曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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 155/194
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 156/194
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 157/194
FCOM 19 AUG 10
ENG DUAL FAILURE
Applicable to: ,
, MSN
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 2.5 degrees down. For weight above 60 000 kg /132 000 lb, raise the nose by 1 ° for every
additional 10 000 kg /22 000 lb (e.g. if weight is 70 000 kg /154 000 lb pitch is 3.5 ° down).
At 280 kt, the aircraft can fly up to about :
‐ 2.0 nm per 1 000 ft at 0 000 kg /132 000 lb
‐ 2.2 nm per 1 000 ft at 760 000 kg/154 000 lb
‐ 2.4 nmper 1 000 ft at 80 000 kg /176 000 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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 11(8)
