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Use the ECAM flap setting, if required for abnormal operations. In all other cases:
FULL is preferred for ‐ optimized landing performance.
‐ If the aircraft weight is above the maximum weight for go-around See , use FLAP 3 for landing.
In all cases, if landing configuration is different from FLAP FULL, use 1+F for go-around.
Note: For weights greater than 70 000 kg (or 154 000 lb) S speed is greater than VFE CONF 2
(200 kt). Consequently the crew must select on FCU a speed below 200 kt before setting
FLAPS 2. When in FLAPS 2, the crew can use managed speed again.
LDG DIST...............................................................................................................................CHECK
PACK 1 and 2.............................................................................................. OFF or supplied by APU
Selecting packs OFF (or supplied from APU) will increase the maximum thrust available from the
engines, in the event of a go-around.
�� In the final stages of approach:
TARGET SPEED.....................................................................................................................VLS
Reduce the selected speed on the FCU to reach VLS at runway threshold.
Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min).
�� At main landing gear touchdown:
REVERSE THRUST................................................................................. USE MAX AVAILABLE
�� After nosewheel touchdown:
BRAKES................................................................................................APPLY AS NECESSARY
Maximum braking may be used after nosewheel touchdown. But, if landing distance permits,
delay or reduce braking to take full benefit of the available runway length.
�� Landing complete:
BRAKE FANS �� ...................................................................................................................ON
Be prepared for tire deflation, if temperatures exceed 800 °C.
OAT °C AIRPORT ELEVATION (FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
<10 85 83 84 81 77 71 66 61
15 85 83 83 81 77 70 64 57
20 85 83 83 81 75 67 61 55
25 85 83 83 79 72 64 58
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 38/182
FCOM 19 AUG 10
OVERWEIGHT LANDING (Cont'd)
OAT °C AIRPORT ELEVATION (FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
30 84 83 81 77 69
35 84 83 79 73 66
40 84 81 75 69
45 82 76 70
50 78 72
55
MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1000 KG)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 39/182
FCOM 19 AUG 10
OVERWEIGHT LANDING
Applicable to: MSN,
LDG CONF.................................................................................................................. AS REQUIRED
Use the ECAM flap setting, if required for abnormal operations. In all other cases:
FULL is preferred for ‐ optimized landing performance.
‐ If the aircraft weight is above the maximum weight for go-around See Table below, use FLAP 3
for landing.
In all cases, if landing configuration is different from FLAP FULL, use 1+F for go-around.
Note: For weights greater than 70 000 kg (or 154 000 lb) S speed is greater than VFE CONF 2
(200 kt). Consequently the crew must select on FCU a speed below 200 kt before setting
FLAPS 2. When in FLAPS 2, the crew can use managed speed again.
LDG DIST...............................................................................................................................CHECK
PACK 1 and PACK 2................................................................................... OFF or supplied by APU
Selecting packs OFF (or supplied from APU) will increase the maximum thrust available from the
engines, in the event of a go-around.
�� In the final stages of approach:
TARGET SPEED.....................................................................................................................VLS
Reduce the selected speed on the FCU to reach VLS at runway threshold.
Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min).
�� At main landing gear touchdown:
REVERSE THRUST................................................................................. USE MAX AVAILABLE
�� After nosewheel touchdown:
BRAKES................................................................................................APPLY AS NECESSARY
Maximum braking may be used after nosewheel touchdown. But, if landing distance permits,
　
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