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

MCT/FLX positions:
THR LEVERS...................................................................................................................... TOGA
�� If FLEX temp is set, and thrust levers are at CLB or between CLB and MCT/FLX
positions:
THR LEVERS................................................................................................................. MCT/FLX
ENG T.O THRUST DISAGREE
Applicable to:
L2 Two or more FADECs select different thrust takeoff mode (DRT, FLX, MAX) on the ground.
Crew awareness.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 70/196
FCOM 19 AUG 10
ENG T.O THRUST DISAGREE
Applicable to: ,
L2 The two FADECs select different thrust takeoff mode (FLEX, MAX) on the ground.
Crew awareness.
ENG 1(2)(3)(4) FUEL FILTER CLOG
Applicable to:
L2Crew awareness.
Maintenance action is due.
ENG 1(2) FUEL FILTER CLOG
Applicable to: ,
L2Crew awareness.
Maintenance action is due.
ENG 1(2) CTL VALVE FAULT
Applicable to: ,
L2HPTCC, LPTCC or nacelle cooling valve is failed open.
L1HPTCC VALVE OPEN
LPTCC VALVE OPEN
NAC COOL VALVE OPEN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 71/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) IGN A(B) FAULT
Applicable to:
L2Crew awareness.
STATUS
INOP SYS
ENG 1 (2)(3)(4) IGN A (B)
ENG 1(2) IGN A(B) FAULT
Applicable to: ,
L2Crew awareness.
STATUS
INOP SYS
ENG 1 (2) IGN A (B)
ENG 1(2)(3)(4) IGN A+B FAULT
Applicable to:
AVOID ADVERSE WEATHER
STATUS
AVOID ADVERSE WEATHER INOP SYS
ENG 1 (2)(3)(4) IGN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 72/196
FCOM 19 AUG 10
ENG 1(2) IGN A+B FAULT
Applicable to: ,
AVOID ADVERSE WEATHER
STATUS
AVOID ADVERSE WEATHER INOP SYS
ENG 1 (2) IGN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 73/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) EIU FAULT
(ON GROUND)
Applicable to:
L2 As the databus between the EIU and the ECU fails:
Autothrust control ‐ is lost on the affected engine.
‐ Thrust reverser is lost on the affected engine, and on the opposite in case of engine 1 or 4.
‐ When idle is selected, only high ground idle is available.
‐ Bleed corrections on N1 limit are lost.
‐ Manual start is lost.
‐ Flex takeoff and derated takeoff are lost.
‐ On ground, the affected engine's anti-ice fault light may be ON, if the engine does not run.
‐ On ground, when the crossbleed valve is open, the 2 packs may be controlled closed.
L1 T.O THR:TOGA ONLY
HI IDLE
L2 FADEC increases minimum idle on the related engine, as if the bleed, pack, wing, and anti ice,
valves were opened.
L1�� BEFORE T.O:
PACK 1+2.............................................................................................................................. OFF
WING ANTI ICE (IF ENG ANTI ICE ON)................................................................................ ON
L2 As the FADEC directly receives the ENG ANTI-ICE pb-sw position, it assumes that the WING
ANTI ICE pb-sw is selected ON, when the engine anti-ice is selected ON.
WING ANTI ICE pb-sw must be selected ON to have the selection in accordance with the
FADEC bleed status.
L1 BOTH PACK AVAIL IN FLT
STATUS
T.O THR:TOGA ONLY
ENG (affected) AUTOSTART ONLY
BOTH PACKS AVAIL IN FLT
ENG (affected) HI IDLE
CAT 2 ONLY
INOP SYS
PACK 1+2
A/THR
REV 1+4 (2)(3)
CAT 3
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 74/196
FCOM 19 AUG 10
ENG 1(2) EIU FAULT
(ON GROUND)
Applicable to: ,
L2 As the databus between the EIU and the FADEC fails:
‐ Autothrust control is lost.
‐ Thrust reverser is lost on the affected engine.
‐ When idle is selected , only high ground idle is available on the affected engine.
‐ Bleed corrections on N1 limit are lost on the affected engine.
‐ Manual start is lost on the affected engine.
‐ Flex takeoff is lost.
L1 T.O THR:TOGA ONLY
HI IDLE
L2 FADEC increases minimum idle on the related engine, as if the bleed, pack, wing, and anti ice,
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A330/A340機組操作手冊 FLIGHT CREW OPERATING MANUAL FCOM 8(146)