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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 ), 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 68 000 kg (150 000 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.
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 32/182
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
10 75 73 71 69 66 63 60 57
15 75 73 71 69 66 63 60 57
20 75 73 71 69 66 63 60 56
25 75 73 71 69 66 63 58
30 75 72 71 68 65 60 55
35 74 72 70 67 62 57
40 74 72 69 64
45 74 70 66
50 71 67
55 68
MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1000 lb)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 33/182
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 , use FLAP 3 for landing.
In all cases, if landing configuration is different from FLAP FULL, use 1+F for go-around.
Note: At very high weights, VFE CONF1 is close to VLS clean. To select CONF1, deselect
A/THR, decelerate to (or slightly below) VLS and select CONF1 when below VFE. When
established at CONF1, the crew can reengage A/THR and 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,
　
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