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L1�� EARLY IN APPR:
L2 (If ditching is foreseen, Refer to PRO-ABN-80 DITCHINGprocedure, instead of the following):
L1CAB SECURE...................................................................................................................ORDER
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
�� AT TOUCHDOWN:
ENG MASTERS......................................................................................................................OFF
L2 LP and HP valves close.
L1 APU MASTER SW..................................................................................................................OFF
L2 APU LP valve closes.
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 144/194
FCOM 19 AUG 10
ENG DUAL FAILURE (Cont'd)
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 145/194
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
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
See (1)
BRK Y ACCU PR ONLY
See (2)
SLATS SLOW
INOP SYS
See below
INOP SYS
G+Y HYD F/CTL PROT STABILIZER
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 146/194
FCOM 19 AUG 10
ENG DUAL FAILURE (Cont'd)
R AIL REVERSER 1+2 ADR 2+3
IR 2+3 RA 1+2 SPLR 1+2+4+5
ELAC 2 SEC 2+3 FLAPS
YAW DAMPER A/CALL OUT AP 1+2
A/THR FUEL PUMPS ANTI SKID
N/W. STEER AUTO BRK L/G RETRACT
CAB PR 1+2 PACK 1+2
(1) AL2t landing gear extension, control reverts to direct law in pitch as well as in roll (Refer to
00011770 **Not found**).
(2) 7 full brake applications are available.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 147/194
FCOM 19 AUG 10
ENG DUAL FAILURE
Applicable to:
L2 The ENG DUAL FAILURE warning inhibits the ELEC EMER CONFIG warning.
The FCOM Volume 3 includes all steps of the ECAM ENG DUAL FAILURE procedure.
However, to facilitate handling of all the ECAM procedures associated with a dual engine failure,
it is recommended using the QRH ENG DUAL FAILURE paper procedure that also includes the
DITCHING and FORCED LANDING procedures. When applying the QRH ENG DUAL FAILURE
　
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