| Company | Cessna Aircraft Company | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.6
88.7
|
|
| Height (m) |
0.6
2.0
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
16.2
925
|
|
| Aspect ratio |
1.7
7.5
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
546.6
276,800
|
|
| Loaded weight (kg) |
5
997.9
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
3
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
225.3
28,165
|
|
| Сruise Speed (km/h) |
52
193.1
3,087
|
|
| Stall Speed (km/h) |
40
83.7
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
159.0
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
145
60,000
|
1 powerplant |
| Performance | ||
| Endurance (h) |
0.0
4.5
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
210.3
36,000
|
|
| Stat | ||
| Number built (qt) |
0
5,174
43,000
|
|
| First flight | 01.06.1948 | |
