| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.9
88.7
|
|
| Height (m) |
0.6
4.9
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
21.2
95
|
|
| Weights | ||
| Empty weight (kg) |
8
8,504.9
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
13,222.2
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
462
28,165
|
|
| Power | ||
| Total Power (hp) |
0.4
3,050
60,000
|
2 powerplants 1525 hp each |
| Performance | ||
| Range (Ferry range) (km) |
4
2,092
40,700
|
|
| Stat | ||
| Number built (qt) |
0
83
43,000
|
|
| First flight | 04.12.1952 | |
| Stop production | 1988 | |
