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| AIRCRAFT
DIMENSIONS |
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|
metric |
 |
imperial |
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Overall
length |
|
31.44 m. |
|
103 ft. 2 in. |
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Height
|
|
12.51 m. |
|
41 ft. 1 in. |
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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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Cabin
length |
|
21.38 m. |
|
70 ft. 2 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 |
|
10.25 m. |
|
33 ft. 8 in. |
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Wheel
track |
|
7.59 m. |
|
24 ft. 11 in. |
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| BASIC
OPERATING DATA |
|
|
metric |
|
imperial |
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Engines |
|
two CFM56-5
or PW 6000A |
|
two CFM56-5
or PW 6000A |
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Engine
thrust range |
|
96-106 kN |
|
21,600-23,800 lb. slst |
|
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Typical
passenger seating |
|
107 |
|
107 |
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Range
(w/max. passengers) |
|
5,750 km. |
|
3,100 nm. |
|
|
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Max.
operating Mach number (Mmo) |
|
0.82 Mo. |
|
0.82 Mo. |
|
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Bulk
hold volume - Standard/option |
|
21.21 m3 |
|
749 ft3 |
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
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Maximum
ramp weight |
|
59.4 (68.4) tonnes |
|
131 (150.8) lbs. x 1000 |
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Maximum
takeoff weight |
|
59 (68) tonnes |
|
130.1 (149.9)
lbs. x 1000 |
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|
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Maximum
landing weight |
|
56 (57.5) tonnes |
|
123.5 (126.8)
lbs. x 1000 |
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|
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Maximum
zero fuel weight |
|
53 (54.5) tonnes |
|
116.8 (120.2)
lbs. x 1000 |
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|
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Maximum
fuel capacity |
|
24,210 Litres |
|
6,400 US gal. |
|
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Typical
volumetric payload |
|
11 tonnes |
|
24.25
lbs. x 1000 |
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