| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
19.4
88.7
|
|
| Height (m) |
0.6
6.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
56.7
925
|
|
| Wingspan (Beam) (m) |
0.1
23.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
9,933.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
15,921.1
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Capacity passengers (per.) |
1
24
400
|
10–24 passengers |
| Speeds | ||
| Max. Speed (km/h) |
25
590
28,165
|
|
| Сruise Speed (km/h) |
52
560.1
3,087
|
max cruise, at 7600 m |
| Fuel | ||
| Fuel Capacity (l) |
23
5,867
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
4,380
60,000
|
2 powerplants 2190 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
10,241
161,544
|
|
| Range (Ferry range) (km) |
4
4,088
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
582
36,000
|
|
| Stat | ||
| Number built (qt) |
0
200
43,000
|
|
| Introduction | 1958 | |
| First flight | 14.08.1958 | |
