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ft |
|
m |
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Overall
Length |
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103ft 2in |
|
31,44m |
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Cabin
Length |
|
|
70ft 2in |
|
21,38m |
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|
Fuselage
Diameter |
|
|
13ft 0in |
|
3,96m |
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Max. Cabin
Width |
|
|
12ft 1in |
|
3,70m |
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|
Height |
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41ft 2in |
|
12,76m |
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Wheelbase |
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33ft 10in |
|
10,25m |
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Track |
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|
24ft 1in |
|
7,59m |
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ft |
|
m |
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Wing Span
(geometric) |
|
|
111ft 8in |
|
34,09m |
|
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Wing Area
(reference) |
|
|
1320ft2 |
|
122,6m2 |
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Sweep (25%
chord) |
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|
25
degrees |
|
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lb
X 1000 |
|
tonnes |
|
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Max. Ramp
Weight |
|
|
131,0 (150,8) |
|
59,4 (68,4) |
|
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Max.
Take-off Weight |
|
|
130,1 (149,9) |
|
59,0 (68,0) |
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Max.
Landing Weight |
|
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123,5 (132,3) |
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56,0 (60,0) |
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Max. Zero
fuel Weight |
|
|
116,8 (122,4) |
|
53,0 (55,5) |
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|
Max. fuel
Capacity |
|
|
6
300 USg 23 860 Litres |
|
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Typical
operating Weight Empty |
|
|
84,6 |
|
38,4 |
|
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Typical
Volumetric Payload |
|
|
25,2 |
|
11,4 |
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Powerplants |
|
|
two CFM56-5 or PW 6000 |
|
|
|
Thrust
Range |
|
|
21
600-23 800 lb slst |
|
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Typical
Seating (two class) |
|
|
107 |
|
|
|
Range (max.
pax) |
|
|
1
500 (3 250)nm 3 250 (6 000)km
|
|
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Max.
Operating Mach n° (Mmo) |
|
|
0,82Mo |
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Bulk Hold
Volume - Standard/Option |
|
|
749ft3 21,21m3 |
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| |
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