page
G
Abbreviation
G/S
GBAS
GEN
GLS
GNSS
GPS
GPWS
GSM
Term
Glideslope
Ground-Based Augmentation System
Generator
GPS Landing System
Global Navigation Satellite System
Global Positioning System
Ground Proximity Warning System
Global System for Mobile Communication
H
Abbreviation
HF
HKCAD
HPC
HUD
Term
High Frequency
Hong Kong Civil Aviation Department
High Pressure Compressor
Head Up Display
GLG A319-112 FLEET
AFM
←A→
GEN-ABB P 4/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
I
Abbreviation
IAC
IAC AR
IAS
ICAO
IDG
IFR
IGN
IL
ILS
IR
IRS
ISA
ISIS
ISPSS
Term
Instrução de Aviação Civil (Civil Aviation Instruction)
Interstate Aviation Committee Aviation Register
Indicated Airspeed
International Civil Aviation Organization
Integrated Drive Generator
Instrument Flight Rules
Ignition
Information Leaflet
Instrument Landing System
Inertial Reference
Inertial Reference System
International Standard Atmosphere
Integrated Standby Instrument System
In-Seat Power Supply System
J
Abbreviation
JAA
JAR
JCAB
Term
Joint Aviation Authorities
Joint Aviation Regulation
Japan Civil Aviation Bureau
K
Abbreviation
KOZ
Term
Keep Out Zone
L
Abbreviation
L/G
LD
LDA
LDG
LEDU
LETR
LGCIU
LH
LIP
LNAV
LOC
Term
Landing Gear
Landing Distance
Localizer Directional Aid
Landing Distances Available
Landing
List of Effective Documentary Unit
List of Effective Temporary Revision
Landing Gear Control and Interface Unit
Left Hand
Lift Improvement Package
Lateral Navigation
Localizer
GLG A319-112 FLEET
AFM
←A→
Continued on the following page
GEN-ABB P 5/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
LOC-BC
LPV
LRBL
LS
Term
Localizer Back Course
Localizer Performance with Vertical Guidance
Least Risk Bomb Location
Landing System
Continued from the previous page
M
Abbreviation
MAC
MAP
MAPSC
MCDL
MCDU
MCPSC
MCT
MDA
MDH
MEA
MLE
MLS
MLW
MMEL
MMO
MMR
MOPS
MORA
MSN
MTOW
MZFW
Term
Mean Aerodynamic Chord
Missed Approach Point
Maximum Approved Passenger Seating Configuration
Master Configuration Deviation List
Multipurpose Control & Display Unit
Maximum Certificated Passenger Seating Capacity
Maximum Continuous Thrust
Minimum Descent Altitude
Minimum Descent Height
Minimum En route Altitude
Maximum Landing Gear Extended Mach
Microwave Landing Distance
Maximum Landing Weight
Master Minimum Equipment List
Maximum Operating Mach
Multi-Mode Receiver
Minimum Operational Performance Standards
Minimum Off Route Altitude
Manufacturer Serial Number
Maximum Takeoff Weight
Maximum Zero Fuel Weight
N
Abbreviation
N1
N2
NAI
NDB
NAV
ND
NPA
NSA
Term
Low Pressure Rotor Speed
High Pressure Rotor Speed
Nose Air Intake
Non-Directional Beacon
Navigation
Navigation Display
Non Precision Approach
Norme Sud Aviation
GLG A319-112 FLEET
AFM
←A→
GEN-ABB P 6/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
O
Abbreviation
OANS
OAT
OCL
OEI
OEW
OLB
OLD
OVHT
OW
Term
On-board Airport Navigation System
Outside Air Temperature
Oceanic Clearance
One Engine Inoperative
Operational Empty Weight
Ops Library Browser
Operational Landing Distance
Overheat
Operational Weight
P
Abbreviation
P/B
PAPI
PAR
PC
PED
PF
PFC
PFD
PM
PTU
PVI
Term
Pushbutton
Precision Approach Path Indicator
Precision Approach Radar
Personal Computer
Portable Electronic Devices
Pilot Flying
Porous Friction Course
Primary Flight Display
Pilot Monitoring
Power Transfer Unit
Paravisual Indicator
Q
Abbreviation
QFE
QFU
QNH
Term
Field Elevation Atmosphere Pressure
Runway Heading
Sea Level Atmosphere Pressure
R
Abbreviation
RA
RAT
RBS
RF
RH
RLD
Term
Radio Altimeter
Resolution Advisory
Ram Air Turbine
Radio Beacon System
Radius to Fix
Right Hand
Required Landing Distance
GLG A319-112 FLEET
AFM
Continued on the following page
←A→
GEN-ABB P 7/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
RNAV
RNP
ROP
ROPS
ROW
RVR
RVSM
Term
Area Navigation
Required Navigation Performance
Runway Overrun Protection
Runway Overrun Prevention System
Runway Overrun Warning
Runway Visual Range
Reduced Vertical Separation Minima
Continued from the previous page
S
Abbreviation
SA
SAAAR
SAC
SAC-TI
SAL
SAT
SATCOM
SB
SD
SDF
SEC
SES
SFCC
SIL
SRS
STAT INV
SWY
Term
Single Aisle
Special Aircrew and Aircraft Authorization Required
Single Annular Combustor
Single Annular Combustor- Tech Insertion
Steep Approach Landing
Static Air Temperature
Satellite Communication
Service Bulletin
System Display
Simplified Directional Facility
Spoiler Elevator Computer
Single European Sky
Slat Flap Control Computer
Service Information Letter
Speed Reference System
Static Inverter
Stopway
T
Abbreviation
TA
TAB
TAT
TAWS
TCAS
TDU
TGL
TI
TO
TOD
Term
Traffic Advisory
Tabulation and Interpolation Program
Total Air Temperature
Terrain Awareness and Warning System
Traffic Alert and Collision Avoidance System
Temporary Documentary Unit
Temporary Guidance Leaflet
Tech Insertion
Takeoff
Takeoff Distance
GLG A319-112 FLEET
AFM
←A→
Continued on the following page
GEN-ABB P 8/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
Abbreviation
TODA
TOGA
TOR
TORA
TR
TRU
Continued from the previous page
Term
Takeoff Distance Available
Takeoff - Go-Around
Takeoff Run
Takeoff Run Available
Temporary Revision
Transformer Rectifer Unit
V
Abbreviation
V1
V2
VA
VALPHAMAX
VAPP
VC
V/DEV
VDL
VFE
VFR
VHF
VLE
VLO
VLOF
VLS
VMC
VMCA
VMCG
VMIN
VMIN 1G
VMO
VNAV
VOR
VR
VREF
VS1G
VSW
Term
Takeoff Decision Speed
Takeoff Safety Speed
Maximum Design Maneuvering Speed
Speed at Alpha-Max
Final Approach Speed
Design Cruise Speed
Vertical Deviation
VHF Data Link
Maximum Flap Extended Speed
Visual Flight Rules
Very High Frequency
Max L/G Extended Speed
Max L/G Operating Speed
Lift-Off Speed
Lowest Selectable Speed
Visual Meteorological Conditions
Minimum Control Airspeed
Minimum Control Speed Ground
Minimum Operating Speed
Minimum Operating Speed under 1g Load Factor
Maximum Operating Speed
Vertical Navigation
VHF Omnidirectional Range
Rotation Speed
Landing Reference Speed
Stall Speed under 1g Load Factor
Stall Warning Speed
GLG A319-112 FLEET
AFM
←A→
GEN-ABB P 9/10
16 MAR 15
GENERAL
ABBREVIATIONS
A319
AIRPLANE FLIGHT MANUAL
W
Abbreviation
WBM
WV
WX
Term
Weight and Balance Manual
Weight Variant
Weather mode (ND)
Z
Abbreviation
ZFCG
Zp
Term
Zero Fuel Center of Gravity
Pressure Altitude
GLG A319-112 FLEET
AFM
←A
GEN-ABB P 10/10
16 MAR 15
GENERAL
UNITS
A319
AIRPLANE FLIGHT MANUAL
CORRESPONDENCE BETWEEN UNITS
APPROVED
Ident.: GEN-UNIT-00006979.0001001 / 23 NOV 09
Criteria: SA
METRIC TO US
LENGTH
SPEED
WEIGHT
FORCE
PRESSURE
VOLUME
MOMENTUM
TEMPERATURE
1 mm
1m
1m
1 km
1 m/s
1 km/h
1g
1 kg
1t
1N
1 daN
1 bar
1 mbar
1l
1 m³
1 daN.m
METRIC
0.0394 in
3.281 ft
1.094 yd
0.540 NM
3.281 ft/s
0.540 kt
0.0353 oz
2.204623 lb
2 204.623 lb
0.2248 lb
2.248 lb
14.505 PSI
0.0145 PSI
0.2642 US Gal
264.2 US Gal
88.50 lb.in
US
US TO METRIC
LENGTH
SPEED
WEIGHT
FORCE
PRESSURE
VOLUME
GLG A319-112 FLEET
AFM
1 in
1 ft
1 yd
1 NM
1 ft/s
1 kt
1 oz
1 lb
1 lb
1 lb
1 lb
1 PSI
1 PSI
1 US Gal
1 US Gal
US
25.4 mm
0.3048 m
0.914 m
1.852 km
0.3048 m/s
1.852 km/h
28.35 g
0.45359 kg
0.0004536 t
4.448 N
0.4448 daN
0.0689 bar
68.947 mbar
3.785 l
0.003785 m³
A→
METRIC
Continued on the following page
GEN-UNIT P 1/2
25 JAN 11
GENERAL
UNITS
A319
AIRPLANE FLIGHT MANUAL
MOMENTUM
1 lb.in
Continued from the previous page
METRIC
0.0113 daN.m
US
TEMPERATURE
GLG A319-112 FLEET
AFM
←A
GEN-UNIT P 2/2
25 JAN 11
GENERAL
3-VIEW DRAWING
A319
AIRPLANE FLIGHT MANUAL
3-VIEW DRAWING
APPROVED
Ident.: GEN-VIEW-00006880.0004001 / 23 NOV 09
Criteria: A319
Front View
GLG A319-112 FLEET
AFM
A→
GEN-VIEW P 1/4
08 APR 11
GENERAL
3-VIEW DRAWING
A319
AIRPLANE FLIGHT MANUAL
Top View
Side View
Reference area
Root chord
MAC (LA)
Aspect ratio
GLG A319-112 FLEET
AFM
WING
122.4 m²
6.074 m
4.194 m
9.396
←A→
1 317 ft² 72 in²
19 ft 11 in
13 ft 9 in
GEN-VIEW P 2/4
08 APR 11
GENERAL
3-VIEW DRAWING
A319
AIRPLANE FLIGHT MANUAL
Reference area
MAC (LH)
Aspect ratio
Distance from 25 % LA to
25 % LH
Reference area
MAC (LV)
Aspect ratio
Distance from 25 % LA to
25 % LV
GLG A319-112 FLEET
AFM
31 m²
2.701 m
HORIZONTAL TAIL PLANE
5.00
15.454 m
21.51 m²
3.948 m
VERTICAL TAIL PLANE
1.6
14.589 m
←A
333 ft² 98 in²
8 ft 10 in
50 ft 9 in
231 ft² 77 in²
12 ft 11 in
47 ft 11 in
GEN-VIEW P 3/4
08 APR 11
GENERAL
3-VIEW DRAWING
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
GEN-VIEW P 4/4
08 APR 11
LIMITATIONS
Intentionally left blank
LIMITATIONS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
LIM-PLP-TOC P 1/4
14 NOV 17
LIMITATIONS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
LIM-22 AUTO FLIGHT SYSTEM
LIM-22-FMS Flight Management System
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
LIM-PLP-TOC P 2/4
14 NOV 17
LIMITATIONS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
LIM-49 AUXILIARY POWER UNIT
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
LIM-PLP-TOC P 3/4
14 NOV 17
LIMITATIONS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-PLP-TOC P 4/4
14 NOV 17
LIMITATIONS
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: LIM-GEN-00006957.0001001 / 23 NOV 09
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
APPROVED
Ident.: LIM-GEN-00006958.0001001 / 23 NOV 09
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
APPROVED
Ident.: LIM-GEN-00006959.0001001 / 23 NOV 09
Criteria: SA
Minimum flight crew: 2 pilots.
MAXIMUM OPERATING ALTITUDE
APPROVED
Ident.: LIM-GEN-00006960.0002001 / 23 NOV 09
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
APPROVED
Ident.: LIM-GEN-00006961.0001001 / 02 DEC 13
Criteria: SA
Slats and flaps retracted: -1 to +2.5 g.
Slats and/or flaps extended: 0 to +2.0 g.
GLG A319-112 FLEET
AFM
A to E
LIM-GEN P 1/2
14 DEC 13
LIMITATIONS
GENERAL
A319
AIRPLANE FLIGHT MANUAL
ICING CONDITIONS DEFINITION
APPROVED
Ident.: LIM-GEN-00009165.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
F
LIM-GEN P 2/2
14 DEC 13
LIMITATIONS
WEIGHTS AND LOADING
A319
AIRPLANE FLIGHT MANUAL
WEIGHT LIMITATIONS
APPROVED
Ident.: LIM-WGHT-00006860.0014001 / 23 NOV 09
Criteria: (A319 and 25328)
Weight Variant : WV 01
Maximum Taxi Weight
Maximum Takeoff Weight (MTOW)
Maximum Landing Weight (MLW)
Maximum Zero Fuel Weight (MZFW)
Minimum Weight
Note:
70 400 kg
155 205 lb
61 000 kg
134 481 lb
70 000 kg
57 000 kg
35 400 kg
154 323 lb
125 663 lb
78 044 lb
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
Criteria: ((319-111 or 319-112 or 319-113 or 319-114 or 319-131 or 319-132) and 25328)
APPROVED
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.
GLG A319-112 FLEET
AFM
A to B →
LIM-WGHT P 1/4
25 JAN 11
LIMITATIONS
WEIGHTS AND LOADING
A319
AIRPLANE FLIGHT MANUAL
CG Envelope WV 01
PERFORMANCE LIMITATIONS
APPROVED
Ident.: LIM-WGHT-00006962.0001001 / 23 NOV 09
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)
GLG A319-112 FLEET
AFM
← B to C →
LIM-WGHT P 2/4
25 JAN 11
LIMITATIONS
WEIGHTS AND LOADING
A319
AIRPLANE FLIGHT MANUAL
‐ Brake energy limit (observe brake temperature warning (300 °C))
‐ Tire speed.
LOADING
APPROVED
Ident.: LIM-WGHT-00006963.0001001 / 23 NOV 09
Criteria: SA
The aircraft must be loaded in accordance with the loading instructions given in the Weight and
Balance Manual (WBM) chapter 1-10.
GLG A319-112 FLEET
AFM
← C to D
LIM-WGHT P 3/4
25 JAN 11
LIMITATIONS
WEIGHTS AND LOADING
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-WGHT P 4/4
25 JAN 11
LIMITATIONS
AIRSPEEDS
A319
AIRPLANE FLIGHT MANUAL
VMO/MMO
APPROVED
Ident.: LIM-SPD-00007065.0001001 / 23 NOV 09
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
APPROVED
Ident.: LIM-SPD-00007319.0004001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B →
LIM-SPD P 1/2
25 JAN 11
LIMITATIONS
AIRSPEEDS
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: LIM-SPD-00006883.0004001 / 23 NOV 09
Criteria: (320-231 or 320-232 or 320-233 or A318 or A319)
MAXIMUM SLATS/FLAPS EXTENDED SPEEDS OR OPERATING SPEEDS (VFE)
Flight Phase
Intermediate approach
Takeoff 1+F
Approach and takeoff
Approach, takeoff
and landing
Landing
Slats Position
18 °
Flaps Position
0°
Flaps Lever Position
1
VFE
230 kt IAS
22 °
15 °
2
200 kt IAS
18 °
10 °
1
215 kt IAS
22 °
20 °
3
185 kt IAS
27 °
40 °
FULL
177 kt IAS
VLO AND VLE/MLE
APPROVED
Ident.: LIM-SPD-00007317.0001001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
← B to D
LIM-SPD P 2/2
25 JAN 11
LIMITATIONS
OPERATIONAL PARAMETERS
A319
AIRPLANE FLIGHT MANUAL
ENVIRONMENTAL ENVELOPE
APPROVED
Ident.: LIM-OPS-00006919.0015001 / 23 NOV 09
Criteria: ((A319 or 321-200) and 30748)
TAILWIND
APPROVED
Ident.: LIM-OPS-00007309.0001001 / 23 NOV 09
Criteria: SA
Maximum tailwind for takeoff and landing: 10 kt
GLG A319-112 FLEET
AFM
A to B
LIM-OPS P 1/2
25 JAN 11
LIMITATIONS
OPERATIONAL PARAMETERS
A319
AIRPLANE FLIGHT MANUAL
RUNWAY SLOPE
APPROVED
Ident.: LIM-OPS-00007310.0001001 / 23 NOV 09
Criteria: SA
Maximum mean runway slope: ± 2 %
GLG A319-112 FLEET
AFM
C
LIM-OPS P 2/2
25 JAN 11
LIMITATIONS
TOWING AND TAXIING
A319
AIRPLANE FLIGHT MANUAL
MANEUVERS ON GROUND
APPROVED
Ident.: LIM-09-00007357.0001001 / 23 NOV 09
Criteria: SA
During towing, ±85 ° of nosewheel travel must not be exceeded.
Note:
Mechanical stop is designed at ±95 ° of nosewheel travel.
TOWBARLESS OPERATIONS
APPROVED
Ident.: TDU / LIM-09-00016592.0001001 / 09 JUL 15
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
APPROVED
Ident.: LIM-09-00007358.0001001 / 03 AUG 10
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.
GLG A319-112 FLEET
AFM
A to C
LIM-09 P 1/2
30 JUL 15
LIMITATIONS
TOWING AND TAXIING
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-09 P 2/2
30 JUL 15
LIMITATIONS
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
CABIN PRESSURIZATION
APPROVED
Ident.: LIM-21-00007261.0001001 / 23 NOV 09
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).
GLG A319-112 FLEET
AFM
A
LIM-21 P 1/2
25 JAN 11
LIMITATIONS
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-21 P 2/2
25 JAN 11
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FLIGHT MANAGEMENT SYSTEM
GENERAL
Ident.: LIM-22-FMS-00009567.0002001 / 23 NOV 09
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
APPROVED
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
APPROVED
Ident.: LIM-22-FMS-00009568.0016001 / 13 MAR 17
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
GLG A319-112 FLEET
AFM
A to B →
LIM-22-FMS P 1/4
14 APR 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
FLIGHT MANAGEMENT SYSTEM
AIRPLANE FLIGHT MANUAL
‐ 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
APPROVED
Ident.: LIM-22-FMS-00009569.0003001 / 23 NOV 09
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
En Route
In Terminal Area
In Approach
GLG A319-112 FLEET
AFM
1 NM
With AP OFF and
FD ON in NAV
With AP OFF
and FD OFF
0.51 NM
0.51 NM
1 NM
0.5 NM
0.3 NM
0.3 NM
← B to C →
1.1 NM
Not authorized
LIM-22-FMS P 2/4
14 APR 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
FLIGHT MANAGEMENT SYSTEM
AIRPLANE FLIGHT MANUAL
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
Criteria: ((A319 or A320 or A321) and (25205 or 26111 or 26485 or 26999 or 28382 or 30241 or 30631 or 30635))
APPROVED
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
APPROVED
Ident.: TDU / LIM-22-FMS-00009620.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
← C to E
LIM-22-FMS P 3/4
14 APR 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FLIGHT MANAGEMENT SYSTEM
APPROACHES
APPROVED
Ident.: LIM-22-FMS-00009571.0002001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
F
LIM-22-FMS P 4/4
14 APR 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
FLIGHT GUIDANCE SYSTEM
AIRPLANE FLIGHT MANUAL
AIRWORTHINESS STANDARDS COMPLIANCE
APPROVED
Ident.: LIM-22-FGS-00009235.0001001 / 23 NOV 09
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
APPROVED
Ident.: TDU / LIM-22-FGS-00009711.0009001 / 04 NOV 15
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
FAEL
PAFA
PANC
BIKF
EGAA
EGPF
EGPH
EFRO
EFOU
Note:
Airport location
EAST LONDON BEN SCHOEMAN SOUTH AFR
REP
FAIRBANKS INTL AK USA
ANCHORAGE INTL AK USA
KEFLAVIK ICELAND
BELFAST ALDERGROVE UNITED KINGDOM
GLASGOW UNITED KINGDOM
EDINBURGH UNITED KINGDOM
ROVANIEMI FINLAND
OULU FINLAND
Month/year
August 2018
January 2015
October 2015
January 2015
September 2020
July 2020
September 2020
September 2019
August 2020
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.
GLG A319-112 FLEET
AFM
A to B →
LIM-22-FGS P 1/4
10 OCT 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FLIGHT GUIDANCE SYSTEM
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
APPROVED
Ident.: LIM-22-FGS-00009238.0003001 / 02 DEC 13
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
APPROVED
Ident.: LIM-22-FGS-00009242.0001001 / 28 MAR 17
Criteria: (A318 or A319 or A320)
At takeoff
: 100 ft AGL and at least 5 seconds after liftoff.
In approach using FINAL APP, NAV
: 250 ft AGL.
FPA, NAV V/S, TRK FPA, HDG V/S
In circling approach
: 500 ft AGL.
In ILS approach if CAT 2 or CAT 3
: 160 ft AGL.
capability is not displayed on FMA
In ILS approach when CAT 2 or CAT 3 : Refer to LIM-22-FGS CAT II / CAT III Operations.
capability is displayed on FMA
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.
GLG A319-112 FLEET
AFM
← B to D
LIM-22-FGS P 2/4
10 OCT 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
FLIGHT GUIDANCE SYSTEM
AIRPLANE FLIGHT MANUAL
CAT II / CAT III OPERATIONS
APPROVED
Ident.: LIM-22-FGS-00009243.0013001 / 11 AUG 17
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
GLG A319-112 FLEET
AFM
E→
LIM-22-FGS P 3/4
10 OCT 17
LIMITATIONS
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FLIGHT GUIDANCE SYSTEM
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.
GLG A319-112 FLEET
AFM
←E
LIM-22-FGS P 4/4
10 OCT 17
LIMITATIONS
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELECTRICAL
APPROVED
Ident.: LIM-24-00007263.0001001 / 23 NOV 09
Criteria: SA
Maximum continuous load per generator (100 %): 90 KVA
Maximum continuous load per TRU: 200 A
GLG A319-112 FLEET
AFM
A
LIM-24 P 1/2
25 JAN 11
LIMITATIONS
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-24 P 2/2
25 JAN 11
LIMITATIONS
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL AND ADDITIVE SPECIFICATIONS
APPROVED
Ident.: LIM-28-00007246.0001001 / 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)
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
APPROVED
Ident.: LIM-28-00007248.0003001 / 23 NOV 09
Criteria: (A318 or A319 or 320-200)
Fuel loading varies with specific fuel gravity without any fuel weight limitation.
Tanks
Note:
2 Wing Tanks
1 Center Tank
Total
15 609 l
Tanks
0.80 kg/l
2 Wing Tanks
1 Center Tank
Total
12 487 kg
Fuel Quantity
8 250 l
4 123 US Gal
2 179 US Gal
23 859 l
6 303 US Gal
Fuel Specific Gravity
6 600 kg
19 087 kg
Fuel Weight
6.676 lb/US Gal
27 525 lb
14 547 lb
42 078 lb
When the quantity indications reach "zero" the remaining fuel cannot safely be used.
WARNING
Takeoff on center tank feeding is prohibited.
GLG A319-112 FLEET
AFM
A to B
LIM-28 P 1/4
12 SEP 17
LIMITATIONS
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL IMBALANCE
APPROVED
Ident.: LIM-28-00007254.0015001 / 11 AUG 17
Criteria: (A319 or A320)
FUEL IMBALANCE AT TAKEOFF
INNER TANKS (OUTER BALANCED)
Tank Fuel Quantity
(Heavier Tank)
Full
3 000 kg (6 613 lb)
1 450 kg (3 196 lb)
Maximum Asymmetry
500 kg (1 102 lb)
1 050 kg (2 314 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)
Full
4 300 kg (9 479 lb)
2 250 kg (4 960 lb)
Maximum Asymmetry
1 500 kg (3 306 lb)
1 600 kg (3 527 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.
GLG A319-112 FLEET
AFM
C
LIM-28 P 2/4
12 SEP 17
LIMITATIONS
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL TEMPERATURE LIMITS
APPROVED
Ident.: LIM-28-00007259.0002001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
D
LIM-28 P 3/4
12 SEP 17
LIMITATIONS
FUEL
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-28 P 4/4
12 SEP 17
LIMITATIONS
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYDRAULICS FLUID
APPROVED
Ident.: LIM-29-00007262.0001001 / 23 NOV 09
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
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and (22803 or 27189))
Impacted DU: NONE
Belongs to TR6 Issue 1
APPROVED
In the case of RAT deployment flight testing, limit the speed to 250 kt from RAT deployment to
landing.
GLG A319-112 FLEET
AFM
A to B
LIM-29 P 1/2
25 JAN 11
LIMITATIONS
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-29 P 2/2
25 JAN 11
LIMITATIONS
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
TIRE SPEED
APPROVED
Ident.: LIM-32-00011074.0001001 / 03 AUG 10
Criteria: SA
Maximum tire speed: 195 kt (ground speed).
GLG A319-112 FLEET
AFM
A
LIM-32 P 1/2
25 JAN 11
LIMITATIONS
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-32 P 2/2
25 JAN 11
LIMITATIONS
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
INERTIAL REFERENCE SYSTEM (IRS)
APPROVED
Ident.: LIM-34-00007264.0001001 / 10 NOV 17
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)
APPROVED
Ident.: LIM-34-00007359.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
LIM-34 P 1/2
14 NOV 17
LIMITATIONS
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-34 P 2/2
14 NOV 17
LIMITATIONS
INFORMATION SYSTEMS
A319
AIRPLANE FLIGHT MANUAL
AIRLINE OPERATION CONTROL APPLICATIONS
APPROVED
Ident.: LIM-46-00006965.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
LIM-46 P 1/2
25 JAN 11
LIMITATIONS
INFORMATION SYSTEMS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-46 P 2/2
25 JAN 11
LIMITATIONS
AUXILIARY POWER UNIT
A319
AIRPLANE FLIGHT MANUAL
AUXILIARY POWER UNIT (APU)
APPROVED
Ident.: LIM-49-00007260.0003001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
LIM-49 P 1/2
25 JAN 11
LIMITATIONS
AUXILIARY POWER UNIT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
LIM-49 P 2/2
25 JAN 11
LIMITATIONS
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
MAIN ENGINES
APPROVED
Ident.: LIM-70-00007233.0021001 / 03 AUG 10
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
APPROVED
Ident.: LIM-70-00007235.0002001 / 11 MAY 17
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)
Operating Condition
Time Limit
Starting
Maximum Continuous
Normal
Takeoff and
Go-around One ENG OUT
(1)
(1)
CONT.
5 min
10 min
ENG Indicated
EGT Limit
725 °C
915 °C
950 °C
950 °C
Maximum Rotor Speed
N1
N2
----------
104 %
104 %
----
105 %
105 %
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
APPROVED
Ident.: LIM-70-00007236.0001001 / 23 NOV 09
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
APPROVED
Ident.: LIM-70-00007232.0002001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
A to D →
LIM-70 P 1/2
13 JUN 17
LIMITATIONS
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
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
Criteria: ((318-111 or 318-112 or 320-215) or ((319-111 or 319-112) and 32619) or (319-112 and 33239))
APPROVED
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
APPROVED
Ident.: LIM-70-00006881.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
← D to F
LIM-70 P 2/2
13 JUN 17
EMERGENCY PROCEDURES
Intentionally left blank
EMERGENCY PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
EMER-PLP-TOC P 1/2
12 SEP 17
EMERGENCY PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
EMER-90 MISCELLANEOUS
TABLE OF CONTENTS
Continued from the previous page
STALL RECOVERY.................................................................................................................................................A
EMER DESCENT.................................................................................................................................................... B
EMER DESCENT.................................................................................................................................................... C
EMERGENCY EVACUATION................................................................................................................................. D
DITCHING................................................................................................................................................................ E
FORCED LANDING................................................................................................................................................. F
Emergency Landing (All Engines Failure).............................................................................................................. G
GLG A319-112 FLEET
AFM
EMER-PLP-TOC P 2/2
12 SEP 17
EMERGENCY PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: EMER-GEN-00007037.0001001 / 14 JAN 15
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
APPROVED
Ident.: EMER-GEN-00015177.0001001 / 14 JUL 17
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
Dry
Wet
Compacted Snow
GLG A319-112 FLEET
AFM
Max Reported Braking Action
6 - DRY
5 - GOOD
4 - GOOD to MEDIUM
Continued on the following page
A to B →
EMER-GEN P 1/2
08 AUG 17
EMERGENCY PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
Continued from the previous page
Max Reported Braking Action
3 - MEDIUM
2 - MEDIUM to POOR
1 - POOR
Runway Condition
More than 3 mm of Dry or Wet Snow
More than 3 mm of Standing Water or Slush
Ice (Cold and Dry)
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.
GLG A319-112 FLEET
AFM
←B
EMER-GEN P 2/2
08 AUG 17
EMERGENCY PROCEDURES
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
CAB PR - EXCESS CAB ALT
APPROVED
Ident.: EMER-21-00007053.0004001 / 02 DEC 13
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
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and 35220)
APPROVED
Turn off both packs.
Alert cabin crew.
GLG A319-112 FLEET
AFM
A to B
EMER-21 P 1/2
14 DEC 13
EMERGENCY PROCEDURES
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-21 P 2/2
14 DEC 13
EMERGENCY PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED)
APPROVED
Ident.: EMER-24-00006884.0003001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
A
EMER-24 P 1/2
14 DEC 13
EMERGENCY PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-24 P 2/2
14 DEC 13
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: EMER-26-00007038.0001001 / 14 JAN 15
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)
APPROVED
Ident.: EMER-26-00007041.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
EMER-26 P 1/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
ENG 1 (2) FIRE (ON GROUND)
Ident.: EMER-26-00007042.0002001 / 23 NOV 09
Criteria: ((318-111 or 318-112 or A319 or A320 or A321) and ((20067 or 20069) and (36847 or 37871)))
APPROVED
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
APPROVED
Ident.: EMER-26-00007043.0001001 / 23 NOV 09
Criteria: SA
LAND ASAP
Push APU FIRE pushbutton.
Discharge agent after 10 s.
Shut down APU.
GLG A319-112 FLEET
AFM
C to D
EMER-26 P 2/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
SMOKE - FWD OR AFT CARGO SMOKE
APPROVED
Ident.: EMER-26-00009335.0004001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
E
EMER-26 P 3/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
SMOKE/FUMES/AVNCS SMOKE
APPROVED
Ident.: EMER-26-00007044.0006001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
F→
Continued on the following page
EMER-26 P 4/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
Turn off pack 2.
Continued from the previous page SMOKE/FUMES/AVNCS SMOKE
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.
GLG A319-112 FLEET
AFM
←F
EMER-26 P 5/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
REMOVAL OF SMOKE/FUMES
APPROVED
Ident.: EMER-26-00007045.0001001 / 14 JAN 15
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
GLG A319-112 FLEET
AFM
G→
EMER-26 P 6/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
Continued from the previous page REMOVAL OF SMOKE/FUMES
CAUTION
GLG A319-112 FLEET
AFM
Due to the increased noise level pay particular attention to visual warnings.
←G
EMER-26 P 7/8
16 MAR 15
EMERGENCY PROCEDURES
FIRE/SMOKE
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-26 P 8/8
16 MAR 15
EMERGENCY PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - L + R ELEV FAULT
APPROVED
Ident.: EMER-27-00007051.0001001 / 02 DEC 13
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
APPROVED
Ident.: EMER-27-00009325.0001001 / 23 NOV 09
Criteria: (SA and (28479 or 28916))
Set flaps lever to 0.
GLG A319-112 FLEET
AFM
A to B
EMER-27 P 1/2
14 DEC 13
EMERGENCY PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-27 P 2/2
14 DEC 13
EMERGENCY PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - G + B SYS LO PR
APPROVED
Ident.: EMER-29-00007048.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
A
EMER-29 P 1/4
14 DEC 13
EMERGENCY PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - B + Y SYS LO PR
APPROVED
Ident.: EMER-29-00007049.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
B
EMER-29 P 2/4
14 DEC 13
EMERGENCY PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - G + Y SYS LO PR
APPROVED
Ident.: EMER-29-00007050.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
C
EMER-29 P 3/4
14 DEC 13
EMERGENCY PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-29 P 4/4
14 DEC 13
EMERGENCY PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
L/G - GEAR NOT DOWNLOCKED
APPROVED
Ident.: EMER-32-00007052.0001001 / 04 APR 11
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
APPROVED
Ident.: EMER-32-00009809.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
EMER-32 P 1/2
25 AUG 15
EMERGENCY PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-32 P 2/2
25 AUG 15
EMERGENCY PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL V ALPHA PROT
APPROVED
Ident.: TDU / EMER-34-00016060.0001001 / 05 DEC 14
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).
GLG A319-112 FLEET
AFM
A
EMER-34 P 1/2
06 JAN 15
EMERGENCY PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
EMER-34 P 2/2
06 JAN 15
EMERGENCY PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
DUAL ENG FAILURE (BOTH ENGINES FLAME OUT)
APPROVED
Ident.: EMER-70-00007039.0011001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A→
Continued on the following page
EMER-70 P 1/2
25 JAN 11
EMERGENCY PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: EMER-70-00007040.0001001 / 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)
If OIL PR below 13 PSI:
Shut down affected engine.
GLG A319-112 FLEET
AFM
← A to B
EMER-70 P 2/2
25 JAN 11
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
STALL RECOVERY
APPROVED
Ident.: EMER-90-00013505.0001001 / 04 APR 11
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
APPROVED
Ident.: TDU / EMER-90-00016883.0001001 / 07 OCT 15
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.
GLG A319-112 FLEET
AFM
A to B
EMER-90 P 1/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
EMER DESCENT
APPROVED
Ident.: EMER-90-00006626.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
C
EMER-90 P 2/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY EVACUATION
APPROVED
Ident.: EMER-90-00006625.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D
EMER-90 P 3/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
DITCHING
APPROVED
Ident.: EMER-90-00006622.0002001 / 14 JAN 15
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).
GLG A319-112 FLEET
AFM
E→
Continued on the following page
EMER-90 P 4/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
Continued from the previous page DITCHING
Initiate evacuation.
Check emergency locator transmitter is emitting (if installed).
GLG A319-112 FLEET
AFM
←E
EMER-90 P 5/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
FORCED LANDING
APPROVED
Ident.: EMER-90-00006621.0002001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
Continued on the following page
F→
EMER-90 P 6/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
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).
GLG A319-112 FLEET
AFM
←F
EMER-90 P 7/8
12 SEP 17
EMERGENCY PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY LANDING (ALL ENGINES FAILURE)
APPROVED
Ident.: EMER-90-00021836.0002001 / 11 AUG 17
Criteria: (A319 or A320 or A321)
Start APU (if available).
Use FLAPS 2.
Approach speed:
GW(t)
GW(1000 lb)
VAPP(kt)
40
90
150
50
110
150
60
130
163
70
155
173
80
175
183
90
200
193
95
210
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.
GLG A319-112 FLEET
AFM
G
EMER-90 P 8/8
12 SEP 17
ABNORMAL PROCEDURES
Intentionally left blank
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
AUTO
AUTO
AUTO
FLT
FLT
FLT
FLT
- FCU 1(2) FAULT................................................................................................................................A
- RUD TRV LIM SYS............................................................................................................................B
- FAC 1+2 FAULT................................................................................................................................ C
- 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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 1/6
08 AUG 17
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 2/6
08 AUG 17
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
ELEC
ELEC
ELEC
ELEC
ELEC
ELEC
ELEC
ELEC
-
AC ESS BUS FAULT................................................................................................................................. A
AC BUS 1 FAULT...................................................................................................................................... B
AC BUS 2 FAULT...................................................................................................................................... C
DC ESS BUS FAULT.................................................................................................................................D
DC BUS 1 FAULT...................................................................................................................................... E
DC BUS 2 FAULT...................................................................................................................................... F
DC EMER CONFIG................................................................................................................................... G
DC BUS 1 + 2 FAULT............................................................................................................................... H
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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 3/6
08 AUG 17
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
F/CTL
F/CTL
F/CTL
F/CTL
F/CTL
F/CTL
F/CTL
F/CTL
TABLE OF CONTENTS
Continued from the previous page
- STOP RUDDER INPUT............................................................................................................................. L
- L (R) ELEV FAULT................................................................................................................................... M
- ELAC 1(2) FAULT..................................................................................................................................... N
- SEC FAULT...............................................................................................................................................O
- FCDC 1 + 2 FAULT...................................................................................................................................P
- STABILIZER JAM......................................................................................................................................Q
- ATLN LAW (PROT LOST).........................................................................................................................R
- 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
HYD
HYD
HYD
HYD
HYD
-
G SYS LO PR..............................................................................................................................................A
Y SYS LO PR.............................................................................................................................................. B
B SYS LO PR.............................................................................................................................................. C
RSVR LO AIR PR........................................................................................................................................D
RSVR OVHT................................................................................................................................................ E
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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 4/6
08 AUG 17
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
ABN-32 LANDING GEAR
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 5/6
08 AUG 17
ABNORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
ABN-70 POWER PLANT
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
ABN-PLP-TOC P 6/6
08 AUG 17
ABNORMAL PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: ABN-GEN-00007087.0001001 / 14 JAN 15
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
APPROVED
Ident.: ABN-GEN-00015178.0001001 / 14 JUL 17
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.
GLG A319-112 FLEET
AFM
A to B →
ABN-GEN P 1/2
08 AUG 17
ABNORMAL PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
Runway Condition
Dry
Wet
Compacted Snow
More than 3 mm of Dry or Wet Snow
More than 3 mm of Standing Water or Slush
Ice (Cold and Dry)
Max Reported Braking Action
6 - DRY
5 - GOOD
4 - GOOD to MEDIUM
3 - MEDIUM
2 - MEDIUM to POOR
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.
GLG A319-112 FLEET
AFM
←B
ABN-GEN P 2/2
08 AUG 17
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
ENGINE FAILURE BEFORE V1 (REJECTED TAKEOFF)
APPROVED
Ident.: ABN-OEI-TO-00007100.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
ABN-OEI-TO P 1/4
16 MAR 15
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
ENGINE FAILURE BETWEEN V1 AND V2
APPROVED
Ident.: ABN-OEI-TO-00007102.0001001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
B
ABN-OEI-TO P 2/4
16 MAR 15
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
ENGINE FAILURE DURING INITIAL CLIMB OUT
APPROVED
Ident.: ABN-OEI-TO-00007103.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
C
ABN-OEI-TO P 3/4
16 MAR 15
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
AIRPLANE FLIGHT MANUAL
TAKEOFF
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-OEI-TO P 4/4
16 MAR 15
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
APPROACH AND LANDING
AIRPLANE FLIGHT MANUAL
APPROACH AND LANDING
APPROVED
Ident.: ABN-OEI-LDG-00007104.0002001 / 02 DEC 13
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)
APPROVED
Ident.: ABN-OEI-LDG-00007105.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
ABN-OEI-LDG P 1/2
14 DEC 13
ABNORMAL PROCEDURES
ONE ENGINE INOPERATIVE
A319
APPROACH AND LANDING
AIRPLANE FLIGHT MANUAL
BALKED LANDING
APPROVED
Ident.: ABN-OEI-LDG-00007106.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
C
ABN-OEI-LDG P 2/2
14 DEC 13
ABNORMAL PROCEDURES
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
AIR - PACK 1 + 2 FAULT
APPROVED
Ident.: ABN-21-00007161.0001001 / 04 APR 11
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
APPROVED
Ident.: ABN-21-00006672.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-21-00007162.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C
ABN-21 P 1/2
05 DEC 11
ABNORMAL PROCEDURES
AIR COND/PRESS/VENT
A319
AIRPLANE FLIGHT MANUAL
COND - HOT AIR FAULT
APPROVED
Ident.: ABN-21-00007164.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-21-00007165.0001001 / 04 APR 11
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.
GLG A319-112 FLEET
AFM
D to E
ABN-21 P 2/2
05 DEC 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AUTO FLIGHT SYSTEM
AIRPLANE FLIGHT MANUAL
AUTO FLT - FCU 1(2) FAULT
APPROVED
Ident.: ABN-22-AUTOFLT-00009309.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-22-AUTOFLT-00006936.0005001 / 03 AUG 10
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
Criteria: ((318-121 or 318-122) or ((318-111 or 318-112 or A319) and (36847 or 37871)))
APPROVED
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
APPROVED
Ident.: ABN-22-AUTOFLT-00009310.0001001 / 03 AUG 10
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).
GLG A319-112 FLEET
AFM
A to D
ABN-22-AUTOFLT P 1/2
13 JUN 17
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
AUTO FLIGHT SYSTEM
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-22-AUTOFLT P 2/2
13 JUN 17
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
MULTIPLE FAILURES OR WARNINGS (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009313.0001001 / 23 NOV 09
Criteria: SA
In case of multiple failures or warnings, the most limiting applies.
ALTITUDE LOSS WITH AUTOPILOT MALFUNCTION (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009795.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009315.0001001 / 23 NOV 09
Criteria: SA
Revert to CAT I minima.
Disengage the autopilot no later than 500 ft.
ANTISKID SYSTEM AND/OR NOSEWHEEL STEERING FAILURE (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009338.0001001 / 23 NOV 09
Criteria: SA
Disconnect the autopilot at touchdown or when the failure occurs during landing roll.
GLG A319-112 FLEET
AFM
A to D
ABN-22-CATII P 1/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
ALPHA FLOOR ACTIVATION (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009342.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009343.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
E to F
ABN-22-CATII P 2/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
AIRPLANE FLIGHT MANUAL
RED "RA" FLAG ON TWO PFDS (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009344.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009349.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
G to H
ABN-22-CATII P 3/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
AIRPLANE FLIGHT MANUAL
RED "ATT" FLAG ON ONE PFD (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009350.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009351.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
I to J
ABN-22-CATII P 4/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
AMBER "CHECK HDG" FLAG ON TWO PFDS AND ON TWO NDS (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009352.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
K
ABN-22-CATII P 5/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
AIRPLANE FLIGHT MANUAL
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009353.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009354.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
L to M
ABN-22-CATII P 6/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
"AP OFF" WARNING (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009355.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009314.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
N to O
ABN-22-CATII P 7/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
AIRPLANE FLIGHT MANUAL
LOC OR G/S EXCESSIVE DEVIATION ON PFD (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009356.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009357.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATII-00009358.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
P to R
ABN-22-CATII P 8/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
NO "LAND" AT 350 FT (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009359.0001001 / 23 NOV 09
Criteria: SA
Go around or perform a manual landing if visual references are sufficient.
INCORRECT SELECTED COURSE AT 350 FT > 5 DEG (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009360.0001001 / 23 NOV 09
Criteria: SA
Continue the landing and disconnect autopilot at 50 ft at the latest.
NO "FLARE" AT 30 FT (CAT II)
APPROVED
Ident.: ABN-22-CATII-00009361.0001001 / 23 NOV 09
Criteria: SA
Disconnect the autopilot.
Land manually.
GLG A319-112 FLEET
AFM
S to U
ABN-22-CATII P 9/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT II
APPROACH WITH OR WITHOUT AUTOMATIC LANDING
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-22-CATII P 10/10
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
MULTIPLES FAILURES OR WARNINGS (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009366.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009383.0001001 / 23 NOV 09
Criteria: SA
Revert to CAT I minima.
Disconnect the autopilot no later than 500 ft.
NOSEWHEEL STEERING FAILURE (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009382.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C
ABN-22-CATIIIDH P 1/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
ANTISKID FAILURE (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009381.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009380.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D to E
ABN-22-CATIIIDH P 2/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
ONE ENGINE FAILURE (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009379.0002001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009378.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
F to G
ABN-22-CATIIIDH P 3/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
RED "RA" FLAG ON TWO PFDS (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009377.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
H
ABN-22-CATIIIDH P 4/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
AMBER "CHECK ATT" FLAG ON TWO PFDS (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009386.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
I
ABN-22-CATIIIDH P 5/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
RED "ATT" FLAG ON ONE PFD (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009385.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
J
ABN-22-CATIIIDH P 6/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
AMBER "CHECK HDG" FLAG ON TWO PFDS AND TWO NDS (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009376.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
K
ABN-22-CATIIIDH P 7/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009375.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
L
ABN-22-CATIIIDH P 8/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
RED "SPD" FLAG ON ONE PFD (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009374.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
M
ABN-22-CATIIIDH P 9/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
"AP OFF" WARNING (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009373.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009372.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
N to O
ABN-22-CATIIIDH P 10/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
TOTAL LOSS OF A/THR ("CAT 3" DECREASES TO "CAT 2") (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009384.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009371.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
P to Q
ABN-22-CATIIIDH P 11/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH DH
"AUTOLAND" LIGHT (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009370.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009369.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIIDH-00009368.0001001 / 23 NOV 09
Criteria: SA
Revert to CAT II minima.
Disconnect autopilot at 50 ft at the latest.
NO "FLARE" AT 30 FT (CAT III WITH DH)
APPROVED
Ident.: ABN-22-CATIIIDH-00009367.0001001 / 23 NOV 09
Criteria: SA
If visual references are not sufficient:
Go around.
If visual references are sufficient:
Disconnect autopilot.
Land manually.
GLG A319-112 FLEET
AFM
R to U
ABN-22-CATIIIDH P 12/12
25 JAN 11
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
MULTIPLE FAILURES OR WARNINGS (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009393.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009394.0001001 / 23 NOV 09
Criteria: SA
Revert to CAT I minima.
Disconnect autopilot no later than 500 ft.
NOSEWHEEL STEERING FAILURE (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009395.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C
ABN-22-CATIIInoDH P 1/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
ANTISKID FAILURE (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009396.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009397.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D to E
ABN-22-CATIIInoDH P 2/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
ONE ENGINE FAILURE (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009413.0002001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009398.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009399.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
F to H
ABN-22-CATIIInoDH P 3/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
AMBER "CHECK ATT" FLAG ON TWO PFDS (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009400.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
I
ABN-22-CATIIInoDH P 4/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
RED "ATT" FLAG ON ONE PFD (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009401.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
J
ABN-22-CATIIInoDH P 5/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
AMBER "CHECK HDG" FLAG ON TWO PFDS AND TWO NDS (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009402.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
K
ABN-22-CATIIInoDH P 6/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
RED "HDG" FLAG ON ONE PFD AND ONE ND (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009403.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
L
ABN-22-CATIIInoDH P 7/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
RED "SPD" FLAG ON ONE PFD (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009404.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009405.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
M to N
ABN-22-CATIIInoDH P 8/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
CAPABILITY DECREASE (EXCEPT IF DUE TO A/THR LOSS) (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009406.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009407.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
O to P
ABN-22-CATIIInoDH P 9/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
LOC OR G/S EXCESSIVE DEVIATION ON PFD (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009408.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009409.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009410.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009411.0001001 / 23 NOV 09
Criteria: SA
Revert to CAT II minima.
Disconnect autopilot at 50 ft at the latest.
GLG A319-112 FLEET
AFM
Q to T
ABN-22-CATIIInoDH P 10/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
NO "FLARE" AT 30 FT (CAT III NO DH)
APPROVED
Ident.: ABN-22-CATIIInoDH-00009412.0001001 / 23 NOV 09
Criteria: SA
If visual references are not sufficient:
Go around.
If visual references are sufficient:
Disconnect autopilot.
Land manually.
GLG A319-112 FLEET
AFM
U
ABN-22-CATIIInoDH P 11/12
14 DEC 13
ABNORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FAILURES OR WARNINGS DURING A CAT III APPROACH WITH NO DH
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-22-CATIIInoDH P 12/12
14 DEC 13
ABNORMAL PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELEC - AC ESS BUS FAULT
APPROVED
Ident.: ABN-24-00007139.0002001 / 23 NOV 09
Criteria: (SA and 37871)
Set AC ESS FEED to ALTN.
Set ATC/XPDR to SYS 2.
ELEC - AC BUS 1 FAULT
APPROVED
Ident.: ABN-24-00007140.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-24-00007141.0001001 / 23 NOV 09
Criteria: SA
Set ventilation extract to OVRD.
GLG A319-112 FLEET
AFM
A to C
ABN-24 P 1/4
10 SEP 14
ABNORMAL PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELEC - DC ESS BUS FAULT
APPROVED
Ident.: ABN-24-00007143.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-24-00007148.0002001 / 02 DEC 13
Criteria: (SA and 151269)
Set ventilation blower to OVRD.
Set ventilation extract to OVRD.
Avoid icing conditions.
GLG A319-112 FLEET
AFM
D to E
ABN-24 P 2/4
10 SEP 14
ABNORMAL PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELEC - DC BUS 2 FAULT
APPROVED
Ident.: ABN-24-00007150.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-24-00007152.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-24-00007154.0002001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
F to H
ABN-24 P 3/4
10 SEP 14
ABNORMAL PROCEDURES
ELECTRICAL POWER
A319
AIRPLANE FLIGHT MANUAL
ELEC - DC ESS BUS SHED
APPROVED
Ident.: ABN-24-00007159.0002001 / 02 DEC 13
Criteria: (SA and 151269)
Set ventilation extract to OVRD.
Avoid icing conditions.
GLG A319-112 FLEET
AFM
I
ABN-24 P 4/4
10 SEP 14
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - FLAPS FAULT
APPROVED
Ident.: ABN-27-00007108.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-27-00006637.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
ABN-27 P 1/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - SLATS FAULT
APPROVED
Ident.: ABN-27-00007109.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-27-00006638.0002001 / 23 NOV 09
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).
GLG A319-112 FLEET
AFM
C to D
ABN-27 P 2/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
APPROACH SPEED INCREMENT AND LANDING DISTANCE MULTIPLICATION FACTOR
APPROVED
Ident.: ABN-27-00006879.0005001 / 02 DEC 13
Criteria: A319
Slats at or
above 0
and below 1
Slats at or
above 1 and
at or below 3
Slats above 3
(1)
APPROACH SPEED INCREMENT
LANDING DISTANCE MULTIPLICATION FACTOR
Flaps at or above Flaps at or above Flaps at or above
Flaps at 3
0 and below 1+F
1+F and below 2
2 and below 3
Flaps above 3
VREF + 30 kt
VREF + 25 kt
VREF + 25 kt
not allowed
VREF + 25 kt
VREF + 15 kt
VREF + 10 kt
VREF + 10 kt
VREF + 10 kt
VREF + 25 kt
VREF + 15 kt
VREF + 10 kt
VREF + 5 kt
VREF + 5 kt
VREF + 45 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.
GLG A319-112 FLEET
AFM
E
ABN-27 P 3/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE LIMITATION FOR LANDING IN CLEAN CONFIGURATION
APPROVED
Ident.: ABN-27-00007110.0003001 / 03 AUG 10
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
GLG A319-112 FLEET
AFM
F→
Continued on the following page
ABN-27 P 4/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: ABN-27-00006639.0001001 / 02 DEC 13
Criteria: SA
If spoilers 3+4 affected:
Do not use speed brakes.
For landing:
Apply necessary landing performance corrections.
F/CTL - GND SPLR FAULT
APPROVED
Ident.: ABN-27-00007114.0001001 / 23 NOV 09
Criteria: SA
Refer to ABN-27 F/CTL - SPLR FAULT.
F/CTL - SPD BRK DISAGREE
APPROVED
Ident.: ABN-27-00007117.0001001 / 23 NOV 09
Criteria: SA
Retract speed brakes.
Refer to ABN-27 F/CTL - SPLR FAULT.
F/CTL - SPD BRK FAULT
APPROVED
Ident.: ABN-27-00007118.0001001 / 23 NOV 09
Criteria: SA
Refer to ABN-27 F/CTL - SPLR FAULT.
Note:
Associated ground spoilers are only available through thrust reversers selection.
GLG A319-112 FLEET
AFM
← F to J
ABN-27 P 5/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - RUDDER JAM
APPROVED
Ident.: ABN-27-00007119.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-27-00015241.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-27-00007120.0004001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
K to M
ABN-27 P 6/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - ELAC 1(2) FAULT
APPROVED
Ident.: ABN-27-00007121.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-27-00006640.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
N to O
ABN-27 P 7/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - FCDC 1 + 2 FAULT
APPROVED
Ident.: ABN-27-00007131.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-27-00007132.0001001 / 23 NOV 09
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)
APPROVED
Ident.: ABN-27-00006618.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
P to R
ABN-27 P 8/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
F/CTL - DIRECT LAW (PROT LOST)
APPROVED
Ident.: ABN-27-00006671.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
S
ABN-27 P 9/10
08 AUG 17
ABNORMAL PROCEDURES
FLIGHT CONTROLS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-27 P 10/10
08 AUG 17
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL - L(R) TK PUMP 1+2 LO PR
APPROVED
Ident.: ABN-28-00007194.0002001 / 23 NOV 09
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
APPROVED
Ident.: ABN-28-00007198.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
ABN-28 P 1/6
10 SEP 14
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL - L+R WING TK LO LVL
APPROVED
Ident.: ABN-28-00007200.0004001 / 02 DEC 13
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
APPROVED
Ident.: ABN-28-00009364.0003001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
C to D
ABN-28 P 2/6
10 SEP 14
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL GRAVITY FEEDING
APPROVED
Ident.: ABN-28-00006624.0001001 / 23 NOV 09
Criteria: SA
Descend to gravity feed ceiling (if applicable):
Flight conditions at the time of gravity feeding
Flight time above FL 300 greater
than 30 min (Fuel deaerated)
Flight time above FL 300 lower
than 30 min (Fuel non-deaerated)
Aircraft flight level never exceeded
FL 300 (Fuel non-deaerated)
(1)
Gravity feed ceiling
Current FL (1)
FL 300 (1)
The highest of:
‐ FL 150 (1)
‐ 7 000 ft above takeoff airport altitude
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:
GLG A319-112 FLEET
AFM
Fuel from opposite wing is used until imbalance is reduced to 0.
E
ABN-28 P 3/6
10 SEP 14
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL - L INNER (R INNER) (L OUTER) (R OUTER) TK HI TEMP
APPROVED
Ident.: ABN-28-00007201.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-28-00007203.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
F to G
ABN-28 P 4/6
10 SEP 14
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL LEAK
APPROVED
Ident.: ABN-28-00006692.0003001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
H→
ABN-28 P 5/6
10 SEP 14
ABNORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
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
GLG A319-112 FLEET
AFM
Do not use reverse.
←H
ABN-28 P 6/6
10 SEP 14
ABNORMAL PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - G SYS LO PR
APPROVED
Ident.: ABN-29-00006656.0005001 / 02 DEC 13
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
APPROVED
Ident.: ABN-29-00006657.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-29-00006658.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
A to C
ABN-29 P 1/4
14 DEC 13
ABNORMAL PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - RSVR LO AIR PR
APPROVED
Ident.: ABN-29-00009203.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-29-00009204.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D to E
ABN-29 P 2/4
14 DEC 13
ABNORMAL PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
HYD - RSVR LO LVL
APPROVED
Ident.: ABN-29-00009205.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
F
ABN-29 P 3/4
14 DEC 13
ABNORMAL PROCEDURES
HYDRAULIC
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-29 P 4/4
14 DEC 13
ABNORMAL PROCEDURES
ICE AND RAIN PROTECTION
A319
AIRPLANE FLIGHT MANUAL
ANTI ICE - CAPT (F/O) PROBES HEAT FAULT
APPROVED
Ident.: ABN-30-00007178.0001001 / 23 NOV 09
Criteria: SA
If ADR 3 available:
Use AIR DATA switching as appropriate.
DOUBLE AOA HEAT FAILURE
APPROVED
Ident.: ABN-30-00007179.0002001 / 23 NOV 09
Criteria: (SA and 31283)
If icing conditions cannot be avoided:
Turn off one of affected ADRs.
WING A.ICE - SYS FAULT OR OFF
APPROVED
Ident.: ABN-30-00006619.0012001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
A to C
ABN-30 P 1/2
16 MAR 15
ABNORMAL PROCEDURES
ICE AND RAIN PROTECTION
A319
AIRPLANE FLIGHT MANUAL
ANTI ICE - CAPT + F/O (CAPT + STBY) (F/O + STBY) PITOT HEAT FAULT
APPROVED
Ident.: ABN-30-00009388.0002001 / 23 NOV 09
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
APPROVED
Ident.: ABN-30-00009389.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D to E
ABN-30 P 2/2
16 MAR 15
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
A319
AIRPLANE FLIGHT MANUAL
FWS - FWC 1 + 2 FAULT
APPROVED
Ident.: ABN-31-00007209.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-31-00007210.0001001 / 23 NOV 09
Criteria: SA
Monitor overhead panel.
Note:
Only ECAM ENG, FUEL, F/CTL, WHEEL pages are available.
GLG A319-112 FLEET
AFM
A to B
ABN-31 P 1/4
14 DEC 13
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
A319
AIRPLANE FLIGHT MANUAL
DISPLAY UNIT FAILURE
APPROVED
Ident.: ABN-31-00007211.0001001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
C→
Continued on the following page
ABN-31 P 2/4
14 DEC 13
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
A319
AIRPLANE FLIGHT MANUAL
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.
GLG A319-112 FLEET
AFM
←C
ABN-31 P 3/4
14 DEC 13
ABNORMAL PROCEDURES
INDICATING/RECORDING SYSTEM
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-31 P 4/4
14 DEC 13
ABNORMAL PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
L/G GRAVITY EXTENSION
APPROVED
Ident.: ABN-32-00006663.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-32-00007168.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-32-00007169.0001001 / 23 NOV 09
Criteria: SA
Maximum speed: VLE
Keep landing gear down.
GLG A319-112 FLEET
AFM
A to C
ABN-32 P 1/4
10 SEP 14
ABNORMAL PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
L/G - SHOCK ABSORBER FAULT
APPROVED
Ident.: ABN-32-00007170.0002001 / 23 NOV 09
Criteria: (SA and 37871)
If landing gear not uplocked:
Maximum speed: VLE.
Keep landing gear down.
L/G - DOORS NOT CLOSED
APPROVED
Ident.: ABN-32-00007171.0001001 / 23 NOV 09
Criteria: SA
When speed below VLO (Retraction):
Recycle landing gear.
If unsuccessful:
Maximum speed: VLO (Extension)
BRAKES - A-SKID N-WS FAULT OR OFF
APPROVED
Ident.: ABN-32-00006623.0005001 / 02 DEC 13
Criteria: SA
Apply maximum brake pressure 1 000 PSI.
Note:
Nosewheel steering is inoperative.
Apply necessary landing performance corrections.
BRAKES - AUTO BRK FAULT
APPROVED
Ident.: ABN-32-00007175.0001001 / 02 DEC 13
Criteria: (A319 or A320 or A321)
Apply necessary landing performance corrections.
GLG A319-112 FLEET
AFM
D to G
ABN-32 P 2/4
10 SEP 14
ABNORMAL PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
BRAKES - HOT
APPROVED
Ident.: ABN-32-00007176.0004001 / 02 DEC 13
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
APPROVED
Ident.: ABN-32-00007177.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
H to I
ABN-32 P 3/4
10 SEP 14
ABNORMAL PROCEDURES
LANDING GEAR
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-32 P 4/4
10 SEP 14
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
NAV - RA 1+2 FAULT
APPROVED
Ident.: ABN-34-00007212.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-34-00007213.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-34-00007214.0001001 / 23 NOV 09
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).
GLG A319-112 FLEET
AFM
A to C
ABN-34 P 1/6
11 JUL 17
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
NAV - ADR 1+2 FAULT
APPROVED
Ident.: ABN-34-00007186.0001001 / 15 MAY 17
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
APPROVED
Ident.: ABN-34-00007187.0002001 / 15 MAY 17
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
APPROVED
Ident.: ABN-34-00009566.0002001 / 15 MAY 17
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.
GLG A319-112 FLEET
AFM
D to F
ABN-34 P 2/6
11 JUL 17
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
ADR 1+2+3 FAULT
APPROVED
Ident.: ABN-34-00006691.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-34-00007192.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
G to H
ABN-34 P 3/6
11 JUL 17
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
UNRELIABLE AIRSPEED INDICATION
APPROVED
Ident.: TDU / ABN-34-00009811.0003001 / 11 FEB 16
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.
GLG A319-112 FLEET
AFM
Continued on the following page
I→
ABN-34 P 4/6
11 JUL 17
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
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.
GLG A319-112 FLEET
AFM
←I
ABN-34 P 5/6
11 JUL 17
ABNORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
UNRELIABLE AIRSPEED INDICATION
APPROVED
Ident.: ABN-34-00006690.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
J
ABN-34 P 6/6
11 JUL 17
ABNORMAL PROCEDURES
PNEUMATIC
A319
AIRPLANE FLIGHT MANUAL
AIR - ENG 1(2) BLEED HI TEMP
APPROVED
Ident.: ABN-36-00015197.0001001 / 02 DEC 13
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
APPROVED
Ident.: ABN-36-00007180.0004001 / 02 DEC 13
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
APPROVED
Ident.: ABN-36-00007181.0004001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
A to C
ABN-36 P 1/4
10 SEP 14
ABNORMAL PROCEDURES
PNEUMATIC
A319
AIRPLANE FLIGHT MANUAL
AIR - X BLEED FAULT
APPROVED
Ident.: ABN-36-00007184.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-36-00007188.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-36-00007190.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D to F
ABN-36 P 2/4
10 SEP 14
ABNORMAL PROCEDURES
PNEUMATIC
A319
AIRPLANE FLIGHT MANUAL
AIR - ENG 1(2) BLEED LO TEMP
APPROVED
Ident.: ABN-36-00009345.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-36-00009346.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
G to H
ABN-36 P 3/4
10 SEP 14
ABNORMAL PROCEDURES
PNEUMATIC
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-36 P 4/4
10 SEP 14
ABNORMAL PROCEDURES
DOORS
A319
AIRPLANE FLIGHT MANUAL
DOOR - DOOR NOT CLOSED
APPROVED
Ident.: ABN-52-00010780.0001001 / 04 APR 11
Criteria: SA
If abnormal cabin vertical speed:
Maximum flight level is the higher one of: FL 100 or MEA.
GLG A319-112 FLEET
AFM
A
ABN-52 P 1/2
08 APR 11
ABNORMAL PROCEDURES
DOORS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-52 P 2/2
08 APR 11
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG - STALL
APPROVED
Ident.: TDU / ABN-70-00016178.0001001 / 03 SEP 15
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
APPROVED
Ident.: TDU / ABN-70-00009732.0001001 / 21 OCT 09
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.
GLG A319-112 FLEET
AFM
A to B
ABN-70 P 1/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG - FAIL
APPROVED
Ident.: ABN-70-00006885.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-70-00007091.0001001 / 23 NOV 09
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
APPROVED
Ident.: ABN-70-00007092.0001001 / 23 NOV 09
Criteria: SA
Set affected engine thrust lever to idle.
GLG A319-112 FLEET
AFM
C to E
ABN-70 P 2/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG - REVERSE UNLOCKED
APPROVED
Ident.: ABN-70-00007093.0002001 / 02 DEC 13
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
APPROVED
Ident.: ABN-70-00009156.0001001 / 23 NOV 09
Criteria: (SA and 30660)
If FADEC sets affected engine to idle:
LAND ASAP
Set affected engine thrust lever to idle.
GLG A319-112 FLEET
AFM
F to G
ABN-70 P 3/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG - THR LEVER FAULT
APPROVED
Ident.: ABN-70-00009157.0001001 / 23 NOV 09
Criteria: (SA and 30660)
LAND ASAP
Engage autothrust (if not already engaged).
ENG - THR LEVER DISAGREE
APPROVED
Ident.: ABN-70-00009158.0001001 / 23 NOV 09
Criteria: (SA and 30660)
LAND ASAP
Engage autothrust (if not already engaged).
ENG - OIL HI TEMP
APPROVED
Ident.: ABN-70-00007095.0001001 / 23 NOV 09
Criteria: SA
Shut down affected engine.
ENG - FADEC FAULT
APPROVED
Ident.: ABN-70-00007096.0004001 / 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) 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.
GLG A319-112 FLEET
AFM
H to K
ABN-70 P 4/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG - FADEC HI TEMP (FADEC OVHT)
APPROVED
Ident.: ABN-70-00007097.0002001 / 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) 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
APPROVED
Ident.: ABN-70-00007098.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
L to M
ABN-70 P 5/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
ENG RELIGHT IN FLIGHT
APPROVED
Ident.: ABN-70-00006620.0009001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
Continued on the following page
N→
ABN-70 P 6/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
Continued from the previous page ENG RELIGHT IN FLIGHT
In Flight Engine Relight Envelope
GLG A319-112 FLEET
AFM
←N
ABN-70 P 7/8
22 SEP 15
ABNORMAL PROCEDURES
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-70 P 8/8
22 SEP 15
ABNORMAL PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
BOMB ON BOARD
APPROVED
Ident.: ABN-90-00007024.0002001 / 04 APR 11
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.
GLG A319-112 FLEET
AFM
A→
Continued on the following page
ABN-90 P 1/4
08 APR 11
ABNORMAL PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: ABN-90-00007107.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
← A to B
ABN-90 P 2/4
08 APR 11
ABNORMAL PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
REJECTED TAKEOFF WITH ALL ENGINES OPERATIVE
APPROVED
Ident.: ABN-90-00007183.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
C
ABN-90 P 3/4
08 APR 11
ABNORMAL PROCEDURES
MISCELLANEOUS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
ABN-90 P 4/4
08 APR 11
NORMAL PROCEDURES
Intentionally left blank
NORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
NORM-PLP-TOC P 1/2
10 OCT 17
NORMAL PROCEDURES
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
NORM-28 FUEL
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
NORM-PLP-TOC P 2/2
10 OCT 17
NORMAL PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: NORM-GEN-00009222.0001001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
A
NORM-GEN P 1/2
16 MAR 15
NORMAL PROCEDURES
GENERAL
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-GEN P 2/2
16 MAR 15
NORMAL PROCEDURES
PREFLIGHT CHECKS
A319
AIRPLANE FLIGHT MANUAL
ELECTRICAL
APPROVED
Ident.: NORM-PFLT-00007056.0002001 / 23 NOV 09
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
APPROVED
Ident.: NORM-PFLT-00007057.0001001 / 23 NOV 09
Criteria: SA
If required by local Airworthiness Authorities:
Check that the cockpit door is closed and locked before each flight.
BRAKING EFFICIENCY TEST
APPROVED
Ident.: NORM-PFLT-00007058.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C
NORM-PFLT P 1/2
10 OCT 17
NORMAL PROCEDURES
PREFLIGHT CHECKS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-PFLT P 2/2
10 OCT 17
NORMAL PROCEDURES
TAKEOFF
A319
AIRPLANE FLIGHT MANUAL
TAKEOFF PROCEDURE
APPROVED
Ident.: NORM-TO-00007059.0001001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
A→
NORM-TO P 1/2
16 MAR 15
NORMAL PROCEDURES
TAKEOFF
A319
AIRPLANE FLIGHT MANUAL
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.
GLG A319-112 FLEET
AFM
←A
NORM-TO P 2/2
16 MAR 15
NORMAL PROCEDURES
FLIGHT
A319
AIRPLANE FLIGHT MANUAL
BUFFET ONSET
APPROVED
Ident.: NORM-FLT-00007063.0003001 / 03 AUG 10
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
GLG A319-112 FLEET
AFM
A→
NORM-FLT P 1/4
07 MAR 17
NORMAL PROCEDURES
FLIGHT
A319
AIRPLANE FLIGHT MANUAL
BUFFET ONSET (Weight in kg)
GLG A319-112 FLEET
AFM
←A→
NORM-FLT P 2/4
07 MAR 17
NORMAL PROCEDURES
FLIGHT
A319
AIRPLANE FLIGHT MANUAL
BUFFET ONSET (Weight in lb)
FLIGHT IN SEVERE TURBULENCE
APPROVED
Ident.: NORM-FLT-00007066.0007001 / 14 FEB 17
Criteria: A319
Turn on seat belts signs.
Disconnect autothrust.
GLG A319-112 FLEET
AFM
← A to B →
NORM-FLT P 3/4
07 MAR 17
NORMAL PROCEDURES
FLIGHT
A319
AIRPLANE FLIGHT MANUAL
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
GLG A319-112 FLEET
AFM
←B
NORM-FLT P 4/4
07 MAR 17
NORMAL PROCEDURES
APPROACH AND LANDING
A319
AIRPLANE FLIGHT MANUAL
NORMAL LANDING
APPROVED
Ident.: NORM-LDG-00007067.0001001 / 23 NOV 09
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)
APPROVED
Ident.: NORM-LDG-00007068.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-LDG-00007069.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-LDG-00007070.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to D →
NORM-LDG P 1/2
25 JAN 11
NORMAL PROCEDURES
APPROACH AND LANDING
A319
AIRPLANE FLIGHT MANUAL
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.
GLG A319-112 FLEET
AFM
←D
NORM-LDG P 2/2
25 JAN 11
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
DEMONSTRATED SYSTEM CONFIGURATION
AIRPLANE FLIGHT MANUAL
AP/FD, SPEED MODES, AUTOTHRUST
APPROVED
Ident.: NORM-22-CONF-00009463.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009464.0001001 / 02 DEC 13
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
APPROVED
Ident.: NORM-22-CONF-00009465.0002001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009466.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009467.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to E
NORM-22-CONF P 1/2
13 JUN 17
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
DEMONSTRATED SYSTEM CONFIGURATION
AIRPLANE FLIGHT MANUAL
CAT II ILS APPROACH
APPROVED
Ident.: NORM-22-CONF-00009468.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009469.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009470.0001001 / 23 NOV 09
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
APPROVED
Ident.: NORM-22-CONF-00009472.0003001 / 23 NOV 09
Criteria: (319-111 or 319-112 or 319-113 or 319-114 or 319-115)
Initiation Height (ft)
50 ft to 100 ft
40 ft
30 ft
20 ft
GLG A319-112 FLEET
AFM
Height Loss (ft)
30 ft
25 ft
20 ft
15 ft
F to I
NORM-22-CONF P 2/2
13 JUN 17
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
NON PRECISION APPROACH
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: NORM-22-NPA-00009575.0001001 / 02 DEC 13
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
APPROVED
Ident.: NORM-22-NPA-00009576.0004001 / 02 DEC 13
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.
GLG A319-112 FLEET
AFM
A to B
NORM-22-NPA P 1/2
14 DEC 13
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
NON PRECISION APPROACH
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-22-NPA P 2/2
14 DEC 13
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
PRECISION APPROACH
AIRPLANE FLIGHT MANUAL
CAT II AND CAT III APPROACH AND/OR AUTOMATIC LANDING
APPROVED
Ident.: NORM-22-PA-00009482.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A→
NORM-22-PA P 1/4
16 MAR 15
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
PRECISION APPROACH
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: NORM-22-PA-00009476.0001001 / 14 JAN 15
Criteria: SA
Required Equipment
AP
AP disconnect P/B
Autothrust
ILS or MLS Receiver
Attitude Indication
PFD/ND Displays
Radio Altimeter
Auto Callout Radio Altimeter
DH Indication
Flight Warning Computer
"AP OFF" warning
"AUTOLAND" light
GLG A319-112 FLEET
AFM
CAT II
1 AP engaged
2
0
2
N°1+N°2+STBY
2/1
1 (But two display)
1(3)
1(1)
1
1
1
← A to B →
CAT III Single
CAT III Dual
1 AP engaged
2 AP engaged
2
2
1
1
2
2
N°1+N°2+STBY
N°1+N°2+STBY
2/2
2/2
2
2
1
1
1(1)
1(1)
1
2
1
2
1
1
Continued on the following page
NORM-22-PA P 2/4
16 MAR 15
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
PRECISION APPROACH
AIRPLANE FLIGHT MANUAL
Required Equipment
Rain Repellent (if activated)
or Windshield Wipers
Windshield Heat
Nosewheel steering
Antiskid
BSCU Channel
Beam Excessive Deviation
FMA
"A/THR OFF" caution
Rudder Travel Limit
Yaw Damper/Rudder Trim
ELAC
ADR/IR
FAC
Hydraulic Circuit
FMGC Electrical Supply Split
Continued from the previous page
CAT III Single
CAT III Dual
CAT II
1(2)
1(2)
1(2)
1(2)
1(5)
1(5)
1(5)
1(1)
1
0
1(4)
1/1
1
2/2
1
2
0
1(2)
1(5)
1(5)
1(5)
2
2
1
1(4)
1/1
1
2/2
1
2
0
1(2)
1
1
1
2
2
1
1(4)
2/2
2
3/3
2
3
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.
GLG A319-112 FLEET
AFM
←B
NORM-22-PA P 3/4
16 MAR 15
NORMAL PROCEDURES
AUTO FLIGHT SYSTEM
A319
AIRPLANE FLIGHT MANUAL
PRECISION APPROACH
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-22-PA P 4/4
16 MAR 15
NORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
FUEL SYSTEM
APPROVED
Ident.: NORM-28-00009172.0001001 / 23 NOV 09
Criteria: ((A320 and 20024) or (A318 or A319 or A321))
Tanks must be emptied in the following order:
1. Center tank
2. Wing tanks.
GLG A319-112 FLEET
AFM
A
NORM-28 P 1/2
25 JAN 11
NORMAL PROCEDURES
FUEL
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-28 P 2/2
25 JAN 11
NORMAL PROCEDURES
ICE AND RAIN PROTECTION
A319
AIRPLANE FLIGHT MANUAL
OPERATIONS IN ICING CONDITIONS
APPROVED
Ident.: NORM-30-00007071.0001001 / 23 NOV 09
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)
APPROVED
Ident.: NORM-30-00007080.0001001 / 23 NOV 09
Criteria: SA
Use rain repellent in the case of heavy rain only.
GLG A319-112 FLEET
AFM
A to B
NORM-30 P 1/2
25 JAN 11
NORMAL PROCEDURES
ICE AND RAIN PROTECTION
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-30 P 2/2
25 JAN 11
NORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
GROUND PROXIMITY WARNING SYSTEM (GPWS)
APPROVED
Ident.: NORM-34-00007081.0001001 / 23 NOV 09
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)
APPROVED
Ident.: NORM-34-00009174.0001001 / 23 NOV 09
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)
APPROVED
Ident.: NORM-34-00009175.0002001 / 23 NOV 09
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
ADR
ATC Transponder
Flight Warning Computer (for Altitude Alert function)
Autopilot
PFD function (for altitude indication)
FCU (for altitude target selection and
OP CLB/OP DES mode engagement)
Quantity
2
1
1
1
2
1
Minimum Equipment/Functions Required to begin RVSM Operation
GLG A319-112 FLEET
AFM
A to C
NORM-34 P 1/2
13 JUN 17
NORMAL PROCEDURES
NAVIGATION
A319
AIRPLANE FLIGHT MANUAL
WINDSHEAR WARNING AND GUIDANCE SYSTEM
APPROVED
Ident.: NORM-34-00009761.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
D
NORM-34 P 2/2
13 JUN 17
NORMAL PROCEDURES
AUXILIARY POWER UNIT
A319
AIRPLANE FLIGHT MANUAL
AUXILIARY POWER UNIT (APU)
APPROVED
Ident.: NORM-49-00006923.0009001 / 23 NOV 09
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).
GLG A319-112 FLEET
AFM
A
NORM-49 P 1/2
25 JAN 11
NORMAL PROCEDURES
AUXILIARY POWER UNIT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
NORM-49 P 2/2
25 JAN 11
PERFORMANCE
Intentionally left blank
PERFORMANCE
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
1
PERF-OCTO PERFORMANCE DATABASE
General.....................................................................................................................................................................A
Performance Database............................................................................................................................................ B
Complementary Performance Data File .................................................................................................................C
Continued on the following page
GLG A319-112 FLEET
AFM
PERF-PLP-TOC P 1/2
12 DEC 17
PERFORMANCE
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
PERF-ENG ENGINE MANAGEMENT
TABLE OF CONTENTS
Continued from the previous page
Takeoff Thrust..........................................................................................................................................................A
Maximum Continuous Thrust...................................................................................................................................B
Go-Around Thrust.................................................................................................................................................... C
PERF-FLEX REDUCED THRUST TAKEOFF
Reduced Thrust Takeoff.......................................................................................................................................... A
GLG A319-112 FLEET
AFM
PERF-PLP-TOC P 2/2
12 DEC 17
PERFORMANCE
PRELIMINARY PAGES
A319
SUMMARY OF HIGHLIGHTS
AIRPLANE FLIGHT MANUAL
Localization
Title
PERF-PLP-TOC
PERFORMANCE DATABASE
PERF-OCTO
Complementary Performance Data
File
GLG A319-112 FLEET
AFM
Toc
Index
ID
Reason
1
C
1
Documentation update: Deletion of the "00021722.0001001
Complementary Performance Data File" documentary unit.
Documentation update: Addition of "Complementary Performance
Data File" documentary unit
PERF-PLP-SOH P 1/2
12 DEC 17
PERFORMANCE
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
SUMMARY OF HIGHLIGHTS
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-PLP-SOH P 2/2
12 DEC 17
PERFORMANCE
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: PERF-GEN-00006988.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
PERF-GEN P 1/2
25 JAN 11
PERFORMANCE
GENERAL
A319
AIRPLANE FLIGHT MANUAL
AIRCRAFT CONFIGURATION
APPROVED
Ident.: PERF-GEN-00007266.0001001 / 23 NOV 09
Criteria: (A319 or A320 or A321)
The performance has been established in the following configuration :
Slats / Flaps
1+F
2
3
Engine Thrust
Takeoff thrust
En route
0
Go-around
2
3
3
FULL
Maximum Continuous Thrust
(MCT)
Go-around thrust taking
Mach number into account
Takeoff
Landing
Remarks
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.
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
APPROVED
Ident.: PERF-GEN-00007267.0001001 / 03 AUG 10
Criteria: (A319 or A320 or A321)
At takeoff and landing: 38 kt (gust included).
GLG A319-112 FLEET
AFM
B to C
PERF-GEN P 2/2
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
SPEED CORRECTIONS IN GROUND EFFECT
APPROVED
Ident.: PERF-CAL-TO-00007268.0003001 / 23 NOV 09
Criteria: A319
CAPTAIN AND FIRST OFFICER ADR 1 OR 2
ADR 3
GLG A319-112 FLEET
AFM
A→
PERF-CAL-TO P 1/4
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
STANDBY AIRSPEED INDICATOR
GLG A319-112 FLEET
AFM
←A
PERF-CAL-TO P 2/4
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
SPEED CORRECTIONS OUT OF GROUND EFFECT
APPROVED
Ident.: PERF-CAL-TO-00007269.0004001 / 23 NOV 09
Criteria: A319
ADR 1 OR 2 OR 3
ΔV = IAS - CAS ≤ ± 1 kt
STANDBY AIRSPEED INDICATOR
CONF. 1
CONF. 2
CONF. 3
GLG A319-112 FLEET
AFM
B
PERF-CAL-TO P 3/4
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
TAKEOFF
AIRPLANE FLIGHT MANUAL
ALTITUDE CORRECTIONS
APPROVED
Ident.: PERF-CAL-TO-00007270.0004001 / 23 NOV 09
Criteria: A319
ADR 1 OR 2 OR 3
ΔZP ≤ ± 20 ft
STANDBY ALTITUDE INDICATOR
CONF. 1
CONF. 2
CONF. 3 L/G UP
GLG A319-112 FLEET
AFM
C
PERF-CAL-TO P 4/4
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
CRUISE (CLEAN CONFIGURATION)
AIRPLANE FLIGHT MANUAL
SPEED AND MACH CORRECTIONS
APPROVED
Ident.: PERF-CAL-CRU-00007271.0002001 / 23 NOV 09
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
APPROVED
Ident.: PERF-CAL-CRU-00007272.0002001 / 23 NOV 09
Criteria: (((A320 or A321) and (25490 or 25570)) or A319)
ADR 1 OR 2 OR 3
ΔZP ≤ ± 150 ft
GLG A319-112 FLEET
AFM
A to B
PERF-CAL-CRU P 1/2
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
AIRPLANE FLIGHT MANUAL
CRUISE (CLEAN CONFIGURATION)
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-CAL-CRU P 2/2
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
SPEED CORRECTIONS IN GROUND EFFECT
APPROVED
Ident.: PERF-CAL-LDG-00007273.0003001 / 23 NOV 09
Criteria: A319
CAPTAIN AND FIRST OFFICER ADR 1 OR 2
ADR 3
GLG A319-112 FLEET
AFM
A→
PERF-CAL-LDG P 1/6
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
STANDBY AIRSPEED INDICATOR
GLG A319-112 FLEET
AFM
←A
PERF-CAL-LDG P 2/6
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
SPEED CORRECTIONS OUT OF GROUND EFFECT
APPROVED
Ident.: PERF-CAL-LDG-00007274.0004001 / 03 AUG 10
Criteria: A319
ADR 1 OR 2 OR 3
ΔV = IAS - CAS ≤ ± 1 kt
STANDBY AIRSPEED INDICATOR
CONF 3 LANDING GEAR DOWN
GLG A319-112 FLEET
AFM
B→
PERF-CAL-LDG P 3/6
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
CONF FULL
GLG A319-112 FLEET
AFM
←B
PERF-CAL-LDG P 4/6
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
ALTITUDE CORRECTIONS
APPROVED
Ident.: PERF-CAL-LDG-00007275.0004001 / 03 AUG 10
Criteria: A319
ADR 1 OR 2 OR 3
ΔZP ≤ ± 20 ft
STANDBY ALTITUDE INDICATOR
CONF 3 LANDING GEAR DOWN
GLG A319-112 FLEET
AFM
C→
PERF-CAL-LDG P 5/6
25 JAN 11
PERFORMANCE
AIRSPEED AND ALTITUDE CALIBRATION
A319
LANDING
AIRPLANE FLIGHT MANUAL
CONF FULL
GLG A319-112 FLEET
AFM
←C
PERF-CAL-LDG P 6/6
25 JAN 11
PERFORMANCE
TAKEOFF PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
SPEEDS DEFINITIONS
APPROVED
Ident.: PERF-TO-00006991.0001001 / 23 NOV 09
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 %).
GLG A319-112 FLEET
AFM
A
PERF-TO P 1/4
08 APR 11
PERFORMANCE
TAKEOFF PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
DISTANCES DEFINITIONS
APPROVED
Ident.: PERF-TO-00006992.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
B
PERF-TO P 2/4
08 APR 11
PERFORMANCE
TAKEOFF PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
TAKEOFF PERFORMANCE
APPROVED
Ident.: PERF-TO-00006904.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
C
PERF-TO P 3/4
08 APR 11
PERFORMANCE
TAKEOFF PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
TAKEOFF FLIGHT PATH
APPROVED
Ident.: PERF-TO-00006935.0001001 / 04 APR 11
Criteria: SA
GLG A319-112 FLEET
AFM
D
PERF-TO P 4/4
08 APR 11
PERFORMANCE
IN FLIGHT PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
IN-FLIGHT PERFORMANCE
APPROVED
Ident.: PERF-FLT-00006995.0006001 / 04 APR 11
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.
GLG A319-112 FLEET
AFM
A
PERF-FLT P 1/2
08 APR 11
PERFORMANCE
IN FLIGHT PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-FLT P 2/2
08 APR 11
PERFORMANCE
LANDING PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
APPROACH CLIMB AND LANDING CLIMB
APPROVED
Ident.: PERF-LDG-00006909.0001001 / 02 DEC 13
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
APPROVED
Ident.: PERF-LDG-00006996.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
PERF-LDG P 1/4
14 DEC 13
PERFORMANCE
LANDING PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
LANDING DISTANCE DEFINITIONS
APPROVED
Ident.: PERF-LDG-00006997.0001001 / 23 NOV 09
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
APPROVED
Ident.: PERF-LDG-00006910.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
C to D
PERF-LDG P 2/4
14 DEC 13
PERFORMANCE
LANDING PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
AUTOLAND LANDING DISTANCE INCREMENTS
APPROVED
Ident.: PERF-LDG-00006998.0007001 / 23 NOV 09
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:
WEIGHT
42 000 kg
(92 600 lb)
45 000 kg
(92 200 lb)
50 000 kg
(110 230 lb)
55 000 kg
(121 250 lb)
60 000 kg
(132 280 lb)
GLG A319-112 FLEET
AFM
CONF FULL
WIND
(kt)
0
5
10
15
20
25
30
0
5
10
15
20
25
30
0
5
10
15
20
25
30
0
5
10
15
20
25
30
0
5
10
15
20
25
30
E→
LANDING DISTANCE INCREMENT
0
0
0
0
0
0
12 m/40 ft
0
0
0
0
0
11 m/36 ft
30 m/99 ft
0
0
0
0
0
17 m/55 ft
34 m/112 ft
0
0
0
0
0
0
11 m/37 ft
0
0
0
0
0
0
0
Continued on the following page
PERF-LDG P 3/4
14 DEC 13
PERFORMANCE
LANDING PERFORMANCE
A319
AIRPLANE FLIGHT MANUAL
WEIGHT
65 000 kg
(143 300 lb)
CONF FULL
WIND
(kt)
0
5
10
15
20
25
30
Continued from the previous page
LANDING DISTANCE INCREMENT
0
0
0
0
0
0
0
Increase by 15 % on foreseen wet runway.
GLG A319-112 FLEET
AFM
←E
PERF-LDG P 4/4
14 DEC 13
PERFORMANCE
PERFORMANCE DATABASE
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: PERF-OCTO-00021844.0001001 / 11 AUG 17
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.
GLG A319-112 FLEET
AFM
A
PERF-OCTO P 1/4
12 DEC 17
PERFORMANCE
PERFORMANCE DATABASE
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE DATABASE
APPROVED
Ident.: PERF-OCTO-00006895.0028001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
B
PERF-OCTO P 2/4
12 DEC 17
PERFORMANCE
PERFORMANCE DATABASE
A319
AIRPLANE FLIGHT MANUAL
COMPLEMENTARY PERFORMANCE DATA FILE
APPROVED
1 Ident.: PERF-OCTO-00021722.0005001 / 07 NOV 17
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.
CP32FA01
Required version of
PEP/AFM_OCTO FM module
V34 or higher
CP32FA02
V34 or higher
Approved CPDF
Performance Data(1)
‐ Computerized performance
penalties in the case of ice
accretion
‐ Integration of ROW data
‐ Autoland
CP32FA03
V34 or higher
V35 or higher
‐ Introduction of wet snow and
dry snow contaminants
‐ Autoland
V34 or higher (V35 or higher for
‐ Tachometer inoperative item
neo)
for MMEL
(1)
Applicability
A320 Family (except neo)
A320 Family (except neo)
A321neo equipped with CFM
engines and Autoland
A320 Family without Sharklet
A321neo equipped with Pratt &
Whitney engines and Autoland
A320 Family equipped with
BSCU L4.10
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.
GLG A319-112 FLEET
AFM
C
PERF-OCTO P 3/4
12 DEC 17
PERFORMANCE
PERFORMANCE DATABASE
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-OCTO P 4/4
12 DEC 17
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
TAKEOFF THRUST
APPROVED
Ident.: PERF-ENG-00006989.0022001 / 23 NOV 09
Criteria: 319-112
CFM 56-5B6 - TAKEOFF M = .0
GLG A319-112 FLEET
AFM
A→
PERF-ENG P 1/6
25 JAN 11
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
CFM 56-5B6 - TAKEOFF M = .0
GLG A319-112 FLEET
AFM
←A
PERF-ENG P 2/6
25 JAN 11
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
MAXIMUM CONTINUOUS THRUST
APPROVED
Ident.: PERF-ENG-00007420.0015001 / 23 NOV 09
Criteria: (319-111 or 319-112)
CFM 56-5B5 / CFM 56-5B6 - MAXIMUM CONTINUOUS - VC = 230 kt
GLG A319-112 FLEET
AFM
B
PERF-ENG P 3/6
25 JAN 11
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
GO-AROUND THRUST
APPROVED
Ident.: PERF-ENG-00007455.0012001 / 23 NOV 09
Criteria: 319-112
CFM 56-5B6 - GO-AROUND M = .225
GLG A319-112 FLEET
AFM
C→
PERF-ENG P 4/6
25 JAN 11
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
CFM 56-5B6 - GO-AROUND M = .225
GLG A319-112 FLEET
AFM
←C
PERF-ENG P 5/6
25 JAN 11
PERFORMANCE
ENGINE MANAGEMENT
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-ENG P 6/6
25 JAN 11
PERFORMANCE
REDUCED THRUST TAKEOFF
A319
AIRPLANE FLIGHT MANUAL
REDUCED THRUST TAKEOFF
APPROVED
Ident.: PERF-FLEX-00006990.0008001 / 23 NOV 09
Criteria: (319-112 and (32619 or 33239))
CFM56-5B6
N1 CORRECTIONS FOR AIR BLEED
AIR CONDITIONING ON
ENG ANTI-ICE ON
FLEX TAKEOFF
N1
NO AIR BLEED
MACH .000
ENG AND WING ANTI-ICE ON
- 0.7
0.0
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 %
GLG A319-112 FLEET
AFM
A
PERF-FLEX P 1/2
25 JAN 11
PERFORMANCE
REDUCED THRUST TAKEOFF
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
PERF-FLEX P 2/2
25 JAN 11
APPENDICES AND
SUPPLEMENTS
Intentionally left blank
EASA AD No.: 2017-0257R1
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
Effective Date:
Type/Model designation(s):
A318, A319, A320 and A321 aeroplanes
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,
Page 1 of 7
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EASA AD No.: 2017-0257R1
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.
Page 2 of 7
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An agency of the European Union
EASA AD No.: 2017-0257R1
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.
Page 3 of 7
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EASA AD No.: 2017-0257R1
Appendix 1 – AFM Procedure
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EASA AD No.: 2017-0257R1
Appendix 1 – AFM Procedure (continued)
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EASA AD No.: 2017-0257R1
Appendix 1 – AFM Procedure (continued)
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EASA AD No.: 2017-0257R1
Appendix 1 – AFM Procedure (end)
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APPENDICES AND SUPPLEMENTS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
APP-PLP-TOC P 1/2
12 SEP 17
APPENDICES AND SUPPLEMENTS
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
APP-INTX-ABN ABNORMAL PROCEDURES
Continued from the previous page
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
GLG A319-112 FLEET
AFM
APP-PLP-TOC P 2/2
12 SEP 17
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Ident.: APP-NOI-00007036.0002001 / 23 NOV 09
Criteria: (321-111 or 321-112 or 321-131 or 321-231 or 321-232 or A318 or A319 or A320)
APPROVED
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.
GLG A319-112 FLEET
AFM
A
APP-NOI P 1/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
EXTERNAL NOISE
APPROVED
Ident.: APP-NOI-00006882.0045001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
B→
APP-NOI P 2/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
Flyover Noise Levels
GLG A319-112 FLEET
AFM
←B→
APP-NOI P 3/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
Lateral Noise Levels
GLG A319-112 FLEET
AFM
←B→
APP-NOI P 4/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
Approach Noise Levels
GLG A319-112 FLEET
AFM
←B
APP-NOI P 5/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
EXTERNAL NOISE
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-NOI P 6/6
25 JAN 11
APPENDICES AND SUPPLEMENTS
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Ident.: APP-TCAS-00007060.0005001 / 02 DEC 13
Criteria: ((SA and (150842 or 152353 or 153870 or 39146)) or (SA and 152830))
APPROVED
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
Criteria: (SA and (26877 or 27698 or 27740 or 27753 or 28738 or 28739 or 30163))
APPROVED
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
Note:
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.
Following a TCAS II "clear of conflict" advisory, the pilot should expeditiously return to the
applicable ATC clearance unless otherwise directed by ATC.
GLG A319-112 FLEET
AFM
A to B
APP-TCAS P 1/2
12 JAN 17
APPENDICES AND SUPPLEMENTS
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-TCAS P 2/2
12 JAN 17
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-INOP-00006946.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-INOP P 1/4
25 JAN 11
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
APPROVED
Ident.: APP-INOP-00007064.0002001 / 23 NOV 09
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
One pair of spoilers inoperative in the retracted
position
Affected Performance
‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
Note:
ATA 27
Two pairs (surfaces 1 and 2) of spoilers
inoperative in the retracted position
All ground spoilers control system inoperative
One or more engine de-icing valve in open
position
ATA 30
One brake inoperative
In case only spoilers 5 are inop.
on each wing, the effect on ASD,
decision speed and landing distance
is negligible.
‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
‐
‐
‐
‐
‐
‐
‐
‐
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
‐ Accelerate Stop Distance (ASD) and decision
speed
‐ Landing distance
ATA 32
Continued on the following page
GLG A319-112 FLEET
AFM
B→
APP-INOP P 2/4
25 JAN 11
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
A319
AIRPLANE FLIGHT MANUAL
ATA 70
Continued from the previous page
Affected Performance
Dispatch Case
Ground idle system inoperative
GLG A319-112 FLEET
AFM
‐ Accelerate Stop Distance (ASD)
‐ Landing distance
←B
APP-INOP P 3/4
25 JAN 11
APPENDICES AND SUPPLEMENTS
DISPATCH WITH INOPERATIVE ITEMS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-INOP P 4/4
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
GENERAL
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-LGDN-GEN-00007074.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-LGDN-GEN P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-GEN P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
LIMITATIONS
AIRPLANE FLIGHT MANUAL
LIMITATIONS
APPROVED
Ident.: APP-LGDN-LIM-00007075.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-LGDN-LIM P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-LIM P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
EMERGENCY PROCEDURES
AIRPLANE FLIGHT MANUAL
ENG DUAL FAILURE
APPROVED
Ident.: APP-LGDN-EMER-00007079.0006001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-LGDN-EMER P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-EMER P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
ABNORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
F/CTL FLIGHT CONTROLS FAILURE
APPROVED
Ident.: APP-LGDN-ABN-00007078.0001001 / 23 NOV 09
Criteria: SA
A flight control failure case normally leading to ALTN LAW will lead to DIRECT LAW.
GLG A319-112 FLEET
AFM
A
APP-LGDN-ABN P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
ABNORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-ABN P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
NORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
PREFLIGHT CHECK
APPROVED
Ident.: APP-LGDN-NORM-00007076.0001001 / 23 NOV 09
Criteria: SA
The L/G DOWN VMO/MMO switch located in the avionic bay on 188VU must be set on L/G DOWN
position.
GLG A319-112 FLEET
AFM
A
APP-LGDN-NORM P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-NORM P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
PERFORMANCE
AIRPLANE FLIGHT MANUAL
PERFORMANCE
APPROVED
Ident.: APP-LGDN-PERF-00007354.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-LGDN-PERF P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-PERF P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
APPENDICES AND SUPPLEMENTS
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
APPROVED
Ident.: APP-LGDN-APP-00009236.0001001 / 23 NOV 09
Criteria: SA
The combination with the following supplement is not allowed:
‐ Extended Operations ETOPS (if applicable)
GLG A319-112 FLEET
AFM
A
APP-LGDN-APP P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
FLIGHT WITH LANDING GEAR DOWN
A319
AIRPLANE FLIGHT MANUAL
APPENDICES AND SUPPLEMENTS
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-LGDN-APP P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
GENERAL
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-INTX-GEN-00007085.0007001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-INTX-GEN P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-INTX-GEN P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
LIMITATIONS
AIRPLANE FLIGHT MANUAL
LIMITATIONS
APPROVED
Ident.: APP-INTX-LIM-00009744.0006001 / 03 AUG 10
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".
GLG A319-112 FLEET
AFM
A
APP-INTX-LIM P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-INTX-LIM P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
ABNORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
ENG RELIGHT IN FLIGHT IN CASE OF SAC/DAC INTERMIX
APPROVED
Ident.: APP-INTX-ABN-00007089.0001001 / 02 DEC 13
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
GLG A319-112 FLEET
AFM
A
APP-INTX-ABN P 1/2
14 DEC 13
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
ABNORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
ENG RELIGHT IN FLIGHT IN CASE OF SAC-TI INTERMIX
APPROVED
Ident.: APP-INTX-ABN-00009652.0001001 / 23 NOV 09
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
GLG A319-112 FLEET
AFM
B
APP-INTX-ABN P 2/2
14 DEC 13
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
NORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
TAKEOFF PROCEDURE
APPROVED
Ident.: APP-INTX-NORM-00007088.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-INTX-NORM P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
ENGINE INTERMIX
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-INTX-NORM P 2/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
GENERAL
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-HAO-GEN-00007111.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-HAO-GEN P 1/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-HAO-GEN P 2/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
LIMITATIONS
AIRPLANE FLIGHT MANUAL
ENVIRONMENTAL ENVELOPE
APPROVED
Ident.: APP-HAO-LIM-00007112.0093001 / 11 AUG 17
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
GLG A319-112 FLEET
AFM
A
APP-HAO-LIM P 1/2
12 SEP 17
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-HAO-LIM P 2/2
12 SEP 17
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
NORMAL PROCEDURES
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
APPROVED
Ident.: APP-HAO-NORM-00007122.0006001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-HAO-NORM P 1/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-HAO-NORM P 2/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
PERFORMANCE
AIRPLANE FLIGHT MANUAL
PERFORMANCE
APPROVED
Ident.: APP-HAO-PERF-00007129.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
APP-HAO-PERF P 1/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
HIGH ALTITUDE AIRPORTS OPERATIONS
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-HAO-PERF P 2/2
22 SEP 15
APPENDICES AND SUPPLEMENTS
TAWS-GPWS
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-TAWS-00007228.0001001 / 14 JAN 15
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
APPROVED
Ident.: APP-TAWS-00007229.0001001 / 23 NOV 09
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
APPROVED
Ident.: APP-TAWS-00007231.0002001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C →
APP-TAWS P 1/2
16 MAR 15
APPENDICES AND SUPPLEMENTS
TAWS-GPWS
A319
AIRPLANE FLIGHT MANUAL
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.
GLG A319-112 FLEET
AFM
←C
APP-TAWS P 2/2
16 MAR 15
APPENDICES AND SUPPLEMENTS
NARROW RUNWAY
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-NRWY-00006985.0002001 / 23 NOV 09
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
APPROVED
Ident.: APP-NRWY-00006987.0001001 / 23 NOV 09
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
APPROVED
Ident.: APP-NRWY-00007014.0001001 / 03 AUG 17
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.
GLG A319-112 FLEET
AFM
A to C
APP-NRWY P 1/2
08 AUG 17
APPENDICES AND SUPPLEMENTS
NARROW RUNWAY
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
APPROVED
Ident.: APP-NRWY-00006986.0002001 / 23 NOV 09
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
ΔVMCG (kt)
30 m
+ 2.5
35 m
+ 1.5
40 m
+0
and linear interpolation in between.
GLG A319-112 FLEET
AFM
D
APP-NRWY P 2/2
08 AUG 17
APPENDICES AND SUPPLEMENTS
OPERATIONS ON WET GROOVED/PFC RUNWAYS
A319
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: APP-PFC-00007028.0001001 / 23 NOV 09
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
APPROVED
Ident.: APP-PFC-00007029.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to B
APP-PFC P 1/2
25 JAN 11
APPENDICES AND SUPPLEMENTS
OPERATIONS ON WET GROOVED/PFC RUNWAYS
A319
AIRPLANE FLIGHT MANUAL
Intentionally left blank
GLG A319-112 FLEET
AFM
APP-PFC P 2/2
25 JAN 11
MASTER CONFIGURATION
DEVIATION LIST
Intentionally left blank
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 1/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
MCDL-27-07 Rubber Seal under Slat
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 2/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
MCDL-28 FUEL
MCDL-28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 3/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
MCDL-33-05 Logo Light Lens (Cover) 3LY, 4LY
TABLE OF CONTENTS
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 4/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
MCDL-52-03 Access Door to Potable Water Filling and Drainage
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 5/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 6/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
MCDL-53-03 Root Fillet Fairing
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 7/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
MCDL-57-04 Inboard Flap Rubbing Strip
Continued from the previous page
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
GLG A319-112 FLEET
AFM
MCDL-PLP-TOC P 8/8
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
SUMMARY OF HIGHLIGHTS
AIRPLANE FLIGHT MANUAL
Localization
Title
Toc
Index
ID
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
MCDL-33-07
Landing Light Lens 7LB, 8LB
A
1
MCDL-52-05
Access Door To Air Conditioning
Ground Supply 191 CB
MCDL-52-21
Blue Hydraulic Access Door 197 FB
MCDL-57-01
Wing Tip Fence
MCDL-57-01
Wing Tip Fence
MCDL-57-02
Belly Fairing Sliding Panel
MCDL-57-06
Outer Flap Blade Seal
A
1
Addition of a note to allow item combination.
Removal of the high speed tape content as Operator must refer to
AMM task.
Addition of a note to allow item combination.
Removal of the high speed tape content as Operator must refer to
AMM task.
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
2
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
A
1
Addition of a note to allow item combination.
MCDL-27-01
Flap Track Fairing
MCDL-27-03
Slat Track Closing Plate
MCDL-27-08
Seal Between Inboard and Outboard
Flap
MCDL-27-16
Flap Track Moveable Fairing Pivot
Cover
MCDL-28-01
Refuel/Defuel Coupling Cap 101 QM
Or 41 QM
MCDL-28-02
Refuel Panel Door
MCDL-33-02
Taxi Light Lamp 8LR
GLG A319-112 FLEET
AFM
Reason
MCDL-PLP-SOH P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
SUMMARY OF HIGHLIGHTS
Intentionally left blank
GLG A319-112 FLEET
AFM
MCDL-PLP-SOH P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
INTRODUCTION
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: MCDL-GEN-INTR-00006202.0001001 / 02 OCT 17
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.
GLG A319-112 FLEET
AFM
A
MCDL-GEN-INTR P 1/2
10 OCT 17
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
AIRPLANE FLIGHT MANUAL
INTRODUCTION
Intentionally left blank
GLG A319-112 FLEET
AFM
MCDL-GEN-INTR P 2/2
10 OCT 17
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
LIMITATIONS
AIRPLANE FLIGHT MANUAL
LIMITATIONS
APPROVED
Ident.: MCDL-GEN-LIM-00006203.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
MCDL-GEN-LIM P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET
AFM
MCDL-GEN-LIM P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
PERFORMANCE
AIRPLANE FLIGHT MANUAL
PERFORMANCE DETERMINATION METHOD
APPROVED
Ident.: MCDL-GEN-PERF-00006204.0001001 / 23 NOV 09
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
APPROVED
Ident.: MCDL-GEN-PERF-00006205.0001001 / 23 NOV 09
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).
GLG A319-112 FLEET
AFM
A to B
MCDL-GEN-PERF P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
GENERAL
A319
PERFORMANCE
AIRPLANE FLIGHT MANUAL
PERFORMANCE PENALTIES CALCULATED WITH AFM_OCTO SOFTWARE
APPROVED
Ident.: MCDL-GEN-PERF-00006206.0001001 / 14 JAN 15
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.
GLG A319-112 FLEET
AFM
C
MCDL-GEN-PERF P 2/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
A319
RAM AIR INLET FLAP
AIRPLANE FLIGHT MANUAL
21-01
Ram Air Inlet Flap
Ident.: MCDL-21-01-00006207.0002001 / 23 NOV 09
Criteria: (SA and ((26363 and A319) or (26363 and A320) or (26363 and A321) or A318))
21-01
RAM AIR INLET FLAP
APPROVED
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-21-01 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
A319
RAM AIR INLET FLAP
AIRPLANE FLIGHT MANUAL
ILLUSTRATION RAM AIR INLET FLAP
FOR INFORMATION ONLY
Ident.: MCDL-21-01-00006213.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions: Refer to 21-01 Ram Air Inlet Flap
GLG A319-112 FLEET
AFM
B
MCDL-21-01 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
A319
AIRPLANE FLIGHT MANUAL
21-03
RAM AIR INLET LEADING EDGE
Ram Air Inlet Leading Edge
APPROVED
Ident.: MCDL-21-03-00006216.0001001 / 23 NOV 09
Criteria: SA
21-03
RAM AIR INLET LEADING EDGE
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-21-03 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
AIR CONDITIONING
A319
AIRPLANE FLIGHT MANUAL
RAM AIR INLET LEADING EDGE
ILLUSTRATION RAM AIR INLET LEADING EDGE
FOR INFORMATION ONLY
Ident.: MCDL-21-03-00006219.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 21-03 Ram Air Inlet Leading Edge
GLG A319-112 FLEET
AFM
B
MCDL-21-03 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
COMMUNICATION
A319
STATIC DISCHARGER
AIRPLANE FLIGHT MANUAL
23-01
Static Discharger
APPROVED
Ident.: MCDL-23-01-00006220.0001001 / 02 DEC 13
Criteria: SA
23-01
STATIC DISCHARGER
Quantity installed
–
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
GLG A319-112 FLEET
AFM
A
MCDL-23-01 P 1/2
09 JUL 14
MASTER CONFIGURATION DEVIATION LIST
COMMUNICATION
A319
STATIC DISCHARGER
AIRPLANE FLIGHT MANUAL
ILLUSTRATION STATIC DISCHARGER
FOR INFORMATION ONLY
Ident.: MCDL-23-01-00006221.0001001 / 12 JUN 14
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
GLG A319-112 FLEET
AFM
B
MCDL-23-01 P 2/2
09 JUL 14
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
FLAP TRACK FAIRING
AIRPLANE FLIGHT MANUAL
27-01
Flap Track Fairing
APPROVED
Ident.: MCDL-27-01-00006235.0001001 / 29 NOV 17
Criteria: (A319 or A320)
1
27-01
FLAP TRACK FAIRING
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-01 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
FLAP TRACK FAIRING
AIRPLANE FLIGHT MANUAL
ILLUSTRATION FLAP TRACK FAIRING
FOR INFORMATION ONLY
Ident.: MCDL-27-01-00006236.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-01 Flap Track Fairing
GLG A319-112 FLEET
AFM
B
MCDL-27-01 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-03
SLAT TRACK CLOSING PLATE
Slat Track Closing Plate
APPROVED
Ident.: MCDL-27-03-00006239.0001001 / 29 NOV 17
Criteria: SA
1
27-03
SLAT TRACK CLOSING PLATE
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-03 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
SLAT TRACK CLOSING PLATE
AIRPLANE FLIGHT MANUAL
ILLUSTRATION SLAT TRACK CLOSING PLATE
FOR INFORMATION ONLY
Ident.: MCDL-27-03-00006240.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions: Refer to 27-03 Slat Track Closing Plate
GLG A319-112 FLEET
AFM
B
MCDL-27-03 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-05
ACCESS PANEL FOR BEARINGS AT ELEVATOR
Access Panel for Bearings at Elevator
APPROVED
Ident.: MCDL-27-05-00006243.0001001 / 23 NOV 09
Criteria: SA
27-05
ACCESS PANEL FOR BEARINGS AT ELEVATOR
Quantity installed
8
Two may be missing.
Refer to MCDL-27-05 Illustration Access Panel for Bearings at Elevator
GLG A319-112 FLEET
AFM
A
MCDL-27-05 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
ACCESS PANEL FOR BEARINGS AT ELEVATOR
ILLUSTRATION ACCESS PANEL FOR BEARINGS AT ELEVATOR
FOR INFORMATION ONLY
Ident.: MCDL-27-05-00006244.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-05 Access Panel for Bearings at Elevator
GLG A319-112 FLEET
AFM
B
MCDL-27-05 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-06
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
Flap Track Fairing Rear Top Cover and Tail Cone
APPROVED
Ident.: MCDL-27-06-00006245.0001001 / 02 DEC 13
Criteria: SA
27-06
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
Quantity installed
–
(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
GLG A319-112 FLEET
AFM
A
MCDL-27-06 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
ILLUSTRATION FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
FOR INFORMATION ONLY
Ident.: MCDL-27-06-00006246.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-06 Flap Track Fairing Rear Top Cover and Tail Cone
GLG A319-112 FLEET
AFM
B
MCDL-27-06 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
RUBBER SEAL UNDER SLAT
AIRPLANE FLIGHT MANUAL
27-07
Rubber Seal under Slat
APPROVED
Ident.: MCDL-27-07-00006247.0001001 / 02 DEC 13
Criteria: SA
27-07
RUBBER SEAL UNDER SLAT
Quantity installed
–
(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
GLG A319-112 FLEET
AFM
A
MCDL-27-07 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
RUBBER SEAL UNDER SLAT
AIRPLANE FLIGHT MANUAL
ILLUSTRATION RUBBER SEAL UNDER SLAT
FOR INFORMATION ONLY
Ident.: MCDL-27-07-00006248.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-07 Rubber Seal under Slat
GLG A319-112 FLEET
AFM
B
MCDL-27-07 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-08
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
Seal Between Inboard and Outboard Flap
APPROVED
Ident.: MCDL-27-08-00006250.0001001 / 29 NOV 17
Criteria: (A319 or A320 or A321)
1
27-08
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-08 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
ILLUSTRATION SEAL BETWEEN INBOARD AND OUTBOARD FLAP
FOR INFORMATION ONLY
Ident.: MCDL-27-08-00006251.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-08 Seal Between Inboard and Outboard Flap
GLG A319-112 FLEET
AFM
B
MCDL-27-08 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-09
INBOARD AILERON EDGE TO WING SEAL
Inboard Aileron Edge to Wing Seal
APPROVED
Ident.: MCDL-27-09-00006252.0001001 / 23 NOV 09
Criteria: SA
27-09
INBOARD AILERON EDGE TO WING SEAL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-09 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
INBOARD AILERON EDGE TO WING SEAL
ILLUSTRATION INBOARD AILERON TO WING SEAL
FOR INFORMATION ONLY
Ident.: MCDL-27-09-00006253.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-09 Inboard Aileron Edge to Wing Seal
GLG A319-112 FLEET
AFM
B
MCDL-27-09 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-10
SLAT END SEAL AND WEATHER SEAL
Slat End Seal and Weather Seal
APPROVED
Ident.: MCDL-27-10-00006254.0001001 / 23 NOV 09
Criteria: SA
27-10
SLAT END SEAL AND WEATHER SEAL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-10 P 1/2
03 MAY 16
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
SLAT END SEAL AND WEATHER SEAL
ILLUSTRATION SLAT END SEAL AND WEATHER SEAL
FOR INFORMATION ONLY
Ident.: MCDL-27-10-00006255.0001001 / 24 NOV 15
Criteria: SA
For dispatch conditions:Refer to 27-10 Slat End Seal and Weather Seal
GLG A319-112 FLEET
AFM
B
MCDL-27-10 P 2/2
03 MAY 16
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
SLAT TRACK FILLER BLOCK
27-11
Slat Track Filler Block
APPROVED
Ident.: MCDL-27-11-00006256.0001001 / 23 NOV 09
Criteria: SA
27-11
SLAT TRACK FILLER BLOCK
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-11 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
SLAT TRACK FILLER BLOCK
AIRPLANE FLIGHT MANUAL
ILLUSTRATION SLAT TRACK FILLER BLOCK
FOR INFORMATION ONLY
Ident.: MCDL-27-11-00006257.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-11 Slat Track Filler Block
GLG A319-112 FLEET
AFM
B
MCDL-27-11 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-12
SLAT TRACK SEALING PACKER
Slat Track Sealing Packer
APPROVED
Ident.: MCDL-27-12-00006258.0001001 / 23 NOV 09
Criteria: SA
27-12
SLAT TRACK SEALING PACKER
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-12 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
SLAT TRACK SEALING PACKER
ILLUSTRATION SLAT TRACK SEALING PACKER
FOR INFORMATION ONLY
Ident.: MCDL-27-12-00006259.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-12 Slat Track Sealing Packer
GLG A319-112 FLEET
AFM
B
MCDL-27-12 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-13
INTER-FLAP CUSHION SEAL
Inter-flap Cushion Seal
APPROVED
Ident.: MCDL-27-13-00006249.0001001 / 23 NOV 09
Criteria: SA
27-13
INTER-FLAP CUSHION SEAL
Quantity installed
4
One cushion seal may be missing per wing.
Refer to MCDL-27-13 Illustration Inter-Flap Cushion Seal
GLG A319-112 FLEET
AFM
A
MCDL-27-13 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
INTER-FLAP CUSHION SEAL
AIRPLANE FLIGHT MANUAL
ILLUSTRATION INTER-FLAP CUSHION SEAL
FOR INFORMATION ONLY
Ident.: MCDL-27-13-00006260.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-13 Inter-flap Cushion Seal
GLG A319-112 FLEET
AFM
B
MCDL-27-13 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-14
FLAP TRACK MOVEABLE FAIRING SEAL
Flap Track Moveable Fairing Seal
APPROVED
Ident.: MCDL-27-14-00006261.0001001 / 02 DEC 13
Criteria: SA
27-14
FLAP TRACK MOVEABLE FAIRING SEAL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-14 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
FLAP TRACK MOVEABLE FAIRING SEAL
ILLUSTRATION MOVEABLE FLAP TRACK FAIRING SEAL
FOR INFORMATION ONLY
Ident.: MCDL-27-14-00006262.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-14 Flap Track Moveable Fairing Seal
GLG A319-112 FLEET
AFM
B
MCDL-27-14 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-15
FLAP TRACK FIXED FAIRING SEAL
Flap Track Fixed Fairing seal
APPROVED
Ident.: MCDL-27-15-00006263.0001001 / 02 DEC 13
Criteria: (A318 or A319 or A320)
27-15
FLAP TRACK FIXED FAIRING SEAL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-15 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
FLAP TRACK FIXED FAIRING SEAL
ILLUSTRATION FIXED FLAP TRACK FAIRING SEAL
FOR INFORMATION ONLY
Ident.: MCDL-27-15-00006264.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 27-15 Flap Track Fixed Fairing Seal
GLG A319-112 FLEET
AFM
B
MCDL-27-15 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
27-16
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
Flap Track Moveable Fairing Pivot Cover
APPROVED
Ident.: MCDL-27-16-00006265.0001001 / 29 NOV 17
Criteria: SA
1
27-16
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-27-16 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FLIGHT CONTROL
A319
AIRPLANE FLIGHT MANUAL
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
ILLUSTRATION FLAP TRACK MOVEABLE FAIRING PIVOT COVER
FOR INFORMATION ONLY
Ident.: MCDL-27-16-00006266.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 27-16 Flap Track Moveable Fairing Pivot Cover
GLG A319-112 FLEET
AFM
B
MCDL-27-16 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FUEL
A319
AIRPLANE FLIGHT MANUAL
28-01
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
Refuel/Defuel Coupling Cap 101 QM Or 41 QM
APPROVED
Ident.: MCDL-28-01-00006282.0001001 / 29 NOV 17
Criteria: SA
1
28-01
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
Quantity installed
–
(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
GLG A319-112 FLEET
AFM
A
MCDL-28-01 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FUEL
A319
AIRPLANE FLIGHT MANUAL
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
ILLUSTRATION REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
FOR INFORMATION ONLY
Ident.: MCDL-28-01-00006283.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 28-01 Refuel/Defuel Coupling Cap 101 QM Or 41 QM
GLG A319-112 FLEET
AFM
B
MCDL-28-01 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FUEL
A319
AIRPLANE FLIGHT MANUAL
REFUEL PANEL DOOR 192MB
28-02
Refuel Panel Door
APPROVED
Ident.: MCDL-28-02-00006285.0001001 / 29 NOV 17
Criteria: SA
1
28-02
REFUEL PANEL DOOR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-28-02 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
FUEL
A319
REFUEL PANEL DOOR 192MB
AIRPLANE FLIGHT MANUAL
ILLUSTRATION REFUEL PANEL DOOR 192MB
FOR INFORMATION ONLY
Ident.: MCDL-28-02-00006286.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 28-02 Refuel Panel Door 192MB
GLG A319-112 FLEET
AFM
B
MCDL-28-02 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
ICE AND RAIN PROTECTION
A319
ICING INDICATOR
AIRPLANE FLIGHT MANUAL
30-01
Icing Indicator
APPROVED
Ident.: MCDL-30-01-00006287.0001001 / 23 NOV 09
Criteria: SA
30-01
ICING INDICATOR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-30-01 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
ICE AND RAIN PROTECTION
A319
ICING INDICATOR
AIRPLANE FLIGHT MANUAL
ILLUSTRATION ICING INDICATOR
FOR INFORMATION ONLY
Ident.: MCDL-30-01-00006288.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 30-01 Icing Indicator
GLG A319-112 FLEET
AFM
B
MCDL-30-01 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
A319
NOSE WHEEL HUBCAP
AIRPLANE FLIGHT MANUAL
32-03
Nose Wheel Hubcap
APPROVED
Ident.: MCDL-32-03-00006297.0001001 / 02 DEC 13
Criteria: SA
32-03
NOSE WHEEL HUBCAP
Quantity installed
2
(m) Refer to AMM Task 32-41-00-040-001
One may be missing.
Refer to MCDL-32-03 Illustration Nose Wheel Hubcap
GLG A319-112 FLEET
AFM
A
MCDL-32-03 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
A319
NOSE WHEEL HUBCAP
AIRPLANE FLIGHT MANUAL
ILLUSTRATION NOSE WHEEL HUBCAP
FOR INFORMATION ONLY
Ident.: MCDL-32-03-00006298.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 32-03 Nose Wheel Hubcap
GLG A319-112 FLEET
AFM
B
MCDL-32-03 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
A319
NOSE FITTING TOWING
AIRPLANE FLIGHT MANUAL
32-04
Nose Fitting Towing
APPROVED
Ident.: MCDL-32-04-00006299.0001001 / 02 DEC 13
Criteria: SA
32-04
NOSE FITTING TOWING
Quantity installed
1
(m) Refer to AMM Task 32-21-00-040-001
May be missing.
Refer to MCDL-32-04 Illustration Nose Fitting Towing
GLG A319-112 FLEET
AFM
A
MCDL-32-04 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LANDING GEAR
A319
NOSE FITTING TOWING
AIRPLANE FLIGHT MANUAL
ILLUSTRATION NOSE FITTING TOWING
FOR INFORMATION ONLY
Ident.: MCDL-32-04-00006300.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 32-04 Nose Fitting Towing
GLG A319-112 FLEET
AFM
B
MCDL-32-04 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
33-01
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
Wing/Engine Scan Light Cover 3LX, 4LX
APPROVED
Ident.: MCDL-33-01-00006301.0001001 / 02 DEC 13
Criteria: SA
33-01
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-01 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
ILLUSTRATION WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
FOR INFORMATION ONLY
Ident.: MCDL-33-01-00006302.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-01 Wing/Engine Scan light Cover 3LX, 4LX
GLG A319-112 FLEET
AFM
B
MCDL-33-01 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
TAXI LIGHT LAMP 8LR
AIRPLANE FLIGHT MANUAL
33-02
Taxi Light Lamp 8LR
APPROVED
Ident.: MCDL-33-02-00006303.0001001 / 29 NOV 17
Criteria: SA
1
33-02
TAXI LIGHT LAMP 8LR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-02 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
TAXI LIGHT LAMP 8LR
AIRPLANE FLIGHT MANUAL
ILLUSTRATION TAXI LIGHT LAMP 8LR
FOR INFORMATION ONLY
Ident.: MCDL-33-02-00006304.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-02 Taxi Light Lamp 8LR
GLG A319-112 FLEET
AFM
B
MCDL-33-02 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
REAR NAVIGATION LIGHT LENS 15LA
AIRPLANE FLIGHT MANUAL
33-03
Rear Navigation Light Lens 15LA
APPROVED
Ident.: MCDL-33-03-00006305.0001001 / 02 DEC 13
Criteria: SA
33-03
REAR NAVIGATION LIGHT LENS 15LA
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-03 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
REAR NAVIGATION LIGHT LENS 15LA
ILLUSTRATION REAR NAVIGATION LIGHT LENS 15LA
FOR INFORMATION ONLY
Ident.: MCDL-33-03-00006306.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-03 Rear Navigation Light Lens 15LA
GLG A319-112 FLEET
AFM
B
MCDL-33-03 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
33-04
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON) LIGHT COVER
Upper 7LV and Lower 6LV Anti-collision (Beacon) Light Cover
APPROVED
Ident.: MCDL-33-04-00006307.0001001 / 02 DEC 13
Criteria: SA
33-04
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON)
LIGHT COVER
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-04 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
UPPER 7LV AND LOWER 6LV ANTI-COLLISION (BEACON) LIGHT COVER
ILLUSTRATION UPPER AND LOWER ANTI-COLLISION ( BEACON) LIGHT COVER
FOR INFORMATION ONLY
Ident.: MCDL-33-04-00006308.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-04 Upper 7LV and Lower 6LV Anti-Collision (Beacon) Light
Cover
GLG A319-112 FLEET
AFM
B
MCDL-33-04 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
LOGO LIGHT LENS (COVER) 3LY, 4LY
AIRPLANE FLIGHT MANUAL
33-05
Logo Light Lens (Cover) 3LY, 4LY
APPROVED
Ident.: MCDL-33-05-00006309.0001001 / 02 DEC 13
Criteria: SA
33-05
LOGO LIGHT LENS (COVER) 3LY, 4LY
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-05 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
LOGO LIGHT LENS (COVER) 3LY, 4LY
ILLUSTRATION LOGO LIGHT LENS (COVER) 3LY, 4LY
FOR INFORMATION ONLY
Ident.: MCDL-33-05-00006310.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-05 Logo Light Lens (Cover) 3LY, 4LY
GLG A319-112 FLEET
AFM
B
MCDL-33-05 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
33-07
LANDING LIGHT LENS 7LB, 8LB
Landing Light Lens 7LB, 8LB
APPROVED
Ident.: MCDL-33-07-00006321.0001001 / 29 NOV 17
Criteria: SA
1
33-07
LANDING LIGHT LENS 7LB, 8LB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-07 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
LANDING LIGHT LENS 7LB, 8LB
ILLUSTRATION LANDING LIGHT LENS 7LB, 8LB
FOR INFORMATION ONLY
Ident.: MCDL-33-07-00006322.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-07 Landing Light Lens 7LB, 8LB
GLG A319-112 FLEET
AFM
B
MCDL-33-07 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
33-08
TURN OFF LIGHT LAMP 3LC1, 3LC2
Turn OFF Light Lamp 3LC1, 3LC2
APPROVED
Ident.: MCDL-33-08-00006324.0001001 / 02 DEC 13
Criteria: SA
33-08
TURN OFF LIGHT LAMP 3LC1, 3LC2
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-08 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
AIRPLANE FLIGHT MANUAL
TURN OFF LIGHT LAMP 3LC1, 3LC2
ILLUSTRATION TURN OFF LIGHT LAMP 3LC1, 3LC2
FOR INFORMATION ONLY
Ident.: MCDL-33-08-00006325.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-08 Turn OFF Light Lamp 3LC1, 3LC2
GLG A319-112 FLEET
AFM
B
MCDL-33-08 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
TAKEOFF LIGHT LAMP 7LR
AIRPLANE FLIGHT MANUAL
33-09
Takeoff light lamp 7LR
APPROVED
Ident.: MCDL-33-09-00006327.0001001 / 02 DEC 13
Criteria: SA
33-09
TAKEOFF LIGHT LAMP 7LR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-33-09 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
LIGHTS
A319
TAKEOFF LIGHT LAMP 7LR
AIRPLANE FLIGHT MANUAL
ILLUSTRATION TAKEOFF LIGHT LAMP 7LR
FOR INFORMATION ONLY
Ident.: MCDL-33-09-00006328.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 33-09 Takeoff Light Lamp 7LR
GLG A319-112 FLEET
AFM
B
MCDL-33-09 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
APU
A319
AIRPLANE FLIGHT MANUAL
49-01
APU OVERPRESSURE RELEASE DOOR
APU Overpressure Release Door
APPROVED
Ident.: MCDL-49-01-00006329.0001001 / 23 NOV 09
Criteria: SA
49-01
APU OVERPRESSURE RELEASE DOOR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-49-01 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
APU
A319
AIRPLANE FLIGHT MANUAL
APU OVERPRESSURE RELEASE DOOR
ILLUSTRATION APU OVERPRESSURE RELEASE DOOR
FOR INFORMATION ONLY
Ident.: MCDL-49-01-00006330.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 49-01 APU Overpressure Release Door
GLG A319-112 FLEET
AFM
B
MCDL-49-01 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
A319
AIRPLANE FLIGHT MANUAL
51-02
PASSENGER DOOR SCUFF PLATE
Passenger Door Scuff Plate
APPROVED
Ident.: MCDL-51-02-00006333.0001001 / 23 NOV 09
Criteria: SA
51-02
PASSENGER DOOR SCUFF PLATE
Quantity installed
–
All may be missing.
Refer to MCDL-51-02 Illustration Passenger Door Scuff Plate
GLG A319-112 FLEET
AFM
A
MCDL-51-02 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
A319
AIRPLANE FLIGHT MANUAL
PASSENGER DOOR SCUFF PLATE
ILLUSTRATION PASSENGER DOOR SCUFF PLATE
FOR INFORMATION ONLY
Ident.: MCDL-51-02-00006334.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 51-02 Passenger Door Scuff Plate
GLG A319-112 FLEET
AFM
B
MCDL-51-02 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
A319
AIRPLANE FLIGHT MANUAL
51-04
FAIRING AFT SAFETY STAY POINT 311 AL
Fairing Aft Safety Stay Point 311 AL
APPROVED
Ident.: MCDL-51-04-00006338.0001001 / 23 NOV 09
Criteria: SA
51-04
FAIRING AFT SAFETY STAY POINT 311 AL
Quantity installed
1
May be missing.
Refer to MCDL-51-04 Illustration Fairing Aft Safety Stay Point 311AL
GLG A319-112 FLEET
AFM
A
MCDL-51-04 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
STRUCTURE
A319
AIRPLANE FLIGHT MANUAL
FAIRING AFT SAFETY STAY POINT 311 AL
ILLUSTRATION FAIRING AFT SAFETY STAY POINT 311AL
FOR INFORMATION ONLY
Ident.: MCDL-51-04-00006339.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 51-04 Fairing Aft Safety Stay Point 311 AL
GLG A319-112 FLEET
AFM
B
MCDL-51-04 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-01
TOILET SERVICING AND DRAINAGE DOOR
Toilet Servicing and Drainage Door 172 AR
APPROVED
Ident.: MCDL-52-01-00006441.0003001 / 23 JAN 17
Criteria: ((A319 or A320 or A321) and 20109)
52-01
TOILET SERVICING AND DRAINAGE DOOR 172 AR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-01 P 1/2
07 FEB 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
TOILET SERVICING AND DRAINAGE DOOR
ILLUSTRATION TOILET SERVICING AND DRAINAGE DOOR
FOR INFORMATION ONLY
Ident.: MCDL-52-01-00006442.0002001 / 23 NOV 09
Criteria: (SA and 20109)
for dispatch conditions:Refer to 52-01 Toilet Servicing and Drainage Door
GLG A319-112 FLEET
AFM
B
MCDL-52-01 P 2/2
07 FEB 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: MCDL-52-02-00006447.0001001 / 16 JUN 17
Criteria: (A319 or A320 or A321)
52-02
ACCESS DOOR TO HYDRAULIC GROUND CONNECTORS
197 CB - 197 EB - 198 CB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-02 P 1/2
11 JUL 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO HYDRAULIC GROUND
CONNECTORS 197 CB - 197 EB - 198 CB
ILLUSTRATION ACCESS DOOR TO HYDRAULIC
GROUND CONNECTORS 197 CB - 197 EB - 198 CB
FOR INFORMATION ONLY
Ident.: MCDL-52-02-00006449.0001001 / 24 NOV 15
Criteria: SA
For dispatch conditions:Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197
EB - 198 CB
GLG A319-112 FLEET
AFM
B
MCDL-52-02 P 2/2
11 JUL 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-03
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Access Door To Potable Water Filling And Drainage 133 AL - 171 AL
APPROVED
Ident.: TDU / MCDL-52-03-00016655.0001001 / 06 JUL 15
Criteria: (A319 or A321)
Impacted DU: 00006452 Access Door to Potable Water Filling and Drainage
Belongs to TR564 Issue 1
52-03
ACCESS DOOR TO POTABLE WATER FILLING AND
DRAINAGE 133 AL - 171 AL
Quantity installed
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
Criteria: (A319 or A320 or A321)
Impacted by TDU: 00016655 Access Door to Potable Water Filling and Drainage
52-03
ACCESS DOOR TO POTABLE WATER FILLING AND
DRAINAGE 133 AL - 171 AL - 192 NB
APPROVED
Quantity installed
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
GLG A319-112 FLEET
AFM
A to B →
MCDL-52-03 P 1/4
30 JUL 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
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
Criteria: (A319 or A321)
Impacted DU: 00006453 Illustration Access Door to Potable Water Filling and Drainage
Belongs to TR564 Issue 1
APPROVED
For dispatch conditions: Refer to 52-03 Access Door to Potable Water Filling and Drainage.
GLG A319-112 FLEET
AFM
← B to C
MCDL-52-03 P 2/4
30 JUL 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
ILLUSTRATION ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Ident.: MCDL-52-03-00006453.0001001 / 23 NOV 09
Criteria: (A319 or A320 or A321)
Impacted by TDU: 00016656 Illustration Access Door to Potable Water Filling and Drainage
FOR INFORMATION ONLY
For dispatch conditions:Refer to 52-03 Access Door to Potable Water Filling and Drainage
GLG A319-112 FLEET
AFM
D
MCDL-52-03 P 3/4
30 JUL 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE
Intentionally left blank
GLG A319-112 FLEET
AFM
MCDL-52-03 P 4/4
30 JUL 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
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
APPROVED
Ident.: MCDL-52-04-00006455.0001001 / 14 JAN 15
Criteria: (A319 or A320 or A321)
52-04
ACCESS DOOR TO OPENING CONTROL OF LANDING
GEAR DOORS ON GROUND 195 BB - 196 BB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-04 P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO OPENING CONTROL OF LANDING
GEAR DOORS ON GROUND 195 BB - 196 BB
ILLUSTRATION ACCESS DOOR TO OPENING CONTROL
OF LANDING GEAR DOORS ON GROUND 195 BB - 196 BB
FOR INFORMATION ONLY
Ident.: MCDL-52-04-00006456.0001001 / 03 AUG 10
Criteria: SA
For dispatch conditions:Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on
Ground 195 BB - 196 BB
GLG A319-112 FLEET
AFM
B
MCDL-52-04 P 2/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-05
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB
Access Door To Air Conditioning Ground Supply 191 CB
APPROVED
Ident.: MCDL-52-05-00006457.0001001 / 29 NOV 17
Criteria: SA
1
52-05
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY
191 CB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-05 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB
ILLUSTRATION ACCESS DOOR TO AIR CONDITIONNING GROUND SUPPLY 191 CB
FOR INFORMATION ONLY
Ident.: MCDL-52-05-00006458.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB
GLG A319-112 FLEET
AFM
B
MCDL-52-05 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
EXTERNAL POWER GROUND
CONNECTION ACCESS DOOR ASSY 121 AL
AIRPLANE FLIGHT MANUAL
52-07
External Power Ground Connection Access Door Assy 121 AL
APPROVED
Ident.: MCDL-52-07-00006461.0001001 / 02 OCT 17
Criteria: SA
52-07
EXTERNAL POWER GROUND CONNECTION ACCESS
DOOR ASSY 121 AL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-07 P 1/2
10 OCT 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
EXTERNAL POWER GROUND
CONNECTION ACCESS DOOR ASSY 121 AL
ILLUSTRATION EXTERNAL POWER GROUND CONNECTION ACCESS DOOR ASSY 121 AL
FOR INFORMATION ONLY
Ident.: MCDL-52-07-00006462.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-07 External Power Ground Connection Access Door Assy 121
AL
GLG A319-112 FLEET
AFM
B
MCDL-52-07 P 2/2
10 OCT 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-08
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
Access Door Of Cargo Opening System 134 AR - 154 AR
APPROVED
Ident.: MCDL-52-08-00006463.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
52-08
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154
AR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-08 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
ILLUSTRATION ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR - 154 AR
FOR INFORMATION ONLY
Ident.: MCDL-52-08-00006464.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-08 Access Door of Cargo Opening System 134 AR - 154 AR
GLG A319-112 FLEET
AFM
B
MCDL-52-08 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-09
NOSE LANDING GEAR MAIN DOOR (713, 714)
Nose Landing Gear Main Door (713, 714)
APPROVED
Ident.: MCDL-52-09-00006465.0001001 / 02 DEC 13
Criteria: (A319 or A320)
52-09
NOSE LANDING GEAR MAIN DOOR (713, 714)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-09 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
NOSE LANDING GEAR MAIN DOOR (713, 714)
ILLUSTRATION NOSE LANDING GEAR MAIN DOOR (713, 714)
FOR INFORMATION ONLY
Ident.: MCDL-52-09-00006466.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-09 Nose Landing Gear Main Door (713, 714)
GLG A319-112 FLEET
AFM
B
MCDL-52-09 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-10
NOSE LANDING GEAR AFT DOOR (715, 716)
Nose Landing Gear Aft Door (715, 716)
APPROVED
Ident.: MCDL-52-10-00006467.0001001 / 02 DEC 13
Criteria: SA
52-10
NOSE LANDING GEAR AFT DOOR (715, 716)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-10 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
NOSE LANDING GEAR AFT DOOR (715, 716)
ILLUSTRATION NOSE LANDING GEAR AFT DOOR (715, 716)
FOR INFORMATION ONLY
Ident.: MCDL-52-10-00006468.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-10 Nose Landing Gear Aft Door (715, 716)
GLG A319-112 FLEET
AFM
B
MCDL-52-10 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-11
NOSE LANDING GEAR LEG DOOR (712)
Nose Landing Gear Leg Door (712)
APPROVED
Ident.: MCDL-52-11-00006471.0001001 / 02 DEC 13
Criteria: SA
52-11
NOSE LANDING GEAR LEG DOOR (712)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-11 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
NOSE LANDING GEAR LEG DOOR (712)
ILLUSTRATION NOSE LANDING GEAR LEG DOOR (712)
FOR INFORMATION ONLY
Ident.: MCDL-52-11-00006472.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-11 Nose Landing Gear Leg Door (712)
GLG A319-112 FLEET
AFM
B
MCDL-52-11 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-12
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP)
Main Landing Gear Door (732, 742) (flight with gear up)
APPROVED
Ident.: MCDL-52-12-00006473.0001001 / 02 DEC 13
Criteria: (A318 or A319 or A320)
52-12
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH
GEAR UP)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-12 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP)
ILLUSTRATION MAIN LANDING GEAR DOOR (732, 742)
FOR INFORMATION ONLY
Ident.: MCDL-52-12-00006474.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-12 Main Landing Gear Door (732, 742) (flight with gear up)
GLG A319-112 FLEET
AFM
B
MCDL-52-12 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-13
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP)
Main Landing Gear Door (733, 743) (flight with gear up)
APPROVED
Ident.: MCDL-52-13-00006487.0001001 / 02 DEC 13
Criteria: (A319 or A320 or A321)
52-13
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH
GEAR UP)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-13 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP)
ILLUSTRATION MAIN LANDING GEAR DOOR (733, 743)
FOR INFORMATION ONLY
Ident.: MCDL-52-13-00006488.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-13 Main Landing Gear Door (733, 743) (flight with gear up)
GLG A319-112 FLEET
AFM
B
MCDL-52-13 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-14
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN)
Main Landing Gear Door (732, 742) (Flight with gear down)
APPROVED
Ident.: MCDL-52-14-00006475.0001001 / 02 DEC 13
Criteria: (A318 or A319 or A320)
52-14
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH
GEAR DOWN)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-14 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN)
ILLUSTRATION MAIN LANDING GEAR DOOR (732, 742)
FOR INFORMATION ONLY
Ident.: MCDL-52-14-00006476.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-14 Main Landing Gear Door (732, 742) (flight with gear down)
GLG A319-112 FLEET
AFM
B
MCDL-52-14 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-15
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN)
Main Landing Gear Door (733, 743) (Flight with gear down)
APPROVED
Ident.: MCDL-52-15-00006489.0001001 / 02 DEC 13
Criteria: (A319 or A320 or A321)
52-15
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH
GEAR DOWN)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-15 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN)
ILLUSTRATION MAIN LANDING GEAR DOOR (733, 743)
FOR INFORMATION ONLY
Ident.: MCDL-52-15-00006490.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-15 Main Landing Gear Door (733, 743) (Flight with gear down)
GLG A319-112 FLEET
AFM
B
MCDL-52-15 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-16
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN)
Main Landing Gear Door (734, 744) (Flight with gear down)
APPROVED
Ident.: MCDL-52-16-00006491.0001001 / 02 DEC 13
Criteria: (A318 or A319 or A320)
52-16
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH
GEAR DOWN)
Quantity installed
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)
GLG A319-112 FLEET
AFM
A
MCDL-52-16 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN)
ILLUSTRATION MAIN LANDING GEAR DOOR (734, 744)
FOR INFORMATION ONLY
Ident.: MCDL-52-16-00006492.0001001 / 23 NOV 09
Criteria: SA
for dispatch conditions:Refer to 52-16 Main Landing Gear Door (734, 744) (Flight with gear down)
GLG A319-112 FLEET
AFM
B
MCDL-52-16 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-18
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
Main Landing Gear Door : Seal On Secondary Hinged Fairing
APPROVED
Ident.: MCDL-52-18-00006479.0001001 / 23 NOV 09
Criteria: SA
52-18
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY
HINGED FAIRING
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-18 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
ILLUSTRATION MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
FOR INFORMATION ONLY
Ident.: MCDL-52-18-00006480.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-18 Main Landing Gear Door : Seal on Secondary Hinged Fairing
GLG A319-112 FLEET
AFM
B
MCDL-52-18 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-19
PAX DOOR UPPER COVER PLATE
Pax Door Upper Cover Plate
APPROVED
Ident.: MCDL-52-19-00006481.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
52-19
PAX DOOR UPPER COVER PLATE
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-19 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
PAX DOOR UPPER COVER PLATE
ILLUSTRATION PAX DOOR UPPER COVER PLATE
FOR INFORMATION ONLY
Ident.: MCDL-52-19-00006482.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-19 Pax Door Upper Cover Plate
GLG A319-112 FLEET
AFM
B
MCDL-52-19 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-20
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
Access Door To HP Air Ground Connector 191 DB
APPROVED
Ident.: MCDL-52-20-00006483.0001001 / 14 JAN 15
Criteria: SA
52-20
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-20 P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
ILLUSTRATION ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
FOR INFORMATION ONLY
Ident.: MCDL-52-20-00006484.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-20 Access Door to HP Air Ground Connector 191 DB
GLG A319-112 FLEET
AFM
B
MCDL-52-20 P 2/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-21
BLUE HYDRAULIC ACCESS DOOR 197 FB
Blue Hydraulic Access Door 197 FB
APPROVED
Ident.: MCDL-52-21-00007449.0001001 / 29 NOV 17
Criteria: SA
1
52-21
BLUE HYDRAULIC ACCESS DOOR 197 FB
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-21 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
BLUE HYDRAULIC ACCESS DOOR 197 FB
ILLUSTRATION BLUE HYDRAULIC ACCESS DOOR 197 FB
FOR INFORMATION ONLY
Ident.: MCDL-52-21-00007450.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-21 Blue Hydraulic Access Door 197 FB
GLG A319-112 FLEET
AFM
B
MCDL-52-21 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-22
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
Forward Cargo Door Access Cover Panel 825 AR
APPROVED
Ident.: MCDL-52-22-00007451.0001001 / 02 DEC 13
Criteria: SA
52-22
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-22 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
ILLUSTRATION FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
FOR INFORMATION ONLY
Ident.: MCDL-52-22-00007452.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 52-22 Forward Cargo Door Access Cover Panel 825 AR
GLG A319-112 FLEET
AFM
B
MCDL-52-22 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
52-23
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
Aft Cargo Door Access Cover Panel 826 AR
APPROVED
Ident.: MCDL-52-23-00007453.0001001 / 02 DEC 13
Criteria: SA
52-23
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-52-23 P 1/2
01 SEP 16
MASTER CONFIGURATION DEVIATION LIST
DOORS
A319
AIRPLANE FLIGHT MANUAL
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
ILLUSTRATION AFT CARGO DOOR ACCESS COVER PANEL 826 AR
FOR INFORMATION ONLY
Ident.: MCDL-52-23-00007454.0002001 / 17 AUG 16
Criteria: A319
For dispatch conditions: Refer to 52-23 Aft Cargo Door Access Cover Panel 826 AR
GLG A319-112 FLEET
AFM
B
MCDL-52-23 P 2/2
01 SEP 16
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
A319
AIRPLANE FLIGHT MANUAL
53-01
BELLY FAIRING VENT LOUVER VANE
Belly Fairing Vent Louver Vane
APPROVED
Ident.: MCDL-53-01-00006512.0001001 / 14 JAN 15
Criteria: SA
53-01
BELLY FAIRING VENT LOUVER VANE
Quantity installed
–
(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
GLG A319-112 FLEET
AFM
A
MCDL-53-01 P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
A319
AIRPLANE FLIGHT MANUAL
BELLY FAIRING VENT LOUVER VANE
ILLUSTRATION BELLY FAIRING VENT LOUVER VANE
FOR INFORMATION ONLY
Ident.: MCDL-53-01-00006513.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 53-01 Belly Fairing Vent Louver Vane
GLG A319-112 FLEET
AFM
B
MCDL-53-01 P 2/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
A319
ROOT FILLET FAIRING
AIRPLANE FLIGHT MANUAL
53-03
Root Fillet Fairing
APPROVED
Ident.: MCDL-53-03-00011063.0005001 / 02 DEC 13
Criteria: A319
53-03
ROOT FILLET FAIRING
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-53-03 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
FUSELAGE
A319
ROOT FILLET FAIRING
AIRPLANE FLIGHT MANUAL
ILLUSTRATION ROOT FILLET FAIRING
FOR INFORMATION ONLY
Ident.: MCDL-53-03-00011064.0001001 / 03 AUG 10
Criteria: SA
For dispatch conditions:Refer to 53-03 Root Fillet Fairing
GLG A319-112 FLEET
AFM
B
MCDL-53-03 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
NACELLE STRAKE
AIRPLANE FLIGHT MANUAL
54-01
Nacelle Strake
APPROVED
Ident.: MCDL-54-01-00006516.0005001 / 14 JAN 15
Criteria: A319
54-01
NACELLE STRAKE
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-54-01 P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
NACELLE STRAKE
AIRPLANE FLIGHT MANUAL
ILLUSTRATION NACELLE STRAKE
FOR INFORMATION ONLY
Ident.: MCDL-54-01-00006517.0002001 / 23 NOV 09
Criteria: (A318 or A319 or A321)
For dispatch conditions:Refer to 54-01 Nacelle Strake
GLG A319-112 FLEET
AFM
B
MCDL-54-01 P 2/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AIRPLANE FLIGHT MANUAL
54-03
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
Pylon Pressure Relief Door 413(423) BL - 414(424) BR
APPROVED
Ident.: MCDL-54-03-00006540.0003001 / 02 DEC 13
Criteria: A319
54-03
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424)
BR
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-54-03 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AIRPLANE FLIGHT MANUAL
PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
ILLUSTRATION PYLON PRESSURE RELIEF DOOR 413(423) BL - 414(424) BR
FOR INFORMATION ONLY
Ident.: MCDL-54-03-00006541.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 54-03 Pylon Pressure Relief Door 413(423) BL - 414(424) BR
GLG A319-112 FLEET
AFM
B
MCDL-54-03 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AIRPLANE FLIGHT MANUAL
54-04
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
Pylon Access Door 415(425) AL - 415(425) AR
APPROVED
Ident.: MCDL-54-04-00006543.0001001 / 23 NOV 09
Criteria: SA
54-04
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
Quantity installed
–
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
GLG A319-112 FLEET
AFM
A
MCDL-54-04 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AIRPLANE FLIGHT MANUAL
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
ILLUSTRATION PYLON ACCESS DOOR 415(425) AL - 415(425) AR
FOR INFORMATION ONLY
Ident.: MCDL-54-04-00006544.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 54-04 Pylon Access Door 415(425) AL - 415(425) AR
GLG A319-112 FLEET
AFM
B
MCDL-54-04 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
PYLON FAIRING SEAL
AIRPLANE FLIGHT MANUAL
54-05
Pylon Fairing Seal
APPROVED
Ident.: TDU / MCDL-54-05-00015527.0001001 / 29 OCT 14
Criteria: SA
Impacted DU: 00006545 Pylon Fairing Seal
Belongs to TR423 Issue 1
54-05
PYLON FAIRING SEAL
Quantity installed
6
One may be missing per pylon.
Refer to MCDL-54-05 Illustration Pylon Fairing Seal
54-05
Pylon Fairing seal
APPROVED
Ident.: MCDL-54-05-00006545.0001001 / 23 NOV 09
Criteria: SA
Impacted by TDU: 00015527 Pylon Fairing Seal
54-05
PYLON FAIRING SEAL
Quantity installed
4
One may be missing per pylon.
Refer to MCDL-54-05 Illustration Pylon Fairing Seal
GLG A319-112 FLEET
AFM
A to B
MCDL-54-05 P 1/4
19 NOV 14
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
PYLON FAIRING SEAL
AIRPLANE FLIGHT MANUAL
ILLUSTRATION PYLON FAIRING SEAL
APPROVED
Ident.: TDU / MCDL-54-05-00015528.0001001 / 29 OCT 14
Criteria: SA
Impacted DU: 00006546 Illustration Pylon Fairing Seal
Belongs to TR423 Issue 1
For dispatch conditions:Refer to 54-05 Pylon Fairing Seal
GLG A319-112 FLEET
AFM
C
MCDL-54-05 P 2/4
19 NOV 14
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
PYLON FAIRING SEAL
AIRPLANE FLIGHT MANUAL
ILLUSTRATION PYLON FAIRING SEAL
FOR INFORMATION ONLY
Ident.: MCDL-54-05-00006546.0001001 / 23 NOV 09
Criteria: SA
Impacted by TDU: 00015528 Illustration Pylon Fairing Seal
For dispatch conditions:Refer to 54-05 Pylon Fairing Seal
GLG A319-112 FLEET
AFM
D
MCDL-54-05 P 3/4
19 NOV 14
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AIRPLANE FLIGHT MANUAL
PYLON FAIRING SEAL
Intentionally left blank
GLG A319-112 FLEET
AFM
MCDL-54-05 P 4/4
19 NOV 14
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AERODYNAMIC SEAL
AIRPLANE FLIGHT MANUAL
54-06
Aerodynamic Seal
APPROVED
Ident.: MCDL-54-06-00006547.0001001 / 02 DEC 13
Criteria: SA
54-06
AERODYNAMIC SEAL
Quantity installed
2
(m) Refer to AMM Task 54-53-00-040-001
All may be missing.
Refer to MCDL-54-06 Illustration Aerodynamic Seal
GLG A319-112 FLEET
AFM
A
MCDL-54-06 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
NACELLE / PYLON
A319
AERODYNAMIC SEAL
AIRPLANE FLIGHT MANUAL
ILLUSTRATION AERODYNAMIC SEAL
FOR INFORMATION ONLY
Ident.: MCDL-54-06-00006548.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 54-06 Aerodynamic Seal
GLG A319-112 FLEET
AFM
B
MCDL-54-06 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
WING TIP FENCE
AIRPLANE FLIGHT MANUAL
57-01
Wing Tip Fence
APPROVED
Ident.: MCDL-57-01-00006549.0001001 / 29 NOV 17
Criteria: A319
1
a)
57-01
WING TIP FENCE
Quantity installed
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 –
2
b)
57-01
WING TIP FENCE
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-57-01 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
WING TIP FENCE
AIRPLANE FLIGHT MANUAL
ILLUSTRATION WING TIP FENCE
FOR INFORMATION ONLY
Ident.: MCDL-57-01-00006550.0001001 / 23 NOV 09
Criteria: SA
For dispatch conditions:Refer to 57-01 Wing Tip Fence
GLG A319-112 FLEET
AFM
B
MCDL-57-01 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
AIRPLANE FLIGHT MANUAL
57-02
BELLY FAIRING SLIDING PANEL
Belly Fairing Sliding Panel
APPROVED
Ident.: MCDL-57-02-00006551.0002001 / 29 NOV 17
Criteria: (SA and 26495)
1
57-02
BELLY FAIRING SLIDING PANEL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-57-02 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
AIRPLANE FLIGHT MANUAL
BELLY FAIRING SLIDING PANEL
ILLUSTRATION BELLY FAIRING SLIDING PANEL
FOR INFORMATION ONLY
Ident.: MCDL-57-02-00006552.0002001 / 23 NOV 09
Criteria: (SA and 26495)
For dispatch conditions:Refer to 57-02 Belly Fairing Sliding Panel
GLG A319-112 FLEET
AFM
B
MCDL-57-02 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
OUTBOARD FLAPS RUBBING STRIP
AIRPLANE FLIGHT MANUAL
57-03
Outboard Flap Rubbing Strip Items 10, 15, 20, 40
APPROVED
Ident.: MCDL-57-03-00006564.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
57-03
OUTBOARD FLAP RUBBING STRIP ITEMS 10, 15, 20, 40
Quantity installed
12
All may be missing.
Refer to MCDL-57-03 Illustration Outboard Flap Rubbing Strip
GLG A319-112 FLEET
AFM
A
MCDL-57-03 P 1/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
AIRPLANE FLIGHT MANUAL
OUTBOARD FLAPS RUBBING STRIP
ILLUSTRATION OUTBOARD FLAP RUBBING STRIP
FOR INFORMATION ONLY
Ident.: MCDL-57-03-00006565.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 57-03 Outboard Flap Rubbing Strip
GLG A319-112 FLEET
AFM
B
MCDL-57-03 P 2/2
25 JAN 11
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
AIRPLANE FLIGHT MANUAL
57-04
INBOARD FLAP RUBBING STRIP
Inboard Flap Rubbing Strip items 1, 5, 10, 30
APPROVED
Ident.: MCDL-57-04-00006567.0001001 / 23 NOV 09
Criteria: (A318 or A319 or A320)
57-04
INBOARD FLAP RUBBING STRIP ITEMS 1, 5, 10, 30
Quantity installed
8
All may be missing.
Refer to MCDL-57-04 Illustration Inboard Flap Rubbing Strip
GLG A319-112 FLEET
AFM
A
MCDL-57-04 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
AIRPLANE FLIGHT MANUAL
INBOARD FLAP RUBBING STRIP
ILLUSTRATION INBOARD FLAP RUBBING STRIP
FOR INFORMATION ONLY
Ident.: MCDL-57-04-00006568.0001001 / 02 DEC 13
Criteria: (A318 or A319 or A320)
For dispatch conditions:Refer to 57-04 Inboard Flap Rubbing Strip
GLG A319-112 FLEET
AFM
B
MCDL-57-04 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
OUTER FLAP BLADE SEAL
AIRPLANE FLIGHT MANUAL
57-06
Outer Flap Blade Seal
APPROVED
Ident.: MCDL-57-06-00021897.0001001 / 29 NOV 17
Criteria: (A318 or A319 or A320 or A321)
1
57-06
OUTER FLAP BLADE SEAL
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-57-06 P 1/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
WINGS
A319
OUTER FLAP BLADE SEAL
AIRPLANE FLIGHT MANUAL
ILLUSTRATION OUTER FLAP BLADE SEAL
FOR INFORMATION ONLY
Ident.: MCDL-57-06-00021942.0001001 / 07 SEP 17
Criteria: (A318 or A319 or A320)
Belongs to CP116 Issue 1
For dispatch conditions: Refer to 57-06 Outer Flap Blade Seal
GLG A319-112 FLEET
AFM
B
MCDL-57-06 P 2/2
12 DEC 17
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
A319
FRANGIBLE DRAIN MAST
AIRPLANE FLIGHT MANUAL
71-01
Frangible Drain Mast
APPROVED
Ident.: MCDL-71-01-00006569.0001001 / 02 DEC 13
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
FRANGIBLE DRAIN MAST
Quantity installed
2
(m) Refer to AMM Task 71-71-42-040-045
All may be missing.
Refer to MCDL-71-01 Illustration Frangible Drain Mast
GLG A319-112 FLEET
AFM
A
MCDL-71-01 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
A319
FRANGIBLE DRAIN MAST
AIRPLANE FLIGHT MANUAL
ILLUSTRATION FRANGIBLE DRAIN MAST
FOR INFORMATION ONLY
Ident.: MCDL-71-01-00006570.0001001 / 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)
For dispatch conditions:Refer to 71-01 Frangible Drain Mast
GLG A319-112 FLEET
AFM
B
MCDL-71-01 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
71-09
FAN COWL HOLD OPEN ROD
Fan Cowl Hold Open Rod
APPROVED
Ident.: MCDL-71-09-00006587.0002001 / 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)
71-09
FAN COWL HOLD OPEN ROD
Quantity installed
8
(m) Refer to AMM Task
All may be missing.
Refer to MCDL-71-09 Illustration Fan Cowl Hold Open Rod
GLG A319-112 FLEET
AFM
A
MCDL-71-09 P 1/2
01 DEC 16
MASTER CONFIGURATION DEVIATION LIST
POWER PLANT
A319
AIRPLANE FLIGHT MANUAL
FAN COWL HOLD OPEN ROD
ILLUSTRATION FAN COWL HOLD OPEN ROD
FOR INFORMATION ONLY
Ident.: MCDL-71-09-00006588.0003001 / 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)
For dispatch conditions:Refer to 71-09 Fan Cowl Hold Open Rod
GLG A319-112 FLEET
AFM
B
MCDL-71-09 P 2/2
01 DEC 16
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
78-01
DUCT OPENING ACTUATOR
Duct Opening Actuator
APPROVED
Ident.: TDU / MCDL-78-01-00016031.0001001 / 20 MAR 15
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
DUCT OPENING ACTUATOR
Quantity installed
4
(m) Refer to AMM Task
All may be missing.
Refer to MCDL-78-01 Illustration Duct Opening Actuator
GLG A319-112 FLEET
AFM
A
MCDL-78-01 P 1/2
14 APR 15
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
DUCT OPENING ACTUATOR
ILLUSTRATION DUCT OPENING ACTUATOR
APPROVED
Ident.: TDU / MCDL-78-01-00016033.0001001 / 20 MAR 15
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
GLG A319-112 FLEET
AFM
B
MCDL-78-01 P 2/2
14 APR 15
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
78-09
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
Thrust Reverser 11 and 1 O'clock Struts
APPROVED
Ident.: MCDL-78-09-00006596.0001001 / 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)
78-09
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-78-09 P 1/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
ILLUSTRATION THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
FOR INFORMATION ONLY
Ident.: MCDL-78-09-00006597.0001001 / 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)
For dispatch conditions:Refer to 78-09 Thrust Reverser 11 and 1 O'clock Struts
GLG A319-112 FLEET
AFM
B
MCDL-78-09 P 2/2
14 DEC 13
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
78-11
THRUST REVERSER LOCKOUT FAIRING
Thrust Reverser Lockout Fairing
APPROVED
Ident.: MCDL-78-11-00014886.0001001 / 14 JAN 15
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
THRUST REVERSER LOCKOUT FAIRING
Quantity installed
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
GLG A319-112 FLEET
AFM
A
MCDL-78-11 P 1/2
16 MAR 15
MASTER CONFIGURATION DEVIATION LIST
EXHAUST
A319
AIRPLANE FLIGHT MANUAL
THRUST REVERSER LOCKOUT FAIRING
ILLUSTRATION OF THE THRUST REVERSER LOCKOUT FAIRING
APPROVED
Ident.: MCDL-78-11-00014887.0001001 / 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 320-211 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)
GLG A319-112 FLEET
AFM
B
MCDL-78-11 P 2/2
16 MAR 15
SUPPLEMENTARY
PERFORMANCE
Intentionally left blank
SUPPLEMENTARY PERFORMANCE
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
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
GLG A319-112 FLEET
AFM
SPERF-PLP-TOC P 1/2
12 DEC 17
SUPPLEMENTARY PERFORMANCE
PRELIMINARY PAGES
A319
AIRPLANE FLIGHT MANUAL
TABLE OF CONTENTS
Intentionally left blank
GLG A319-112 FLEET
AFM
SPERF-PLP-TOC P 2/2
12 DEC 17
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
GENERAL
AIRPLANE FLIGHT MANUAL
GENERAL
APPROVED
Ident.: SPERF-CONT-GEN-00009415.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A
SPERF-CONT-GEN P 1/2
25 JAN 11
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
AIRPLANE FLIGHT MANUAL
GENERAL
Intentionally left blank
GLG A319-112 FLEET
AFM
SPERF-CONT-GEN P 2/2
25 JAN 11
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
LIMITATIONS
AIRPLANE FLIGHT MANUAL
LIMITATIONS
APPROVED
Ident.: SPERF-CONT-LIM-00009416.0001001 / 04 APR 11
Criteria: SA
Reduced thrust takeoff is not allowed on contaminated runways.
Takeoff on very low braking friction surface (icy runway) is not recommended.
GLG A319-112 FLEET
AFM
A
SPERF-CONT-LIM P 1/2
08 APR 11
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
AIRPLANE FLIGHT MANUAL
LIMITATIONS
Intentionally left blank
GLG A319-112 FLEET
AFM
SPERF-CONT-LIM P 2/2
08 APR 11
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
PERFORMANCE
AIRPLANE FLIGHT MANUAL
INTRODUCTION
APPROVED
Ident.: SPERF-CONT-PERF-00009417.0001001 / 23 NOV 09
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
APPROVED
Ident.: SPERF-CONT-PERF-00009441.0001001 / 07 NOV 17
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
APPROVED
Ident.: SPERF-CONT-PERF-00009429.0001001 / 23 NOV 09
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.
GLG A319-112 FLEET
AFM
A to C
SPERF-CONT-PERF P 1/2
12 DEC 17
SUPPLEMENTARY PERFORMANCE
CONTAMINATED RUNWAY
A319
AIRPLANE FLIGHT MANUAL
PERFORMANCE
Intentionally left blank
GLG A319-112 FLEET
AFM
SPERF-CONT-PERF P 2/2
12 DEC 17
Source Exif Data:
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