Type | Aircraft | |
Company | Grumman Aerospace Corporation | |
Scheme | Monoplane High wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
17.3
88.7
|
|
Height (m) |
0.6
4.9
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
65.0
925
|
|
Wingspan (Beam) (m) |
0.1
24.6
95
|
|
Wing loading (kg/m2) |
3.1
378.9
829
|
|
Weights | ||
Empty weight (kg) |
8
15,306.9
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
27,215.5
575,000
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
2 pilots, 2 aircrew |
Useful load (kg) |
26.4
9,350
90,700
|
|
Payload (kg) |
23
4,535.9
122,470
|
|
Capacity passengers (per.) |
1
26
400
|
26 passengers, 12 litter patients |
Speeds | ||
Max. Speed (km/h) |
25
635
28,165
|
at 3660 m |
Сruise Speed (km/h) |
52
465
3,087
|
at 8750 m |
Stall Speed (km/h) |
40
152
257.7
|
at idle power |
Fuel | ||
Fuel Capacity (l) |
23
12,424
320,000
|
6905 l + optional 5519 l |
Power | ||
Total Power (hp) |
0.4
9,200
60,000
|
2 powerplants 4600 hp |
Performance | ||
Service ceiling (m) |
0.6
10,210.8
161,544
|
|
Range (Ferry range) (km) |
4
2,407.6
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
1,127.8
36,000
|
|
Stat | ||
Number built (qt) |
0
58
43,000
|
|
Price (USD) |
41.5
39.0 million
750.0 million
|
|
Introduction | 1964 | |
First flight | 18.11.1964 | |
Stop production | 1987 |