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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET LIM-11-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 1/6
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to:
CG limits are given in percentage of the reference chord ‐ length aft of the leading edge.
‐ The reference chord length is 7.27 m (23.85 ft). It is 28.15 m (92.36 ft) aft of the aircraft nose.
‐ The CG must always be within these limits regardless of fuel load.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 2/6
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to:
‐ CG limits are given in percentage of the reference chord length aft of the leading edge.
The reference chord length is 7.27 m (23.85 ft). It is 28.15 m (92.36 ‐ ft) aft of the aircraft nose.
‐ The CG must always be within these limits regardless of fuel load.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 3/6
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to:
‐ CG limits are given in percentage of the reference chord length aft of the leading edge.
‐ The reference chord length is 7.27 m (23.85 ft). It is 28.15 m (92.36 ft) aft of the aircraft nose.
‐ The CG must always be within these limits regardless of fuel load.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 4/6
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to: ,
‐ CG limits are given in percentage of the reference chord length aft of the leading edge.
‐ The reference chord length is 7.27 m (23.85 ft). It is 28.15 m (92.36 ft) aft of the aircraft nose.
‐ The CG must always be within these limits regardless of fuel load.
WEIGHT LIMITATIONS
Applicable to:
Maximum taxi weight....................................................................................... 271 900 kg (599 425 lb)
Maximum takeoff weight (brake release)............................................... 271 000 kg (597 445 lb) See *
Maximum landing weight....................................................................... 190 000 kg (418 870 lb) See *
Maximum zero fuel weight.....................................................................178 000 kg (392 410 lb) See *
Minimum weight...............................................................................................130 000 kg (286 600 lb)
* Weight varies with CG (Refer to LIM-11 CENTER OF GRAVITY LIMITS)
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A330/A340 FLEET LIM-11 P 5/6
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.
WEIGHT LIMITATIONS
Applicable to:
Maximum taxi weight....................................................................................... 271 900 kg (599 425 lb)
Maximum takeoff weight (brake release)............................................... 271 000 kg (597 446 lb) See *
Maximum landing weight................................................................................. 192 000 kg (423 280 lb)
Maximum zero fuel weight...............................................................................178 000 kg (392 410 lb)
Minimum weight...............................................................................................130 000 kg (286 600 lb)
* Weight varies with CG (Refer to LIM-11 CENTER OF GRAVITY LIMITS)
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....................................................................................... 212 900 kg (469 360 lb)
Maximum takeoff weight (brake release)......................................................... 212 000 kg (467 375 lb)
Maximum landing weight................................................................................. 174 000 kg (383 600 lb)
Maximum zero fuel weight...............................................................................164 000 kg (361 554 lb)
Minimum weight...............................................................................................121 000 kg (266 757 lb)
　
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