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S/F JAMMED PROC...........................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM for
managing the approach, and be prepared for a go-around.
The ECAM procedure (below) just provides the final flap lever
selection for landing, depending on the failed flaps’ position.
�� If FLAPS < 3:
FOR LDG............................................................ USE FLAP 2
Selecting FLAP 2 instead of FLAP 3 permits VMAX display
on PFD to be increased.
�� If FLAPS = 3:
FOR LDG..........................................................USE FLAPS 3
�� If FLAPS > 3:
FOR LDG......................................................USE FLAP FULL
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM
INOP SYS
FLAPS
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 28/142
FCOM 19 AUG 10
F/CTL FLAPS/SLATS FAULT/LOCKED
Applicable to: ,
This figure gives the MAX SPEED value displayed on ECAM in case of failure for all Slats/Flaps
positions.
0 ≤ Flaps < 1+F 1+F ≤ Flaps < 2 2 ≤ Flaps < 3 3 ≤ Flaps < FULL Flaps FULL
0 ≤ Slats < 1 VREF + 50 VREF + 40 VREF + 30 VREF + 25 VREF + 25
1 ≤ Slats < 2 VREF + 30 VREF + 20 VREF + 15 VREF + 10 VREF + 10
Slats = 2 VREF + 30 VREF + 15 VREF + 10 VREF + 5 VREF
VLS
CAUTION For flight with SLATS or FLAPS extended, fuel consumption is increased. Refer to
fuel flow indication.
As a guideline, determine the fuel consumption in clean configuration at same
altitude without airspeed limitation (e.g. from ALTERNATE FLIGHT PLANNING
tables) and multiply this result by 1.5 (SLATS EXTENDED) or 2.2 (FLAPS
EXTENDED) or 2.5 (SLATS and FLAPS EXTENDED) to give the fuel consumption
required to reach the destination in the current configuration.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 29/142
FCOM 19 AUG 10
F/CTL FLAPS/SLATS FAULT/LOCKED
Applicable to:
This figure gives the MAX SPEED value displayed on ECAM in case of failure for all Slats/Flaps
positions.
0 ≤ Flaps < 1+F 1+F ≤ Flaps < 2 2 ≤ Flaps ≤ 3 Flaps >3
0 ≤ Slats < 1 VREF + 50 VREF + 35 VREF + 35 VREF + 30
1 ≤ Slats < 2 VREF + 25 VREF + 10 VREF + 10 VREF + 5
Slats = 2 VREF + 25 VREF + 10 VREF + 5 VREF
VLS
CAUTION For flight with SLATS or FLAPS extended, fuel consumption is increased. Refer to
fuel flow indication.
As a guideline, determine the fuel consumption in clean configuration at same
altitude without airspeed limitation (e.g. from ALTERNATE FLIGHT PLANNING
tables) and multiply this result by 1.4 (SLATS EXTENDED) or 2 (FLAPS
EXTENDED) or 2.3 (SLATS and FLAPS EXTENDED) to give the fuel consumption
required to reach the destination in the current configuration.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 30/142
FCOM 19 AUG 10
CONFIG SLATS (FLAPS) NOT IN T.O CONFIG
Applicable to: ALL
L2Crew awareness
F/CTL LVR OUT OF DETENT
Applicable to: ALL
L2 The flaps lever is between two detents.
Crew awareness
F/CTL FLAP/MCDU DISAGREE
Applicable to: ALL
L2 This caution is triggered when pressing the T.O CONFIG key in phase 2 or at takeoff initiation if the
flap lever position and the FLAPS position as entered on the MCDU PERF T.O Page are different.
Crew awareness
F/CTL FLAP LVR NOT ZERO
Applicable to: ALL
L2 The flap lever is not at zero when altitude is above 22 000 ft.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 31/142
FCOM 19 AUG 10
F/CTL PRIM 1(2)(3) FAULT
Applicable to:
PRIM (AFFECTED)..................................................................................................... OFF THEN ON
�� IF UNSUCCESSFUL:
PRIM (AFFECTED).................................................................................................................OFF
�� In case of dual PRIM failure:
SPD BRK................................................................................................................ DO NOT USE
L2 In case of a third PRIM failure: If the speed brakes are out, they immediately retract, inducing a
strong pitch down effect.
L1�� If the trim tank pump is operative:
　
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