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LANDING GEAR
Applicable to:
The center gear may be inhibited by ground maintenance action.
For weight limitations, see the MEL (Refer to 99 Duref Cible MEL).
NOSEWHEEL STEERING (NWS)
Applicable to: ,
The nosewheel steering angle is limited to 65 °.
Asymmetric thrust may be used during turns at high NWS angles, in order to initiate the turn and to
keep the aircraft moving during the turn. But, it should not be used to tighten the turn.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
LANDING GEAR
A330/A340 FLEET LIM-32 P 2/4
FCOM 19 AUG 10
For towing and pushback, the nosewheel steering angle is limited to 60 °. The ground crew should
make use of the 60 ° markings on the nose landing gear door, to ensure that this limitation is not
exceeded.
NOSEWHEEL STEERING (NWS)
Applicable to:
The nosewheel steering angle is limited to 72 °.
No braked pivot is allowed (ie. differential braking cannot be used to fully stop one main gear).
Asymmetric thrust should be used during the turn, to maintain a continuous speed (between 5 and 10
knots). Some anticipation is required to ensure that asymmetric thrust is available at the beginning of
the turn.
For towing and pushback, the nosewheel steering angle is limited to 65 °. The ground crew should
make use of the 65 ° markings on the nose landing gear door, to ensure that this limitation is not
exceeded.
Towbarless operation on the nose landing gear (towing and pushback) is approved when using the
accepted towbarless towing vehicles listed in the Airbus SIL 09–002.
TAXI WITH DEFLATED TIRES
Applicable to:
If tire damage is suspected after landing, or after a rejected takeoff, inspection of the tires is required
before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with the
following limitations :
1. If one tire is deflated on one or more gears (ie. a maximum of four tires), the speed should be
limited to 7 kt when turning.
2. If two tires are deflated on the same main gear (the other main gear tires not being deflated), or on
the center gear, the speed should be limited to 3 kt, and the nosewheel steering angle should be
limited to 30 °.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
LANDING GEAR
A330/A340 FLEET LIM-32 P 3/4
FCOM 19 AUG 10
TAXI WITH DEFLATED TIRES
Applicable to: ,
If tire damage is suspected after landing, or after a rejected takeoff, inspection of the tires is required
before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with the
following limitations :
1. If one tire is deflated on one or more gears (ie. a maximum of three tires), the speed should be
limited to 7 kt when turning.
2. If two tires are deflated on the same main gear (the other main gear tires not being deflated),
speed should be limited to 3 kt, and the nosewheel steering angle should be limited to 30 °.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
LANDING GEAR
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A330/A340 FLEET LIM-32 P 4/4
FCOM 19 AUG 10
LIMITATIONS
NAVIGATION
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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
NAVIGATION
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET LIM-34-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-34-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
INERTIAL REFERENCE SYSTEM.......................................................................................................................1/2
ISIS......................................................................................................................................................................1/2
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS).................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
NAVIGATION
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET LIM-34-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
NAVIGATION
A330/A340 FLEET LIM-34 P 1/2
FCOM 19 AUG 10
INERTIAL REFERENCE SYSTEM
Applicable to: ALL
Refer to DSC-22_20-60-130 GENERAL.
ISIS
Applicable to: ,
When both PFDs are lost, the ISIS bugs function must not be used.
ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)
Applicable to: ALL
• Aircraft navigation is not to be predicated on the use of the terrain display.
　
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