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L2 Aircraft is out of trim due to right aileron up float.
Resetting FAC 1 permits to recover rudder trim even if no indication is available.
L1�� IF NO RELIGHT AFTER 30 S:
ENG MASTERS...................................................................................................... OFF 30 S/ON
L2 Engine masters sw must be left OFF for 30 s to allow ventilation of combustion chamber.
L1�� If UNSUCCESSFUL:
APU (IF AVAIL)........................................................................................................... START
L2 If the APU is available, APU may be started when below FL 250, and APU BLEED may be
used for engine start below FL 200 if the speed is ≥ 180 kt , or below FL 150 if the speed is
< 150 kt.
APU start is unavailable for 45 s after the loss of both engine generators. This 45 s delay
prevents any interference with emergency generator coupling.
L1WING ANTI ICE............................................................................................................... OFF
APU BLEED....................................................................................................................... ON
ENG MASTERS................................................................................................OFF 30 S/ON
L2 Start one engine at a time.
L1OPTIMUM SPEED.......................................................................................................G DOT
L2 Green dot is displayed on the Captain’s PFD. It represents the best lift-to-drag ratio.
L1�� EARLY IN APPR:
L2 (If ditching is foreseen, Refer to PRO-ABN-80 DITCHINGprocedure, instead of the following):
L1CAB SECURE...................................................................................................................ORDER
USE RUDDER WITH CARE
FOR LDG.................................................................................................................. USE FLAP 3
L2 As only blue hydraulic power is available, only the slats will extend and operating times are
noticeably increased.
L1�� AT FEET AGL:
L/G.......................................................................................................................... GRVTY EXTN
L2 Refer to PRO-ABN-32 L/G GRAVITY EXTENSION.
L1 TARGET SPEED................................................................................................................150 KT
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 164/194
FCOM 19 AUG 10
ENG DUAL FAILURE (Cont'd)
�� AT TOUCHDOWN:
ENG MASTERS......................................................................................................................OFF
L2 LP and HP valves close.
L1 APU MASTER SW..................................................................................................................OFF
L2 APU LP valve closes.
L1 EVAC.............................................................................................................................INITIATE
BAT 1+2 (IF TIME PERMITS BEFORE LEAVING AIRCRAFT).............................................OFF
L2 Batteries are left ON, until the flight crew leaves the aircraft, to ensure cabin communications.
Note: Keep batteries on for at least 10 s after switching the ENG MASTERS sw to OFF, to
allow complete closure of fuel LP valves
L1
ASSOCIATED PROCEDURES
HYD G+Y SYS LO PR
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 165/194
FCOM 19 AUG 10
ENG DUAL FAILURE (Cont'd)
L12
STATUS
MIN RAT SPEED..................................................... 140 KT
MAX SPEED ......................................................... 320/0.77
MAX BRK PR....................................................... PSI
MANEUVER WITH CARE
FUEL GRVTY FEED
AVOID NEGATIVE G FACTOR
APPR PROC
�� IF HYD NOT RECOVERED:
FOR LDG............................................................ USE FLAP 3
�� WHEN CONF 3 AND VAPP:
L/G ................................................................... GRVTY EXTN
(Refer to PRO-ABN-32 L/G GRAVITY EXTENSION). Being
stabilized at VAPP before selecting the gear down enables
the aircraft to be trimmed for approach.
APPR SPD........................................................ VREF +25 KT
Approach speed must be increased, due to the loss of flaps.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or to the Refer to 99 Duref Cible
　
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