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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
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Overall
length |
|
67.5 m. |
|
222 ft. 9 in. |
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Height
|
|
17.1 m. |
|
57 ft. 5 in. |
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Fuselage
diameter |
|
5.64 m. |
|
18 ft. 6 in. |
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Maximum
cabin width |
|
5.28 m. |
|
17 ft. 4 in. |
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Cabin
length |
|
53.56 m. |
|
175 ft. 9 in. |
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Wingspan
(geometric) |
|
63.5 m. |
|
208 ft. 2 in. |
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Wing
area (reference) |
|
438 m2 |
|
4,707 ft2 |
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Wing
sweep (25% chord) |
|
31.1 degrees |
|
31.1 degrees |
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Wheelbase |
|
27.59 m. |
|
90 ft. 6 in. |
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Wheel
track |
|
10.69 m. |
|
35 ft. 1 in. |
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| BASIC
OPERATING DATA |
|
|
metric |
|
imperial |
|
|
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Engines |
|
four RR Trent 500 |
|
four RR Trent 500 |
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Engine
thrust range |
|
235 (249) kN |
|
53,000 (56,000)
lb. slst |
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Typical
passenger seating |
|
313 (3-class) |
|
313 (3-class) |
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Range
(w/max. passengers) |
|
16,670 km. |
|
9,000 nm. |
|
|
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Max.
operating Mach number (Mmo) |
|
0.86 Mo. |
|
0.86 Mo. |
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Bulk
hold volume - Standard/option |
|
19.7 / 13.76 m3 |
|
695 / 486 ft3 |
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
|
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Maximum
ramp weight |
|
372 (380) tonnes |
|
820.1 (837.8)
lbs. x 1000 |
|
|
|
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|
Maximum
takeoff weight |
|
372 (380) tonnes |
|
820.1 (837.8)
lbs. x 1000 |
|
|
|
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|
Maximum
landing weight |
|
243 (246) tonnes |
|
535.7 (542.3)
lbs. x 1000 |
|
|
|
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Maximum
zero fuel weight |
|
230 (232) tonnes |
|
506.9 (511.3)
lbs. x 1000 |
|
|
|
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|
Maximum
fuel capacity |
|
215,260 (222,850) Litres |
|
56,870 (58,875) US gal.
|
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Typical
volumetric payload |
|
43.3 tonnes |
|
95.5
lbs. x 1000 |
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