| AIRCRAFT DIMENSIONS |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
 |
|
Overall length |
 |
56.15 m. |
 |
184 ft. 3 in. |
|
 |
 |
 |
|
Height |
 |
17.24 m. |
 |
56 ft. 7 in. |
|
 |
 |
 |
|
Fuselage diameter |
 |
7.31 m. |
 |
24 ft. |
|
 |
 |
 |
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Maximum cabin width |
 |
3.70 m. |
 |
12 ft. 2 in. |
|
 |
 |
 |
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Cabin length |
 |
37.7 m. |
 |
123 ft. 8 in. |
|
 |
 |
 |
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Wingspan (geometric) |
 |
44.84 m. |
 |
147 ft. 2 in. |
|
 |
 |
 |
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Wing area (reference) |
 |
122.40 m2. |
 |
1,317 ft2. |
|
 |
 |
 |
|
Wing sweep (25% chord) |
 |
25 degrees |
 |
25 degrees |
|
 |
 |
 |
|
Wheelbase |
 |
11.05 m. |
 |
36.25 ft. |
|
 |
 |
 |
|
Wheel track |
 |
7.59 m. |
 |
25 ft. |
|
 |
|
 |
|
 |
|
 |
 |
| BASIC OPERATING DATA |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
 |
|
Engines |
 |
GE CF6-80C2A8 |
 |
GE CF6-80C2A8 |
|
 |
 |
 |
|
Engine thrust range |
 |
119 - 120 kN |
 |
26,752 - 26,977 lb. slst |
|
 |
 |
 |
|
Typical passenger seating |
 |
na |
 |
na |
|
 |
 |
 |
|
Range (w/max. passengers) |
 |
40 - tonne payload:2,779 km. / 26 - tonne payload: 4,632 km. |
 |
39.3 - tons payload:1,500 nm. / 25.6 - tons payload: 2,500 nm. |
|
 |
 |
 |
|
Max. operating Mach number (Mmo) |
 |
0.82 Mo. |
 |
0.82 Mo. |
|
 |
 |
 |
|
Bulk hold volume - Standard/option |
 |
na |
 |
na |
|
 |
|
 |
|
 |
|
 |
|
 |
| DESIGN WEIGHTS |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
 |
|
Maximum ramp weight |
 |
na |
 |
na |
|
 |
 |
 |
|
Maximum takeoff weight |
 |
155 tonnes |
 |
341,713 lb. |
|
 |
 |
 |
|
Maximum landing weight |
 |
140 tonnes |
 |
308,644 lb. |
|
 |
 |
 |
|
Maximum zero fuel weight |
 |
133.5 tonnes |
 |
294,314 lb. |
|
 |
 |
 |
|
Maximum fuel capacity |
 |
23,860 (32,250)(34,430) Litres |
 |
6,303 (8,520)(9,095) US gal. |
|
 |
 |
 |
|
Typical operating weight empty |
 |
na |
 |
na |
|
 |
 |
 |
|
Typical volumetric payload |
 |
47 tonnes |
 |
103,616 lb. |
|
 |
|
 |
|
 |
|
 |
Airbus January 2013
| Total orders |
12433 |
| Total deliveries |
7665 |
| In operation |
7117 |
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