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lateral law and thus spoilers will be extended and large aileron deflection will
be used. However adequate roll control remains.
2. Do not follow beta and beta target.
Apply full rudder and rudder trim towards the running engines.
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 105/196
FCOM 19 AUG 10
ENG 1(2) REV UNLOCKED (Cont'd)
L12
STATUS
MAX SPEED............................................................ 300/.82
• IF BUFFET:
MAX SPEED......................................................250/.70
APPR PROC
FOR LDG...................................................................USE FLAP 3
�� IF BUFFET:
GPWS FLAP MODE.........................................................OFF
FOR LDG............................................................ USE FLAP 2
APPR SPD.........................................................VLS +15 KTS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
FUEL UNBALANCE.......................................................MONITOR
• If selected by FADEC:
ENG 1 (2) AT IDLE
• If ENG 1 shutdown:
SLATS SLOW
• If ENG 2 shutdown:
FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
BLUE HYD (YELLOW HYD)
PART SPLRS
REV 1(2)
CAT 3 DUAL
ENG 1(2) BLEED
G ENG 1(2) PUMP
B ENG 1 PUMP (Y ENG 2
PUMP)
GEN 1(2)
ALTN BRK (1)
PART GALLEY
Note: The approach
speed of
VLS +15 kt is
recommended,
both to increase
lateral control
and to maintain
the approach
angle-of-attack
at a reasonable
value. Note that
a reduction in lift
may result from
this failure and,
therefore, a higher
angle-of-attack
than normal may
be advised at a
given speed.
(1) (if ENG 1 shutdown)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 106/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) REV ISOL FAULT
(ON GROUND)
Applicable to:
L2 The hydraulic shut-off valve for the reverser system is abnormally open.
Crew awareness.
ENG 1(2)(3)(4) 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
TO, FLX 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, the FADEC selects the higher
TLA limited at MCT in flight or the FADEC selects idle thrust on ground.
L1�� On ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR FLX/MCT)
L2 The FADEC automatically selects idle power.
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 DN)
L2 At landing gear extension (or when MN < 0.46 if the associated EIU is failed), the FADEC
automatically selects idle thrust.
L1 A/THR (IF ON)...............................................................................................................KEEP ON
A/THR (IF NOT ON).................................................................................................................ON
L2With the autothrust engaged, 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 107/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) THR LEVER DISAGREE (Cont'd)
L12
STATUS
�� On ground:
ENG (AFFECTED) AT IDLE (IF TLA NOT AT TOGA OR
FLX/MCT)
�� In flight:
�� If TLA at, or below, MCT:
ENG (AFFECTED) MAX AVAIL PWR: MCT
�� WHEN L/G DOWN:
or
WHEN MN < 0.46:
(Displayed, if the affected EIU is failed)
ENG (AFFECTED) AT IDLE
APPR PROC
FOR LDG...................................................................USE FLAP 3
INOP SYS
ENG 1(2)(3)(4) THR
REV 1+4(2)(3)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 108/196
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.
　
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