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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(2)
CAT 3
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 75/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) EIU FAULT
(IN FLIGHT)
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 THR LEVER (AFFECTED ENGINE).............................................................................MAN ADJUST
L2Note: It is recommended that the autothrust be disconnected when in descent, and to manually
adjust the thrust levers.
STATUS
ENG (affected) AUTOSTART ONLY
ENG (affected) HI IDLE
CAT 2 ONLY
INOP SYS
ENG 1(2)(3)(4)
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 76/196
FCOM 19 AUG 10
ENG 1(2) EIU FAULT
(IN FLIGHT)
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 THR LEVER (AFFECTED ENGINE).............................................................................MAN ADJUST
STATUS
T.O THR: TOGA ONLY
ENG (affected) HI IDLE
ENG (affected) AUTOSTART ONLY
CAT 2 ONLY
INOP SYS
A/THR
REV 1(2)
CAT 3
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 77/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) STALL
Applicable to:
L2 A stall may be indicated by varying degrees of abnormal engine noises, accompanied by flame
from the engine exhaust (and possibly from engine inlet in severe cases), fluctuating performance
parameters, sluggish or no thrust lever response, high EGT and/or a rapid EGT rise when thrust
lever is advanced. Engine stalls must be reported for maintenance action.
L1 THR LEVERS (AFFECTED ENGINE)..........................................................................................IDLE
ENG MASTER (AFFECTED ENGINE)......................................................................................... OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2)(3)(4) SHUT DOWN
L2 Refer to PRO-ABN-70-A After ENG 1(2)(3)(4) SHUT DOWN
Engine restart at crew discretion.
L1�� If the crew detects a stall before the ECAM caution activation:
The following procedure may be applied:
THR LEVER (AFFECTING ENGINE)....................................................................................IDLE
ENG PARAMETERS (AFFECTED ENGINE)....................................................................CHECK
�� If abnormal parameters:
ENG MASTER (AFFECTED ENGINE)............................................................................ OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2)(3)(4) SHUT DOWN
L2 Refer to PRO-ABN-70-A After ENG 1(2)(3)(4) SHUT DOWN
Engine restart at crew discretion.
L1�� If normal parameters:
ENG A ICE (AFFECTED ENGINE)................................................................................... ON
WING A ICE.......................................................................................................................ON
　
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