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‐ The reference chord length is 4.193 m (13.76 ft). It is 16.31 m (53.51 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 4/10
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 4.193 m (13.76 ft). It is 14.71 m (48.26 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 5/10
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 4.193 m (13.76 ft). It is 14.71 m (48.26 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 6/10
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to: MSN
CG limits are given in percentage of the reference chord ‐ length aft of the leading edge.
‐ The reference chord length is 4.193 m (13.76 ft). It is 16.31 m (53.51 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 7/10
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 4.193 m (13.76 ft). It is 16.31 m (53.51 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......................................................................................... 64 400 kg (141 978 lb)
Maximum takeoff weight (brake release)...........................................................64 000 kg (141 090 lb)
Maximum landing weight................................................................................... 61 000 kg (134 480 lb)
Maximum zero fuel weight.................................................................................57 000 kg (125 660 lb)
Minimum weight...................................................................................................35 400 kg (78 042 lb)
In exceptional cases (in flight turn back or diversion), an immediate landing at weight above
maximum landing weight is permitted, provided the pilot follows the overweight landing procedure.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 8/10
FCOM 19 AUG 10
WEIGHT LIMITATIONS
Applicable to: ,
, MSN,
Maximum taxi weight......................................................................................... 83 400 kg (183 865 lb)
Maximum takeoff weight (brake release)...........................................................83 000 kg (182 983 lb)
Maximum landing weight................................................................................... 73 500 kg (162 040 lb)
Maximum zero fuel weight.................................................................................69 500 kg (153 220 lb)
Minimum weight.................................................................................................47 500 kg (104 718 lb)
In exceptional cases (in flight turn back or diversion), an immediate landing at weight above
maximum landing weight is permitted, provided the pilot follows the overweight landing procedure.
WEIGHT LIMITATIONS
Applicable to:
Maximum taxi weight......................................................................................... 70 400 kg (155 200 lb)
Maximum takeoff weight (brake release)...........................................................70 000 kg (154 320 lb)
Maximum landing weight................................................................................... 61 000 kg (134 480 lb)
Maximum zero fuel weight.................................................................................57 000 kg (125 660 lb)
Minimum weight...................................................................................................35 400 kg (78 042 lb)
　
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