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| AIRCRAFT
DIMENSIONS |
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|
metric |
 |
imperial |
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Overall
length |
|
73 m. |
|
239 ft. 3 in. |
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Height
|
|
24.1 m. |
|
79 ft. 7 in. |
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Fuselage
diameter |
|
7.14 m. |
|
23 ft. 5 in. |
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Maximum
cabin width |
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Cabin
length |
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50.68 m. |
|
166 ft. 3 in. |
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Wingspan
(geometric) |
|
79.8 m. |
|
261 ft. 8 in. |
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Wing
area (reference) |
|
845 m2 |
|
9,100 ft2 |
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Wing
sweep (25% chord) |
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33.5 degrees |
|
33.5 degrees |
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Wheelbase |
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30.4 m. |
|
99 ft. 8 in. |
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Wheel
track |
|
14.3 m. |
|
46 ft. 11 in. |
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| BASIC
OPERATING DATA |
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|
metric |
|
imperial |
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|
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Engines |
|
Trent 900 or
GP 7000 |
|
Trent 900 or
GP 7000 |
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Engine
thrust range |
|
340 kN |
|
76,500 lb. slst |
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Main
deck volume |
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Range
(w/max.) |
|
10,400 km. |
|
5,600 nm. |
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Max.
operating Mach number (Mmo) |
|
0.89 Mo. |
|
0.89 Mo. |
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Bulk
hold volume - Standard/option |
|
14.3 m3 |
|
505 ft3 |
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
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Maximum
ramp weight |
|
592 tonnes |
|
1,305
lbs. X 1000 |
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|
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Maximum
takeoff weight |
|
590 tonnes |
|
1,300
lbs. X 1000 |
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|
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Maximum
landing weight |
|
427 tonnes |
|
941
lbs. X 1000 |
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Maximum
zero fuel weight |
|
402 tonnes |
|
886
lbs. X 1000 |
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Maximum
fuel capacity |
|
310,000 Litres |
|
81,890
US gal. |
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Typical
operating weight empty |
|
252.2 tonnes |
|
555.5
lbs. X 1000 |
|
|
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|
Typical
volumetric payload |
|
149.4 to 157.4 tonnes |
|
329.4 to 347
lbs. X 1000 |
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