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In exceptional conditions (in flight turn back or diversion), an immediate landing at weight above
maximum landing weight is permitted, provided that the pilot follows the overweight landing
procedure.
WEIGHT LIMITATIONS
Applicable to: ,
Maximum taxi weight....................................................................................... 233 900 kg (515 656 lb)
Maximum takeoff weight (brake release)......................................................... 233 000 kg (513 671 lb)
Maximum landing weight................................................................................. 182 000 kg (401 237 lb)
Maximum zero fuel weight...............................................................................170 000 kg (374 782 lb)
Minimum weight...............................................................................................116 000 kg (255 733 lb)
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 6/6
FCOM 19 AUG 10
In exceptional conditions (in flight turn back or diversion), an immediate landing at weight above
maximum landing weight is permitted, provided that the pilot follows the overweight landing
procedure.
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND
AIRPORT OPERATIONS
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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET LIM-12-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-12-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
ENVIRONMENTAL ENVELOPE......................................................................................................................... 1/4
AIRPORT OPERATIONS....................................................................................................................................2/4
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET LIM-12-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
A330/A340 FLEET LIM-12 P 1/4
FCOM 19 AUG 10
ENVIRONMENTAL ENVELOPE
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
A330/A340 FLEET LIM-12 P 2/4
FCOM 19 AUG 10
ENVIRONMENTAL ENVELOPE
Applicable to: ,
AIRPORT OPERATIONS
Applicable to:
Runway slope (mean)...................................................................................................................± 2 %
Runway altitude.......................................................................................................................12 500 ft
Wind for takeoff and landing :
Maximum crosswind demonstrated............................................................. 27 kt gusting up to 33 kt
Maximum tailwind....................................................................................................................... 10 kt
Maximum crosswind values have been demonstrated with flight controls in normal law, as well as
in direct law, with and without yaw damper.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
A330/A340 FLEET LIM-12 P 3/4
FCOM 19 AUG 10
Wind for passenger/cargo door operation :
Maximum wind for passenger door operation is 40 kt (or 50 kt, if the aircraft nose is orientated into
the wind).
Maximum wind for cargo door operation is 40 kt (or 50 kt, if the aircraft nose is orientated into the
wind, or the cargo door is on the leeward side).
The passenger/cargo door must be closed before the wind speed exceeds 60 kt.
AIRPORT OPERATIONS
Applicable to: ,
Runway slope (mean)...................................................................................................................± 2 %
Runway altitude.......................................................................................................................12 500 ft
Wind for takeoff :
Maximum crosswind demonstrated............................................................................................ 32 kt
Maximum tailwind....................................................................................................................... 10 kt
Maximum crosswind value for takeoff has been certified with flight controls in normal law, as well
　
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