Specifications
A318-100 | ||||
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Cockpit crew | Two | |||
Seating capacity | 132 (1-class, maximum) 117 (1-class, typical) 107 (2-class, typical) |
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Cargo capacity | 21.21 m3 (749 cu ft) | |||
Length | 31.44 m (103 ft 2 in) | |||
Wingspan | 34.10 m (111 ft 11 in) | |||
Wing area | 122.6 m2 (1,320 sq ft) | |||
Wing sweepback | 25 degrees | |||
Tail height | 12.51 m (41 ft 1 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 (87,000 lb) | |||
Maximum zero-fuel weight (MZFW) | 54,500 kg (120,000 lb) | |||
Maximum take-off weight (MTOW) | 68.0 t (150,000 lb) | |||
Cruising speed | Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft) | |||
Maximum speed | Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft) | |||
Maximum range, fully loaded | 3,100 nmi (5,700 km; 3,600 mi) | |||
Take off run at MTOW (sea level, ISA) | 1,828 m (5,997 ft) | |||
Maximum fuel capacity | 24,210 L (5,330 imp gal; 6,400 US gal) | |||
Service ceiling | 12,000 m (39,000 ft) | |||
Engines (×2) | Pratt & Whitney PW6000 series or CFM International CFM56-5 series |
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Thrust (×2) | 96–106 kN (22,000–24,000 lbf) |
Source: Airbus, Airliners.net
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