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ENG 1(2) AFTER SHUT DOWN (Cont'd)
GPWS LDG FLAP 3.................................................... ON
APPR SPD.................................................VREF + 10 KT
LDG DIST PROC...................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM
�� If WING A/ICE off and ENG 1(2) FIRE pushbutton not
pressed:
�� IF PERF PERMITS:
X BLEED................................................................. OPEN
If no obstacle constraint exists, open the XBLEED
selector, and decrease the single engine gross ceiling
by1 200 ft (Refer to PER-CRZ-OEI-ALT-10 GROSS
CEILINGS AT LONG RANGE AND GREEN DOT
SPEEDS).
�� IF NO ENG 1 (2) DAMAGE:
CONSIDER ENG 1 (2) RELIGHT
CAT 3 SINGLE ONLY
ONE PACK ONLY IF WAI ON
See (2)
(1) (if affected ENG FIRE pushed)
(2)
NL2ote: If available, the APU may ‐ be started and the APU GEN used
‐ If the ENG 1 FIRE pb is pushed, APU bleed must not be used.
If ENG 2 FIRE pb is pushed, APU bleed may be used, provided the X BLEED selector
is set at SHUT.
‐ After landing, the Fuel Used value of the engine, shutdown in flight, becomes
incorrect.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 70/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN
Applicable to:
LAND ASAP
�� If wing Anti-ice ON:
�� If Elec Emer Config:
PACK 1.............................................................................................................................OFF
L2 In Emer Elec, only Pack 1 pb-sw can be controlled off.
L1�� If not Elec Emer Config:
PACK (AFFECTED SIDE) .............................................................................................. OFF
L2 One pack must be closed when wing anti-ice is in use due to precooler performance.
L1 X BLEED (IF ENG FIRE PB NOT PUSHED)............................................................... OPEN
L2 X BLEED pb-sw must be opened to have symmetrical wing anti-icing.
L1 ENG MODE SEL..................................................................................................................... IGN
L2Continuous ignition is selected, in order to protect the remaining engine.
L1�� IF NO FUEL LEAK:
IMBALANCE..................................................................................................................MONITOR
TCAS MODE SEL �� ............................................................................................................. TA
�� If REV unlocked:
�� IF BUFFET:
MAX SPEED .............................................................................................................. 240 KT
�� If ENG FIRE pb pushed:
XBLEED ............................................................................................................................. SHUT
WING ANTI ICE......................................................................................................................OFF
AVOID ICING CONDITIONS
SECONDARY FAILURES
* HYD
* ELEC
* AIR BLEED
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 71/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
L2Note: In some conditions, with full asymmetric power, the aircraft may be control-limited before
reaching the protection system limit. Therefore, in extreme conditions, where low speed
may be advantageous (GPWS, WINDSHEAR, etc.), reduce speed with care below VLS
and respect the minimum control speed.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 72/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
L12
STATUS
�� If ENG 1(2) FIRE pushbutton pushed:
AVOID ICING CONDITIONS
�� IF A/C ICING SEVERE
MIN SPD........................................................... ALPHA PROT
�� If REV unlocked:
MAX SPEED.............................................................. 300/0.78
APPR PROC
�� 4 doors not stowed (CFM) or reverser deployed
(IAE/PW):
�� IF BUFFET:
FOR LDG......................................................USE FLAP 1
APPR SPD.................................................VREF + 55 KT
RUD TRIM......................................................5 DEG R(L)
When committed to land, set 5 ° rudder trim towards live
　
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