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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 28/182
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 71 69 68 65 63 61 59 56
15 71 69 68 65 63 61 59 56
20 71 69 68 65 63 61 59 55.
25 71 69 68 65 63 61 58 54
30 71 69 68 65 63 61 57
35 71 69 68 65 63
40 71 69 68 65
45 71 69 68
50 71 69
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 29/182
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 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,
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 89 85 81 77 72 67 61 56
15 89 85 81 77 71 65 59 54
20 88 84 81 75 69 63 57 52
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 30/182
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
25 88 84 79 73 67 61 56 50
30 87 81 76 70 64 59 54
35 84 78 73 67 62
40 81 75 69 64
45 76 70 65
50 72 67
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 31/182
FCOM 19 AUG 10
OVERWEIGHT LANDING
Applicable to:
Automatic landing is certified up to the Maximum Landing Weight (MLW). Autoland flight tests have,
however, been successful up to 69 t (152 117 lb).
Depending on the situation (e.g. emergency or other) and provided that the runway is approved for
automatic landing, the flight crew can decide to perform an autoland up to 69 t (152 117 lb).
　
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