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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
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Overall
length |
|
67.9 m. |
|
222 ft. 8 in. |
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Height
|
|
17.1 m. |
|
56 ft. 1 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) |
|
63.45 m. |
|
208 ft. 2 in. |
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Wing
area (reference) |
|
439.4 m2 |
|
4,729 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 |
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|
metric |
|
imperial |
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|
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Engines |
|
four RR Trent 500 |
|
four RR Trent 500 |
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Engine
thrust range |
|
236 (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) |
|
16,100 (16,700) km. |
|
8,670 (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 |
|
373.2 (381.2) tonnes |
|
822.8 (840.4)
lbs. x 1000 |
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|
|
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Maximum
takeoff weight |
|
372 (380) tonnes |
|
820.1 (837.8)
lbs. x 1000 |
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|
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Maximum
landing weight |
|
243 (246) tonnes |
|
535.7 (542.3)
lbs. x 1000 |
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|
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Maximum
zero fuel weight |
|
230 (232) tonnes |
|
507.1 (511.5)
lbs. x 1000 |
|
|
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Maximum
fuel capacity |
|
214,810 (222,000) Litres |
|
56,750 (58,646) US gal.
|
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Typical
operating weight empty |
|
170.9 (174.8) tonnes |
|
376.8 (385.4)
lbs. x 1000 |
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Typical
volumetric payload |
|
43.3 tonnes |
|
95.5
lbs. x 1000 |
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