 |
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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
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|
Overall
length |
|
63.6 m. |
|
208 ft. 10 in. |
|
|
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Height
|
|
16.85 m. |
|
55 ft. 3 in. |
|
|
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Fuselage
diameter |
|
5.64 m. |
|
13 ft. |
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|
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Maximum
cabin width |
|
3.70 m. |
|
18 ft. 6 in. |
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|
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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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|
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Wing
area (reference) |
|
361.6 m2 |
|
3,892 ft2 |
|
|
|
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|
Wing
sweep (25% chord) |
|
30 degrees |
|
30 degrees |
|
|
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Wheelbase |
|
25.60 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 |
|
four CFM56-5C4/P |
|
four CFM56-5C4/P |
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Engine
thrust range |
|
139-151 kN |
|
31,200-
34,000 lb. slst |
|
|
|
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|
Typical
passenger seating |
|
295 |
|
295 |
|
|
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|
|
Range
(w/max. passengers) |
|
13,350 (13,700) km. |
|
7,200 (7,400) 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 |
|
275.9 (277.4) tonnes |
|
606.0 (609.6)
lbs. x
1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
275 (276.5) tonnes |
|
183 (206.1)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
190 (192) tonnes |
|
418.9 (423.3)
lbs. x
1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
178 (181) tonnes |
|
392.4 (399)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
140,640 (147,850) Litres |
|
37,150 (39,060) US gal.
|
|
|
|
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|
Typical
operating weight empty |
|
129.3 (130.2) tonnes |
|
285 (287)
lbs. x 1000 |
|
|
|
|
|
Typical
volumetric payload |
|
43.5 (41) tonnes |
|
95.9 (90.5)
lbs. x 1000 |
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