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�� When landing configuration is established:
DECELERATE TO CALCULATED APPROACH SPEED IN FINAL APPROACH
FOR GO AROUND
The table (See below) provides the MAX SPEEDS for the abnormal configurations.
�� IF SLATS FAULT:
�� FOR CIRCUIT:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed: MAX SPEED - 10 KT
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 18/22
FCOM 19 AUG 10
LANDING WITH SLATS OR FLAPS JAMMED (Cont'd)
�� FOR DIVERSION:
SELECT CLEAN CONFIGURATION
Recommended flaps retraction speed is between MAX SPEED - 10 kt and MAX SPEED.
Recommended diversion speed: MAX SPEED - 10 KT.
�� IF FLAPS FAULT:
�� FOR CIRCUIT:
MAINTAIN SLATS/FLAPS CONFIGURATION
Recommended speed: MAX SPEED - 10 KT
�� FOR DIVERSION:
�� If FLAPS jammed at 0:
SELECT CLEAN CONFIGURATION
Recommended speed for slats retraction is between MAX SPEED - 10 kt and MAX
SPEED of actual slat/flap position.
Normal operating speeds
�� If FLAPS jammed > 0:
MAINTAIN SLAT/FLAP CONFIGURATION
Recommended speed for diversion: MAX SPEED - 10 KT
Note: In the majority of cases, VFE on PFD ‐ is equal to the MAX SPEED. In
this case, VFE can be used as MAX SPEED. In case the SPD LIM flag
is displayed on the PFD, use the MAX SPEED displayed on the ECAM
status page.
‐ In some cases, MAX SPEED - 10 kt may be a few knots higher than the
VFE. In this situation, pilot may follow the VFE.
‐ In case of a go-around with CONF FULL selected, the L/G NOT DOWN
warning is triggered at landing gear retraction.
Flaps
Slats F = 0 0 < F ≤ 1 0 < F ≤ 2 0 < F ≤ 3 F > 3
S = 0 NO LIMITATION
0 < S ≤ 1 230 kt 215 kt 200 kt 185 kt Not allowed
(177 kt)
1 < S ≤ 3 200 kt 200 kt 185 kt 177 kt
S > 3 177 kt 177 kt 177 kt 177 kt
MAX SPEED
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 19/22
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
ALTERNATE FLIGHT PLANNING tables, Refer to PER-FPL-FLP-ALN-20
ALTERNATE PLANNING ISA) and multiply this result by 1.6 (SLATS
EXTENDED), or 1.8 (FLAPS EXTENDED, or 2 (SLATS and FLAPS
EXTENDED), to obtain the fuel consumption required to reach the destination in
the current configuration.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 20/22
FCOM 19 AUG 10
LANDING WITH SLATS OR FLAPS JAMMED
Applicable to: ,
, MSN
LANDING CONF.....................................................................................................................CONF 3
�� Repeat the following until landing configuration is reached:
SPEED SEL......................................................................................................VFE NEXT - 5 KT
Decelerate towards VFE NEXT - 5 kt but not below VLS. In case of turbulence, to avoid VFE
exceedance, the pilot may decide to decelerate to a lower speed, but not below VLS.
Note: ‐ The autopilot may be used down to 500 ft AGL. As it is not tuned for abnormal
configurations, its behavior can be less than optimum and must be monitored.
‐ Approach with selected speed is recommended.
‐ A/THR is recommended, except in the case of a G+B SYS LO PR warning.
‐ OVERSPEED warning and VLS, displayed on the PFD, are computed according to
the actual flaps/slats position.
‐ VFE and VFE NEXT are displayed on the PFD according to the FLAPS lever
position. If not displayed, use the placard speeds.
‐ If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever
can be set in the required next position, while the speed is reduced to follow VLS
reduction as surfaces extend. The VFE warning threshold should not be triggered.
In this case, disconnect the A/THR. A/THR can be re-engaged when the landing
configuration is established.
As speed reduces through VFE NEXT:
FLAPS LEVER................................................................................................ONE STEP DOWN
�� When landing configuration is established:
　
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