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INOP SYS
(BLUE HYD or YELLOW HYD
PART SPLRS) (1)
REV 1+4(2)(3)(1+4)
CAT 3 DUAL
ENG 1(2)(3)(4) BLEED
G ENG 1 PUMP (G ENG 4
PUMP)
GEN 1(2)(3)(4)
ALTN BRK (2)
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 2 or 3 shutdown)
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 95/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) REV UNLOCKED - FWSPAGE (Cont'd)
(2) (If ENG 2 shutdown)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 96/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) REV UNLOCKED
Applicable to:
�� On the ground:
L2Note: This ECAM warning may be triggered after an aircraft bounce at landing. Any aircraft
bounce should be reported to the maintenance.
L1�� If IDLE not automatically selected by FADEC:
THR LEVER (AFFECTED ENGINE)...............................................................................IDLE
�� If IDLE automatically selected by FADEC:
ENG (AFFECTED) AT IDLE
THR LEVER (AFFECTED ENGINE)...............................................................................IDLE
L2 Select thrust lever at idle, even if idle is automatically selected by the FADEC.
L1�� In flight:
MAX SPEED...................................................................................................................... 300/.82
�� If IDLE not automatically selected by FADEC:
THR LEVER (AFFECTED ENGINE)...............................................................................IDLE
�� If IDLE automatically selected by FADEC:
ENG (AFFECTED) AT IDLE
THR LEVER (AFFECTED ENGINE)...............................................................................IDLE
L2 Select thrust lever at idle, even if idle is automatically selected by the FADEC.
L1�� IF BUFFET:
L2 The warning alone without buffet or vibration may be a false warning.
L1MAX SPEED................................................................................................................250/.70
THR LEVER (AFFECTED ENGINE)...............................................................................IDLE
ENG MASTER (AFFECTED ENGINE)............................................................................ OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2)(3)(4) SHUT DOWN
Refer to PRO-ABN-70-A After ENG 1(2)(3)(4) SHUT DOWN
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 97/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) REV UNLOCKED (Cont'd)
Note: 1. Lateral control (up to the equivalent of ½ stick) is applied by the normal
lateral law and thus spoilers are extended and large aileron deflection are
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 98/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) REV UNLOCKED (Cont'd)
L12
STATUS
MAX SPEED............................................................ 300/.82
• IF BUFFET:
MAX SPEED......................................................250/.70
APPR PROC
FOR LDG...................................................................USE FLAP 3
This line is replaced by “FOR LDG: USE FLAP 3” when CONF 3
is selected, as a reminder.
�� IF BUFFET:
GPWS FLAP MODE.........................................................OFF
FOR LDG............................................................ USE FLAP 2
This line is replaced by “FOR LDG: USE FLAP 2” when
CONF 2 is selected, as a reminder.
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
APPR SPD...........................................................VLS +15 KT
The approach speed of VLS +15 kt is recommended, both
to increase lateral control and to maintain the approach
　
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