 |
|
| AIRCRAFT
DIMENSIONS |
|
|
metric |
 |
imperial |
|
|
|
|
|
|
|
|
|
Overall
length |
|
44.51 m. |
|
146 ft. |
|
|
|
|
|
Height
|
|
11.76 m. |
|
38 ft. 7 in. |
|
|
|
|
|
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) |
|
122.6 m2 |
|
1,320 ft2 |
|
|
|
|
|
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. |
|
|
|
|
|
|
|
|
| BASIC
OPERATING DATA |
|
|
metric |
|
imperial |
|
|
|
|
|
|
|
|
|
Engines |
|
two CFM56-5
or IAE V2500 |
|
two CFM56-5
or IAE V2500 |
|
|
|
|
|
Engine
thrust range |
|
133 (138) (147) kN |
|
27,000 (33,000)
lb. slst |
|
|
|
|
|
Typical
passenger seating |
|
185 |
|
185 |
|
|
|
|
|
Range
(w/max. passengers) |
|
4,400 (5,600) km. |
|
2,350 (3,050) nm. |
|
|
|
|
|
Max.
operating Mach number (Mmo) |
|
0.82 Mo. |
|
0.82 Mo. |
|
|
|
|
|
Bulk
hold volume - Standard/option |
|
51.76 m3 |
|
1,829 ft3 |
|
|
|
|
|
|
|
|
| DESIGN
WEIGHTS |
|
|
metric |
|
imperial |
|
|
|
|
|
|
|
|
|
Maximum
ramp weight |
|
83.4 (93.9) tonnes |
|
183.9 (207)
lbs. x 1000 |
|
|
|
|
|
Maximum
takeoff weight |
|
83 (93.5) tonnes |
|
183 (206.1)
lbs. x 1000 |
|
|
|
|
|
Maximum
landing weight |
|
71.5 (77.8) tonnes |
|
166.5 (171.5)
lbs. x 1000 |
|
|
|
|
|
Maximum
zero fuel weight |
|
67.2 (73.8) tonnes |
|
157.6 (162.7)
lbs. x 1000 |
|
|
|
|
|
Maximum
fuel capacity |
|
23,700 (29,680) Litres |
|
6,260 (6,850) US gal. |
|
|
|
|
|
Typical
operating weight empty |
|
48.2 tonnes |
|
106.3
lbs. x 1000 |
|
|
|
|
|
Typical
volumetric payload |
|
21.2 tonnes |
|
46.74
lbs. x 1000 |
|
|
|
|
|
|
|
|
|
|
|
|
