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| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
 |
|
Overall
length |
 |
44.51 m. |
 |
146 ft. |
|
 |
 |
 |
|
Height
|
 |
11.76 m. |
 |
38 ft. 7 in. |
|
 |
 |
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|
Fuselage
diameter |
 |
3.95 m. |
 |
13 ft. |
|
 |
 |
 |
|
Maximum
cabin width |
 |
3.70 m. |
 |
12 ft. 1 in. |
|
 |
 |
 |
|
Cabin
length |
 |
34.44 m. |
 |
113 ft. |
|
 |
 |
 |
|
Wingspan
(geometric) |
 |
34.10 m. |
 |
111 ft. 10 in. |
|
 |
 |
 |
|
Wing
area (reference) |
 |
122 m2 |
 |
1,320 ft |
|
 |
 |
 |
|
Wing
sweep (25% chord) |
 |
25 degrees |
 |
25 degrees |
|
 |
 |
 |
|
Wheelbase |
 |
16.91 m. |
 |
55 ft. 48 in. |
|
 |
 |
 |
|
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 |
 |
120 (148) kN |
 |
27,000 (33,000)
lb. slst |
|
 |
 |
 |
|
Typical
passenger seating |
 |
185 |
 |
185 |
|
 |
 |
 |
|
Range
(w/max. passengers) |
 |
5,500 km. |
 |
3,000 nm. |
|
 |
 |
 |
|
Max.
operating Mach number (Mmo) |
 |
0.82 Mo. |
 |
0.82 Mo. |
|
 |
 |
 |
|
Bulk
hold volume - Standard/option |
 |
51.76 m3 |
 |
1,829 ft3 |
|
 |
|
 |
|
 |
|
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| DESIGN
WEIGHTS |
|
|
metric |
 |
imperial |
|
 |
|
 |
|
 |
|
 |
|
Maximum
ramp weight |
 |
83.4 (93.9) tonnes |
 |
183.9 (207)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
takeoff weight |
 |
89 (93.5) tonnes |
 |
196.2 (206.1)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
landing weight |
 |
75.5 (77.8) tonnes |
 |
166.4 (171.5)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
zero fuel weight |
 |
71.5 (73.8) tonnes |
 |
157.6 (162.7)
lbs. x 1000 |
|
 |
 |
 |
|
Maximum
fuel capacity |
 |
24,050 (30,030) Litres |
 |
6,350 (7,930) US gal. |
|
 |
 |
 |
|
Typical
volumetric payload |
 |
21.2 tonnes |
 |
46.74
lbs. x 1000 |
|
 |
|
 |
|
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|
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