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G+Y HYD F/CTL PROT STABILIZER
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**). A slight transient pitch up may occur, depending on the frozen THS
position.
(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 132/194
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
paper procedure:
If one or more engines are recovered, apply the corresponding ‐ ECAM procedure instead
‐ If no engines are recovered, continue to apply the QRH ENG DUAL FAILURE paper procedure.
If time permits, clear ECAM alerts, and check the STATUS SD page.
L1 LAND ASAP
ENG MODE SEL............................................................................................................................IGN
L2 An immediate relight attempt is made.
L1 THR LEVERS............................................................................................................................. IDLE
OPTIMUM RELIGHT SPD........................................................................................................300 KT
L2 The optimum airspeed to allow an effective windmilling start attempt is 300 kt.
In case of a speed indication failure (volcanic ash), the pitch attitude for optimum relight speed is
4.5 degrees down. For weight above 50 000 kg/110 000 lb , raise the nose by 1 degree for every
additional 10 000 kg/22 000 lb (e.g. if weight is 60 000 kg/132 000 lb pitch is 3.5 ° down).
At 300 kt, the aircraft can fly up to about:
‐ 2.0 nm per 1 000 ft at 50 000 kg/110 000 lb
‐ 2.2 nm per 1 000 ft at 60 000 kg/132 000 lb
‐ 2.4 nm per 1 000 ft at 70 000 kg/154 000 lb
L1 EMER ELEC PWR (IF EMER GEN NOT IN LINE)...............................................................MAN ON
L2 Pressing EMER ELEC PWR MAN ON pb allows extension of RAT and emer gen coupling.
L1 VHF 1/HF 1 /ATC 1.............................................................................................................. USE
L2‐ In Elec emer configuration only VHF 1, HF 1 and ATC 1 are supplied.
L12‐ Notify traffic control of the nature of the emergency and state intention.
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.
L1 FAC 1.......................................................................................................................... OFF THEN ON
L2 Aircraft is out of trim due to right aileron up float.
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 133/194
FCOM 19 AUG 10
ENG DUAL FAILURE (Cont'd)
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.
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
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(161)
