 |
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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
|
|
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|
|
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|
Overall
length |
|
63.6 m. |
|
192 ft. 9 in. |
|
|
|
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|
Height
|
|
16.85 m. |
|
56 ft. 5 in. |
|
|
|
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|
Fuselage
diameter |
|
5.64 m. |
|
18 ft 6 in. |
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|
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|
Maximum
cabin width |
|
5.28 m. |
|
17 ft 4 in. |
|
|
|
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Cabin
length |
|
50.35 m. |
|
165 ft 3 in. |
|
|
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|
|
Wingspan
(geometric) |
|
60.3 m. |
|
197 ft 10 in. |
|
|
|
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|
Wing
area (reference) |
|
362 m2 |
|
3,890 ft2 |
|
|
|
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|
Wing
sweep (25% chord) |
|
30 degrees |
|
30 degrees |
|
|
|
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Wheelbase |
|
25.6 m. |
|
84 ft. |
|
|
|
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Wheel
track |
|
10.69 m. |
|
35 ft. 1 in. |
|
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| BASIC
OPERATING DATA |
|
|
metric |
|
imperial |
|
|
|
|
|
|
|
|
|
Engines |
|
two CF6-80E1
or PW4000
or RR Trent 700 |
|
two CF6-80E1
or PW4000
or RR Trent 700 |
|
|
|
|
|
Engine
thrust range |
|
303-320 kN |
|
68,000-
72,000 lb. slst |
|
|
|
|
|
Typical
passenger seating |
|
295 (3-class)
335 (2-class) |
|
295 (3-class)
335 (2-class) |
|
|
|
|
|
Range
(w/max. passengers) |
|
10,800 km. |
|
5,850 nm. |
|
|
|
|
|
Max.
operating Mach number (Mmo) |
|
0.86 Mo. |
|
0.86 Mo. |
|
|
|
|
|
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 |
|
230.9 (233.9) tonnes |
|
509 (515.7)
lbs. x 1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
230 (233) tonnes |
|
507 (513.7)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
185 (187) tonnes |
|
407.9 (412.3)
lbs. x 1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
173 (175) tonnes |
|
381.3 (385.7)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
97,530 Litres |
|
25,770 US gal. |
|
|
|
|
|
Typical
volumetric payload |
|
45.9 tonnes |
|
101.2
lbs. x 1000 |
|
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