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OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 96/194
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE
Applicable to: MSN
4566,,
L2 Both Thrust Lever Angle (TLA) sensors not in agreement on one engine.
L1 LAND ASAP
�� On ground (if both TLA not at TOGA or FLX/MCT or if only one TLA is at TOGA or
FLX/MCT and the other is below IDLE):
ENG (AFFECTED) IDLE POWER ONLY.
L2 In that situation, the FADEC automatically selects IDLE
L1 THR LEVER (AFFECTED)................................................................................................... IDLE
�� During take-off (if both TLA are above IDLE) :
ENG (AFFECTED) TO, FLX, OR DRT TO ��
L2 If both TLA are above IDLE, the FADEC automatically selects TO, FLX TO, or DRT TO ��
thrust until thrust reduction, after which the maximum available thrust is CLB.
L1�� In cruise (with slats retracted):
AVAIL MAX POWER : CLB
L2 In flight, if the failure occurs while the thrust lever is between idle and MCT, and if the slats are
not extended, (or when MN > M 0.55, if the onside EIU is failed) the FADEC selects the larger
TLA power limited to CLB.
L1 A/THR (IF ENGAGED) .................................................................................................KEEP ON
A/THR (IF NOT ENGAGED AND IF SLATS ARE NOT EXTENDED) .................................... ON
L2With A/THR engaged, thrust is automatically managed between IDLE and higher TLA position.
L1�� In approach (with slats extended):
ENG (AFFECTED) AT IDLE (WHEN SLATS ARE EXTENDED FOR APPROACH)..
L2 If TLA at, or below, MCT and if the slats are extended for approach, (or when MN < 0.47, if the
onside EIU is failed).
L1 THR LEVER (AFFECTED)................................................................................................... IDLE
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 97/194
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE (Cont'd)
L12
STATUS
�� If TLA at, or below, MCT
�� WHEN SLATS OUT
(Displayed, if slats not extended), or
�� WHEN MN < 0.47
(Displayed, if the onside EIU is failed)
ENG (AFFECTED) AT IDLE
For any case of thrust lever disagree (TO, FLEX, or
between Idle and MCT), the FADEC will command idle
thrust for the approach when slats are extended (or when
the Mach number is less than 0.47, if associated EIU is
failed). It is independent of the autothrust condition. The
affected engine’s thrust remains definitively at idle, even
for go-around.
ENG (affected) AVAIL MAX PWR : clb
ON GND ENG (affected) MAX PWR : IDLE.
INOP SYS
ENG 1(2) THR
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 98/194
FCOM 19 AUG 10
ENG 1(2) THR LEVER DISAGREE
Applicable to:
L2 Both Thrust Lever Angle (TLA) sensors not in agreement on one engine.
L1 LAND ASAP
�� On ground (if both TLA not at TOGA or FLX/MCT or if only one TLA is at TOGA or
FLX/MCT and the other is below IDLE):
ENG (AFFECTED) IDLE POWER ONLY.
L2 In that situation, the FADEC automatically selects IDLE
L1 THR LEVER (AFFECTED)................................................................................................... IDLE
�� During take-off (if both TLA are above IDLE) :
ENG (AFFECTED) TO, FLX, OR DRT TO ��
L2 If both TLA are above IDLE, the FADEC automatically selects TO, FLX TO, or DRT TO ��
thrust until thrust reduction, after which the maximum available thrust is CLB.
L1�� In cruise (with slats retracted):
AVAIL MAX POWER : CLB
L2 In flight, if the failure occurs while the thrust lever is between idle and MCT, and if the slats are
not extended, (or when MN > M 0.55, if the onside EIU is failed) the FADEC selects the larger
TLA power limited to CLB.
L1 A/THR (IF ENGAGED) .................................................................................................KEEP ON
A/THR (IF NOT ENGAGED AND IF SLATS ARE NOT EXTENDED) .................................... ON
L2With A/THR engaged, thrust is automatically managed between IDLE and higher TLA position.
L1�� In approach (with slats extended):
ENG (AFFECTED) AT IDLE (WHEN SLATS ARE EXTENDED FOR APPROACH)..
L2 If TLA at, or below, MCT and if the slats are extended for approach, (or when MN < 0.47, if the
onside EIU is failed).
L1 THR LEVER (AFFECTED)................................................................................................... IDLE
　
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