| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Scheme | Low wing High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.8
88.7
|
|
| Height (m) |
0.6
3.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
15.7
925
|
|
| Wingspan (Beam) (m) |
0.1
17.4
95
|
|
| Rotors | ||
| Disc loading (kg/m2) |
17.1
73
73
|
|
| Weights | ||
| Empty weight (kg) |
8
4,573.6
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
6,000
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
pilot, copilot |
| Speeds | ||
| Max. Speed (km/h) |
25
557
28,165
|
|
| Сruise Speed (km/h) |
52
371
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
3,100
60,000
|
2 powerplants 1550 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
8,840
161,544
|
|
| Static ceiling (m) |
3
2,635
5,485
|
|
| Range (Ferry range) (km) |
4
824.1
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
960
36,000
|
|
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| Introduction | 1977 | |
| First flight | 03.05.1977 | |
| Stop production | 2003 | |
