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Reduce speed 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
Max 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) PRESSURE ALTITUDE(FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
10 238 229 221 206 194 178 163 149
15 238 229 221 206 192 175 161 147
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 23/140
FCOM 19 AUG 10
OVERWEIGHT LANDING (Cont'd)
OAT (°C) PRESSURE ALTITUDE(FT)
0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
20 238 229 221 205 189 173 158 144
25 238 229 219 202 187 169 153 140
30 238 229 213 198 182 164 148
35 238 222 205 190 175
40 231 213 197 182
45 220 203 187
50 209 193
55
MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1 000 KG)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 24/140
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 229 t (504 853 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 229 t (504 853 lb).
JETTISON �� ..................................................................................................................CONSIDER
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.
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 speed to reach VLS at runway threshold.
For automatic landing, maintain VLS + 5.
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
Max. braking may be used after nosewheel touchdown. But, if landing distance permits, delay
or reduce braking to fully benefit from available runway length.
�� Landing complete:
BRAKE FANS �� .................................................................................................ON if available
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
10 238 230 222 207 194 179 163 149
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A330/A340 FLEET PRO-ABN-80 P 25/140
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
15 238 230 222 207 192 176 161 147
20 238 230 222 206 190 174 158 143
25 238 230 220 203 188 170 153 138
　
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