Company | Cessna Aircraft Company | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
6.6
88.7
|
|
Height (m) |
0.6
1.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
14.8
925
|
|
Wing loading (kg/m2) |
3.1
44
829
|
|
Rotors | ||
Rotor number (qt) |
1
1
8
|
|
Weights | ||
Empty weight (kg) |
8
403.7
276,800
|
|
Loaded weight (kg) |
5
657.7
242,500
|
|
Capacity | ||
Crew (per.) |
1
1
112
|
|
Capacity passengers (per.) |
1
1
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
201.2
28,165
|
|
Сruise Speed (km/h) |
52
169.0
3,087
|
|
Stall Speed (km/h) |
40
72.4
257.7
|
flaps down |
Never exceed speed (km/h) |
108.0
225.3
1,050
|
|
Fuel | ||
Fuel Capacity (l) |
23
95
320,000
|
|
Power | ||
Total Power (hp) |
0.4
85
60,000
|
1 powerplant |
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
207.3
36,000
|
|
Propellers | ||
Prop blade number (qt) |
1
2
8
|
|
Stat | ||
Number built (qt) |
0
7,664
43,000
|
|
Price (USD) |
41.5
3,495
750.0 million
|