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| AIRCRAFT
DIMENSIONS |
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|
metric |
 |
imperial |
|
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|
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|
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|
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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 |
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3.95 m. |
 |
13 ft. |
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 |
 |
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Maximum
cabin width |
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3.70 m. |
 |
12 ft. 1 in. |
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 |
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Cabin
length |
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21.38 m. |
 |
70 ft. 2 in. |
|
 |
 |
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Wingspan
(geometric) |
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34.10 m. |
 |
111 ft. 10 in. |
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 |
 |
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Wing
area (reference) |
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122 m2 |
 |
1,320 ft |
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 |
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Wing
sweep (25% chord) |
 |
25 degrees |
 |
25 degrees |
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 |
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Wheelbase |
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10.25 m. |
 |
33 ft. 8 in. |
|
 |
 |
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Wheel
track |
 |
7.59 m. |
 |
24 ft. 11 in. |
|
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|
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|
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| BASIC
OPERATING DATA |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
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|
Engines |
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two CFM56-5
or PW 6000A |
 |
two CFM56-5
or PW 6000A |
|
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|
Engine
thrust range |
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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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|
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|
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| DESIGN
WEIGHTS |
|
|
metric |
 |
imperial |
|
 |
|
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|
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|
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|
Maximum
ramp weight |
 |
59.4 (68.4) tonnes |
 |
131 (150.8) lbs. x 1000 |
|
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 |
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|
Maximum
takeoff weight |
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59 (68) tonnes |
 |
130.1 (149.9)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
landing weight |
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56 (57.5) tonnes |
 |
123.5 (126.8)
lbs. x 1000 |
|
 |
 |
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|
Maximum
zero fuel weight |
 |
53 (54.5) tonnes |
 |
116.8 (120.2)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
fuel capacity |
 |
24,210 Litres |
 |
6,400 US gal. |
|
 |
 |
 |
|
Typical
volumetric payload |
 |
11 tonnes |
 |
24.25
lbs. x 1000 |
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|
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