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�� If FLAPS jammed > 0:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed for diversion: MAX SPEED -10 KT
Increased fuel consumption.
Note: In case the SPD LIM flag is displayed on ‐ the PFD, use the MAX SPEED
displayed on the ECAM status page.
‐ In case of a go-around with CONF FULL selected, the L/G NOT DOWN
warning is triggered at landing gear retraction.
‐ In some cases, MAX SPEED -10 KT may be a few knots higher than the
VFE. In this situation, pilots may follow the VFE.
Flaps
Slats F = 0 0 < F ≤ 1 1 < F ≤ 2 2 < F ≤ 3 F > 3
S = 0 NO LIMITATION
0 < S ≤ 1 240 kt 215 kt
1 < S 215 kt 205 kt
196 kt 186 kt 180 kt
MAX SPEED
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A330/A340 FLEET PRO-ABN-10 P 18/18
FCOM 19 AUG 10
LANDING WITH SLATS OR FLAPS JAMMED (Cont'd)
CAUTION For flight with SLATS or FLAPS extended, fuel consumption is increased.
Refer to the fuel flow indication.
As a guideline, determine the fuel consumption in clean configuration at the
same altitude without airspeed limitation (e.g. From the ALTERNATE FLIGHT
PLANNING tables, Refer to PER-FPL-FLP-ALN-20 ALTERNATE PLANNING
- ISA) and multiply this result by 1.5 (SLATS EXTENDED), or 2.2 (FLAPS
EXTENDED), or 2.5 (SLATS and FLAPS EXTENDED), to obtain the fuel
consumption required to reach the destination in the current configuration.
NO FLAPS NO SLATS LANDING
Applicable to: ALL
SPEED SEL....................................................................................................................GREEN DOT
Initial approach, with autothrust in selected mode, is recommended.
Autopilot is permitted down to 500 ft AGL.
GPWS FLAP MODE..................................................................................................................... OFF
FLAPS LEVER........................................................................................................................CONF 1
Disregard the CONF 2 requirement on the ECAM status page.
Set FLAP handle to CONF 1, to benefit from SRS guidance, in case of a go-around.
The VFE displayed on the PFD depends on the flap lever position. So, a false VFE will be given.
Plan a long stabilized approach.
�� For the final approach:
A/THR....................................................................................................................................OFF
SPD SEL............................................................................................................................ VAPP
Select VLS on the PFD (or VREF + 50 kt, if VLS is not available).
At 500 ft, reduce speed to obtain VLS - 5 kt (or VREF + 45 kt, if VLS is not available) at
touchdown.
LDG DIST PROC............................................................................................................... APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A330/A340 FLEET PRO-ABN-21 P 1/70
FCOM 19 AUG 10
AIR PACK 1(2) OVHT
Applicable to:
PACK (AFFECTED)...................................................................................................................... OFF
L2 High flow is automatically selected on the remaining pack.
The fault light goes off when the overheat disappears.
L1 FWD CRG COOLING .................................................................................................................. OFF
L2 (These lines are only displayed, if the forward (aft) cargo cooling is installed, and if the automatic
closure of the cargo cooling cold air valve is not operative.)
L1 �� WHEN PACK OVHT OUT:
PACK (AFFECTED)..................................................................................................................ON
FWD CRG COOLING...............................................................................................................ON
L2 (These lines are only displayed, if the forward (aft) cargo cooling is installed, and if the
automatic closure of the cargo cooling cold air valve is not operative.)
L12
STATUS
�� WHEN PACK OVHT OUT:
PACK (AFFECTED)............................................................ON
FWD CRG COOLING ........................................................ON
(These lines are only displayed, if the forward cargo cooling
is installed and if the automatic closure of the cargo cooling
cold air valve is not operative.)
INOP SYS
PACK 1(2)
FWD CRG TEMP
　
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