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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 93/194
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.
REV AVAIL ON GND
ENG (affected) AVAIL MAX PWR : MCT
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 94/194
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):
ENG (AFFECTED) IDLE POWER ONLY.
L2 In only one TLA is at IDLE or less, the FADEC automatically selects IDLE power.
L1 THR LEVER (AFFECTED)................................................................................................... IDLE
�� During take-off (if one or both TLA are at TOGA or FLX/MCT):
ENG (AFFECTED) TO, FLX, OR DRT TO ��
L2 If the failure occurs during takeoff (with thrust lever in TOGA or FLX/MCT gate), FADEC
maintains TO., FLX TO., or DRT TO �� thrust until thrust reduction, after which the maximum
available thrust is MCT.
L1�� In cruise (with slats retracted):
AVAIL MAX POWER : MCT
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 > 0.55, if the onside EIU is failed) the FADEC selects the larger
TLA power limited to MCT.
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.
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) the FADEC selects IDLE.
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 95/194
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.
REV AVAIL ON GND
ENG (affected) AVAIL MAX PWR : MCT
ON GND ENG (affected) MAX PWR : IDLE.
INOP SYS
ENG 1(2) THR
A318/A319/A320/A321 FLIGHT CREW
　
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