Airbus A318

Information about Airbus A318

Airbus A318 modifications:

  • Airbus A318
  • Airbus A318-111
  • Airbus A318-112
  • Airbus A318-121
  • Airbus A318-122
  • Airbus ACJ318
Cockpit crew Two
Exit Limit 136
1-class max. Seating 132 at 29–30 in (74–76 cm) pitch
1-class, typical 117 at 32 in (81 cm) pitch
2-class, typical 107 (8F @ 38 in, 99Y @ 32 in)
Cargo capacity 21.2 m3 (750 cu ft)
Length 31.44 m (103 ft 2 in)
Wingspan 34.10 m (111 ft 11 in)
Wing area 122.4 m2 (1,318 sq ft)
Wing sweepback 25 degrees
Tail height 12.56 m (41 ft 2 in)
Cabin width 3.70 m (12 ft 2 in)
Fuselage width 3.95 m (13 ft 0 in)
Operating empty weight 39,500 kg (87,100 lb)
Maximum zero-fuel weight (MZFW) 54,500 kg (120,200 lb)
Maximum landing weight (MLW) 57,500 kg (126,800 lb)
Maximum take-off weight (MTOW) 68,000 kg (150,000 lb)
Cruising speed Mach 0.78 (829 km/h; 515 mph)
Maximum speed Mach 0.82 (871 km/h; 541 mph)
Range, typical payload 3,100 nmi, 5,750 km
ACJ range 4,200 nmi, 7,800 km
Takeoff (MTOW, SL, ISA) 1,780 m (5,840 ft)
Landing (MLW, SL, ISA) 1,230 m (4,040 ft)
Fuel capacity 24,210 L (5,330 imp gal; 6,400 US gal)
Ceiling 39,100–41,000 ft (11,900–12,500 m)
Engines (×2) 0
Thrust (×2) 96–106 kN (22,000–24,000 lbf)

Source: https://en.wikipedia.org/wiki/Airbus_A318

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