曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

may be advantageous (GPWS, WINDSHEAR, etc.), reduce speed with care below VLS
and respect the minimum control speed.
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 76/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
L12
STATUS
�� If ENG 1(2) FIRE pushbutton pushed:
AVOID ICING CONDITIONS
�� If REV unlocked:
MAX SPEED.............................................................. 300/0.78
APPR PROC
�� 4 doors not stowed (CFM) or reverser deployed (IAE):
�� IF BUFFET:
FOR LDG......................................................USE FLAP 1
APPR SPD.................................................VREF + 55 KT
RUD TRIM......................................................5 DEG R(L)
When committed to land, set 5 ° rudder trim towards live
engine.
A/THR.........................................................................OFF
GPWS FLAP MODE...................................................OFF
�� WHEN LDG ASSURED:
L/G..........................................................................DOWN
�� AT 800 FT AGL:
TARGET SPD............................................VREF + 40 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
�� 1, 2, or 3 doors not stowed (CFM), or reverse detected
unlocked (IAE):
�� IF BUFFET:
FOR LDG......................................................USE FLAP 3
GPWS LDG FLAP 3.................................................... ON
APPR SPD.................................................VREF + 10 KT
LDG DIST PROC...................................................APPLY
INOP SYS
CAT 3 DUAL
ENG 1(2) BLEED
PACK 1(2)
MAIN GALLEY
GEN 1(2)
G ENG 1 PUMP or
Y ENG 2 PUMP
WING A. ICE (1)
AFT CRG HEAT
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 77/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM
�� If WING A/ICE off and ENG 1(2) FIRE pushbutton not
pressed:
�� IF PERF PERMITS:
X BLEED................................................................. OPEN
If no obstacle constraint exists, open the XBLEED
selector, and decrease the single engine gross ceiling
by1 200 ft (Refer to PER-CRZ-OEI-ALT-10 GROSS
CEILINGS AT LONG RANGE AND GREEN DOT
SPEEDS).
ECON FLOW................................................................ON
AFT CRG HOT AIR �� ............................................OFF
The ECON FLOW pb must be selected ON, and the aft
cargo heat �� must be selected OFF, due to precooler
performance.
�� IF NO ENG 1(2) DAMAGE:
CONSIDER ENG 1 (2) RELIGHT
CAT 3 SINGLE ONLY
ONE PACK ONLY IF WAI ON
See (2)
(1) (if affected ENG FIRE pushed)
(2)
NL2ote: If available, the APU may ‐ be started and the APU GEN used
‐ If the ENG 1 FIRE pb is pushed, APU bleed must not be used.
If ENG 2 FIRE pb is pushed, APU bleed may be used, provided the X BLEED selector
is set at SHUT.
‐ After landing, the Fuel Used value of the engine, shutdown in flight, becomes
incorrect.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 78/194
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN
Applicable to: MSN,
LAND ASAP
�� If wing Anti-ice ON:
�� If Elec Emer Config:
PACK 1.............................................................................................................................OFF
L2 In Emer Elec, only Pack 1 pb-sw can be controlled off.
L1�� If not Elec Emer Config:
PACK (AFFECTED SIDE) .............................................................................................. OFF
L2 One pack must be closed when wing anti-ice is in use due to precooler performance.
L1 X BLEED (IF ENG FIRE PB NOT PUSHED)............................................................... OPEN
L2 X BLEED pb-sw must be opened to have symmetrical wing anti-icing.
L1 ENG MODE SEL..................................................................................................................... IGN
L2Continuous ignition is selected, in order to protect the remaining engine.
L1�� IF NO FUEL LEAK:
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 10(144)