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ELEC GEN 1(2)(3)(4)/APU GEN/EXT PWR OVERLOAD
Applicable to:
GALLEY.......................................................................................................................................OFF
L2 This warning is only displayed if galley automatic shedding has failed.
STATUS
INOP SYS
GALLEY
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 7/166
FCOM 19 AUG 10
ELEC GEN 1(2)/APU GEN/EXT PWR OVERLOAD
Applicable to: ,
GALLEY.......................................................................................................................................OFF
L2 This warning is only displayed if galley automatic shedding has failed.
STATUS
INOP SYS
GALLEY
ELEC STATIC INV FAULT
Applicable to: ALL
L2Crew awareness
ELEC ECMU 1(2) FAULT
Applicable to:
GEN 1+2 (3+4).....................................................................................................................KEEP ON
L2 The closure control of associated generator line contactors is lost, but these contactors remain
closed provided the GEN pb-sw is at on.
The associated AC BUS TIE contactors open. The APU line contactor opens if ECMU 1 is affected.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 8/166
FCOM 19 AUG 10
ELEC ECMU 1(2) FAULT (Cont'd)
STATUS
GEN 1+2 (3+4)...............................................................KEEP ON INOP SYS
ECMU 1(2)
APU GEN (1)
PART GALLEY
EXT PWR A (IF ECMU 2
FAULT)
EXT PWR B (1)
(1) (IF ECMU 1 FAULT)
ELEC ECMU 1(2) FAULT
Applicable to: ,
GEN 1(2)............................................................................................................................. KEEP ON
L2 The closure control of associated generator line contactors is lost, but these contactors remain
closed provided the GEN pb-sw is at on.
The associated AC BUS TIE contactors open. The APU line contactor opens if ECMU 1 is affected.
STATUS
GEN 1(2)........................................................................ KEEP ON INOP SYS
ECMU 1(2)
APU GEN (if ECMU 1 FAULT)
PART GALLEY
EXT PWR A (1)
EXT PWR B (2)
(1) (if ECMU 2 FAULT (on ground))
(2) (if ECMU 1 FAULT (on ground))
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 9/166
FCOM 19 AUG 10
ELEC ECMU 1(2) FAULT
Applicable to:
GEN 1+2 (3+4).....................................................................................................................KEEP ON
L2 The closure control of associated generator line contactors is lost, but these contactors remain
closed provided the GEN pb-sw is at on.
The associated AC BUS TIE contactors open. The APU line contactor opens if ECMU 1 is affected.
GEN 1(2)............................................................................................................................. KEEP ON
L2 The closure control of associated generator line contactors is lost, but these contactors remain
closed provided the GEN pb-sw is at on.
The associated AC BUS TIE contactors open. The APU line contactor opens if ECMU 1 is affected.
STATUS
GEN 1+2 (3+4)...............................................................KEEP ON INOP SYS
ECMU 1(2)
APU GEN (1)
PART GALLEY
EXT PWR A (IF ECMU 2
FAULT)
EXT PWR B (1)
(1) (IF ECMU 1 FAULT)
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 10/166
FCOM 19 AUG 10
ELEC ECMU 1(2) FAULT (Cont'd)
STATUS
GEN 1(2)........................................................................ KEEP ON INOP SYS
ECMU 1(2)
APU GEN (if ECMU 1 FAULT)
PART GALLEY
EXT PWR A (1)
EXT PWR B (2)
(1) (if ECMU 2 FAULT (on ground))
(2) (if ECMU 1 FAULT (on ground))
ELEC BAT 1(2) OR APU BAT FAULT
Applicable to: ,
In case of thermal runaway or short circuit:
BAT (AFFECTED)...................................................................................................................OFF
L2 Battery contactor is automatically opened by Battery Charge Limiter, but the automatic opening
must be manually confirmed open.
STATUS
• IF APU BAT and APU TR fault:
APU START NOT AVAIL
INOP SYS
BAT 1(2) or APU BAT
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(149)
