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If the failure occurs during takeoff (with thrust lever in TOGA or FLX/MCT gate), FADEC maintains
T.O., FLEX, TO, DRT TO �� thrust until thrust reduction, after which the maximum available thrust
is CLB. If the failure occurs while thrust lever is between idle and MCT, FADEC selects the higher
TLA limited at CLB in flight, or the FADEC selects idle thrust on the ground.
L1 LAND ASAP
�� On ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR FLX/MCT)
L2 FADEC selects idle power automatically.
L1�� In flight:
MAX AVAIL PWR: CLB (IF TLA AT OR BELOW MCT AND L/G UP)
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA/FLX/MCT AND L/G DOWN)
L2 At landing gear extension (or when MN < 0.40 if the onside EIU is failed), the FADEC
automatically selects idle thrust.
L1 A/THR (IF ON)...............................................................................................................KEEP ON
A/THR (IF NOT ON).................................................................................................................ON
L2With autothrust engaged active, thrust is automatically managed between idle and the higher
TLA position as long as the landing gear is up.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 109/196
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE (Cont'd)
L12
STATUS
LAND ASAP
�� On ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR
FLX/MCT)
�� In flight:
ENG (AFFECTED) AVAIL MAX PWR: CLB
�� WHEN L/G DOWN,
or
WHEN MN < 0.40:
(Displayed if the onside EIU is failed)
ENG (AFFECTED) AT IDLE
APPR PROC
FOR LDG...................................................................USE FLAP 3
This is line is replaced by “FOR LDG: USE FLAP 3” when CONF
3 is selected, as a reminder.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
INOP SYS
ENG 1(2) THR
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 110/196
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE
Applicable to:
L2 Both thrust lever angle TLA sensors are not in agreement on one engine.
If the failure occurs during takeoff (with thrust lever in TOGA or FLX/MCT gate), FADEC maintains
T.O., FLEX, TO, DRT TO �� thrust until thrust reduction, after which the maximum available thrust
is MCT. If the failure occurs while thrust lever is between idle and MCT, FADEC selects the higher
TLA limited at MCT in flight or FADEC selects idle thrust on the ground or in approach phase (at
landing gear extension).
L1 LAND ASAP
�� On the ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR FLX/MCT)
L2 FADEC selects idle power automatically.
L1�� In flight:
MAX AVAIL PWR: MCT (IF TLA AT OR BELOW MCT AND L/G UP)
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA/FLX/MCT AND L/G DOWN)
L2 At landing gear extension (or when MN < 0.40 if the onside EIU is failed), the FADEC
automatically selects idle thrust.
L1 A/THR (IF ON)...............................................................................................................KEEP ON
A/THR (IF NOT ON).................................................................................................................ON
L2With autothrust engaged active, thrust is automatically managed between idle and the higher
TLA position as long as the landing gear is up.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 111/196
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE (Cont'd)
L12
STATUS
LAND ASAP
�� On ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR
FLX/MCT)
�� In flight:
ENG (AFFECTED) AVAIL MAX PWR: CLB
�� WHEN L/G DOWN,
or
WHEN MN < 0.40:
(Displayed if the onside EIU is failed)
ENG (AFFECTED) AT IDLE
APPR PROC
FOR LDG...................................................................USE FLAP 3
INOP SYS
ENG 1(2) THR
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 112/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) THR LEVER FAULT
Applicable to:
L2No validated thrust lever angle for one engine thrust lever.
L1�� On ground:
ENG (AFFECTED) AT IDLE
　
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