 |
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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
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Overall
length |
|
37.57 m. |
|
123 ft. 3 in. |
|
|
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Height
|
|
11.76 m. |
|
38 ft. 7 in. |
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|
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Fuselage
diameter |
|
3.95 m. |
|
13 ft. |
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Maximum
cabin width |
|
3.70 m. |
|
12 ft. 1 in. |
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|
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Cabin
length |
|
27.51 m. |
|
90 ft. 3 in. |
|
|
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|
Wingspan
(geometric) |
|
34.10 m. |
|
111 ft. 10 in. |
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|
|
|
|
Wing
area (reference) |
|
122 m2 |
|
1,320 ft |
|
|
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Wing
sweep (25% chord) |
|
25 degrees |
|
25 degrees |
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Wheelbase |
|
12.64 m. |
|
41 ft. 5 in. |
|
|
|
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Wheel
track |
|
7.59 m. |
|
24 ft. 11 in. |
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| BASIC
OPERATING DATA |
|
|
metric |
 |
imperial |
|
|
|
|
|
|
|
|
|
Engines |
|
two CFM56-5
or IAE V2500 |
|
two CFM56-5
or IAE V2500 |
|
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|
Engine
thrust range |
|
98-120 kN |
|
22,000-27,000
lb. slst |
|
|
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|
Typical
passenger seating |
|
150 |
|
150 |
|
|
|
|
|
Range
(w/max. passengers) |
|
5,950 km. |
|
3,200 nm. |
|
|
|
|
|
Max.
operating Mach number (Mmo) |
|
0.82 Mo. |
|
0.82 Mo. |
|
|
|
|
|
Bulk
hold volume - Standard/option |
|
37.41 m3 |
|
1,322 ft3 |
|
|
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
|
|
|
|
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|
Maximum
ramp weight |
|
73.9 (77.4) tonnes |
|
162.9 (170.6)
lbs. x 1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
73.5 (78) tonnes |
|
162 (172)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
64.5 (66) tonnes |
|
142.2 (145.5)
lbs. x 1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
61 (62.5) tonnes |
|
134.5 (137.8)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
24,210 (30,190) Litres |
|
6,400 (7,980) US gal. |
|
|
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|
Typical
volumetric payload |
|
16.6 tonnes |
|
36.59
lbs. x 1000 |
|
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