| Type | Helicopter | |
| Company | Fairchild Aircraft | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.5
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Rotors | ||
| Main rotor diameter (m) |
1.2
10.8
62
|
|
| Tail rotor diameter (m) |
0.8
1.8
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
621.4
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,247.4
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Payload (kg) |
23
390.1
122,470
|
|
| Capacity passengers (per.) |
1
4
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
204
28,165
|
|
| Сruise Speed (km/h) |
52
196
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
260
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
316.4
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,328.2
161,544
|
|
| Static ceiling (m) |
3
4,990
5,485
|
|
| Range (Ferry range) (km) |
4
560
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
487.7
36,000
|
|
| Stat | ||
| Number built (qt) |
0
253
43,000
|
|
| Introduction | 1963 | |
| First flight | 21.01.1963 | |
