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ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT ATTEMPT (Cont'd)
If the APU is available, it may be started when below FL 250 and the APU BLEED may be used
for engine start below FL 200.
WING ANTI ICE......................................................................................................................OFF
APU BLEED............................................................................................................................ON
�� IN SEQUENCE:
ENG MASTERS (all non running engines)......................................................................OFF
�� After 30 s:
ENG MASTERS (one at a time)................................................................................. ON
APPROACH PREPARATION
Note: Final descent slope, when configured (CONF 3; L/G DOWN) will be approximately
800 ft/1 nm (with no wind).
BARO.......................................................................................................................................SET
CREW MASKS/OXY SUPPLY (below FL 100).........................................................................OFF
ENG DUAL FAILURE - FUEL REMAINING -
COMMON APPROACH FOR THE ACTION
Applicable to:
APPROACH PREPARATION
Note: Final descent slope, when configured (CONF 3; L/G DOWN) will be approximately
800 ft/1 nm (with no wind).
BARO.......................................................................................................................................SET
CREW MASKS/OXY SUPPLY (below FL 100).........................................................................OFF
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 189/194
FCOM 19 AUG 10
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT ATTEMPT
Applicable to: ,
As long as none of the engines recover, the flight crew must apply this paper procedure when
required by the ECAM ENG DUAL FAILURE procedure. If time permits, clear ECAM alerts, and
check the STATUS SD page.
LAND ASAP
OPTIMUM RELIGHT SPD........................................................................................................300 KT
In the case of a speed indication failure (volcanic ash), Pitch attitude for optimum relight speed is:
WEIGHT PITCH (°)
At or below 50 000 kg/110 000 lb -4.5
60 000 kg/132 000 lb -3.5
70 000 kg/154 000 lb -2.5
At 300 kt, the aircraft can fly up to about 2 nm per 1 000 ft (with no wind).
LANDING STRATEGY.................................................................................................... DETERMINE
Determine whether a runway can be reached, or the most appropriate place for a forced
landing/ditching.
VHF1/HF1 �� /ATC1....................................................................................................................USE
Notify air traffic control of the nature of the emergency, and state intentions. If there is no contact
with air traffic control, switch to code A7700, or transmit a distress message on one of the following
frequencies: VHF frequency 121.5 MHz, HF 2 182 kHz or 8 364 kHz.
ATC........................................................................................................................................NOTIFY
�� IF NO RELIGHT AFTER 30 SEC:
ENG MASTERS...................................................................................................... OFF 30 S/ON
Unassisted start attempts can be repeated until successful, or until APU bleed is available.
�� IF UNSUCCESSFUL:
CREW OXY MASKS (Above FL 100)......................................................................................ON
Cabin altitude will increase, due to the lack of engine bleed: The EXCESS CAB ALT warning
could be triggered. Depending on the situation, to gain gliding distance, the flight crew may
disregard the ECAM emergency descent requirement, because passengers will be provided
with oxygen for a sufficient period of time.
APU (IF AVAIL)..................................................................................................................START
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 190/194
FCOM 19 AUG 10
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT ATTEMPT (Cont'd)
If the APU is available, it may be started when below FL 250 and the APU BLEED may be used
for engine start below FL 200.
WING ANTI ICE......................................................................................................................OFF
APU BLEED............................................................................................................................ON
　
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