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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
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Overall
length |
|
46.66 m. |
|
153 ft. 1 in. |
|
|
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Height
|
|
15.80 m. |
|
51 ft. 10 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 |
|
33.25 m. |
|
109 ft. 1 in. |
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|
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Wingspan
(geometric) |
|
43.90 m. |
|
144 ft. |
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|
|
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Wing
area (reference) |
|
219 m2 |
|
2,360 ft2 |
|
|
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Wing
sweep (25% chord) |
|
28 degrees |
|
28 degrees |
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Wheelbase |
|
15.21 m. |
|
49 ft. 11 in. |
|
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Wheel
track |
|
9.60 m. |
|
31 ft. 6 in. |
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| BASIC
OPERATING DATA |
|
|
metric |
|
imperial |
|
|
|
|
|
|
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|
|
Engines |
|
two CF6-80C2
or PW4000 |
|
two CF6-80C2
or PW4000 |
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|
Engine
thrust range |
|
230-260 kN |
|
52,000-59,000
lb. slst |
|
|
|
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|
Typical
passenger seating (two-class cabin layout) |
|
220 (2-class) |
|
220 (2-class) |
|
|
|
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|
Range
(w/max. passengers) |
|
8,050 (9,600) km. |
|
4,350 (5,200) nm. |
|
|
|
|
|
Max.
operating Mach number (Mmo) |
|
0.84 Mo. |
|
0.84 Mo. |
|
|
|
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|
Bulk
hold volume - Standard/option |
|
17.3 (9.0) m3 |
|
610 (318) ft3 |
|
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
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|
Maximum
ramp weight |
|
150.9 (164.9) tonnes |
|
332.7 (363.5)
lbs. x 1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
150 (164) tonnes |
|
330.7 (361.6)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
123 (124) tonnes |
|
271.2 (273.4)
lbs. x 1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
113 (114) tonnes |
|
249.1 (251.3)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
61,070 (75,470) Litres |
|
16,130 (19,940) US gal.
|
|
|
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|
Typical
volumetric payload |
|
26.7 (21.6) tonnes |
|
58.9 (47.6)
lbs. x 1000 |
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