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as in direct law, with and without yaw damper.
Wind for landing :
Maximum crosswind demonstrated............................................................. 32 kt gusting up to 40 kt
Maximum tailwind....................................................................................................................... 10 kt
Maximum crosswind value for landing has been demonstrated with flight controls in normal law, as
well as in direct law, with and without yaw damper.
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.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
ENVIRONMENTAL ENVELOPE AND AIRPORT OPERATIONS
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A330/A340 FLEET LIM-12 P 4/4
FCOM 19 AUG 10
LIMITATIONS
SPEED LIMITATIONS
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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
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FCOM 19 AUG 10
LIM-13-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
MAXIMUM OPERATING SPEED VMO/MMO.................................................................................................... 1/12
MAXIMUM DESIGN MANEUVERING SPEED VA.............................................................................................1/12
BUFFET ONSET...............................................................................................................................................4/12
MINIMUM CONTROL SPEEDS.........................................................................................................................7/12
STALLING SPEEDS......................................................................................................................................... 8/12
MAXIMUM FLAPS/SLATS SPEEDS................................................................................................................ 11/12
GEAR DOWN SPEEDS..................................................................................................................................11/12
MAXIMUM TIRE SPEED................................................................................................................................ 12/12
WINDSHIELD WIPERS IN USE....................................................................................................................... 12/12
COCKPIT WINDOWOPEN............................................................................................................................ 12/12
SPEEDBRAKES..............................................................................................................................................12/12
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET LIM-13-PLP-TOC P 2/2
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A330/A340 FLIGHT CREW
OPERATING MANUAL
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SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 1/12
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MAXIMUM OPERATING SPEED VMO/MMO
Applicable to: ALL
The maximum operating limit speed VMO/MMO may not be deliberately exceeded in any regime of
flight.
MAXIMUM DESIGN MANEUVERING SPEED VA
Applicable to:
(Applies in alternate or direct flight control laws only).
If alternate or direct law is active, full ailerons and rudder should only be applied at speeds below VA.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
SPEED LIMITATIONS
A330/A340 FLEET LIM-13 P 2/12
FCOM 19 AUG 10
If alternate or direct law is active, maneuvres involving an angle-of-attack near stall should only be
performed at speeds below VA.
CAUTION Rapid and large alternating control inputs, especially in combination with large
changes in pitch, roll, or yaw (e.g. large sideslip angles) may result in structural
failures at any speed, even below VA.
MAXIMUM DESIGN MANEUVERING SPEED VA
Applicable to: ,
(Applies in alternate or direct flight control laws only).
If alternate or direct law is active, full ailerons and rudder should only be applied at speeds below VA.
If alternate or direct law is active, maneuvres involving an angle-of-attack near stall should only be
performed at speeds below VA.
A330/A340 FLIGHT CREW
　
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