 |
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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
|
|
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|
|
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|
Overall
length |
|
33.84 m. |
|
111 ft. |
|
|
|
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Height
|
|
11.76 m. |
|
38 ft. 7 in. |
|
|
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|
Fuselage
diameter |
|
3.95 m. |
|
13 ft. |
|
|
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Maximum
cabin width |
|
3.70 m. |
|
12 ft. 1in. |
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|
|
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Cabin
length |
|
23.78 m. |
|
78 ft. |
|
|
|
|
|
Wingspan
(geometric) |
|
34.10 m. |
|
111 ft. 10 in. |
|
|
|
|
|
Wing
area (reference) |
|
122.6 m2 |
|
1,320 ft2 |
|
|
|
|
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Wing
sweep (25% chord) |
|
25 degrees |
|
25 degrees |
|
|
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Wheelbase |
|
11.04 m. |
|
36 ft. 3 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 |
|
|
|
|
|
Typical
passenger seating |
|
124 |
|
124 |
|
|
|
|
|
Range
(w/max. passengers) |
|
3,350 (6,800) km. |
|
1,800 (3,700) nm. |
|
|
|
|
|
Max.
operating Mach number (Mmo) |
|
0.82 Mo. |
|
0.82 Mo. |
|
|
|
|
|
Bulk
hold volume - Standard/option |
|
27.62 m3 |
|
976 ft3 |
|
|
|
|
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| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
|
|
|
|
|
|
|
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|
Maximum
ramp weight |
|
64.4 (75.9) tonnes |
|
142 (167.3)
lbs. x 1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
64 (75.5) tonnes |
|
141.1 (166.5)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
61 (62.5) tonnes |
|
134.5 (137.8)
lbs. x 1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
57 (58.5) tonnes |
|
125.7 (129.0)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
23,860 (29,840) Litres |
|
6,300 (7,885) US gal. |
|
|
|
|
|
Typical
operating weight empty |
|
40.6 tonnes |
|
89.5
lbs. x 1000 |
|
|
|
|
|
Typical
volumetric payload |
|
13.2 tonnes |
|
29.1
lbs. x 1000 |
|
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