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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
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Overall
length |
|
75.3 m. |
|
247 ft. 1 in. |
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Height
|
|
17.3 m. |
|
58 ft. 9 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 |
|
60.98 m. |
|
200 ft. 1 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 |
|
32.89 m. |
|
107 ft. 11 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 |
|
RR Trent 500 |
|
RR Trent 500 |
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Engine
thrust range |
|
249 kN |
|
56,000 (60,000)
lb. slst |
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Typical
passenger seating |
|
380 |
|
380 |
|
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Range
(w/max. passengers) |
|
14,600 km. |
|
7,900 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 |
|
369.2 (381.2) tonnes |
|
813.9 (840.4)
lbs. x 1000 |
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|
|
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|
Maximum
takeoff weight |
|
368 (380) tonnes |
|
811.3 (837.8)
lbs. x 1000 |
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|
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Maximum
landing weight |
|
259 (265) tonnes |
|
571 (584.2)
lbs. x 1000 |
|
|
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Maximum
zero fuel weight |
|
245 (251) tonnes |
|
540.1 (553.4)
lbs. x 1000 |
|
|
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Maximum
fuel capacity |
|
195,520 Litres |
|
51,750
US gal. |
|
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Typical
volumetric payload |
|
55.6 tonnes |
|
122.6
lbs. x 1000 |
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