|
|
A318-100 |
Cockpit crew |
Two |
Seating capacity
|
132 (1-class,
maximum)
117 (1-class, typical)
107 (2-class, typical) |
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
(87,100 lb) |
Maximum zero-fuel weight
(MZFW) |
54,500 kg
(120,200 lb) |
Maximum take-off weight
(MTOW) |
68.0 t
(149,900 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 |
Thrust (×2) |
96–106 kN
(22,000–24,000 lbf) |
|
|
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