| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
17.0
88.7
|
|
| Height (m) |
0.6
5.0
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
41.8
925
|
swept |
|
1.1
43.4
925
|
spread | |
| Wingspan (Beam) (m) |
0.1
11.2
95
|
swept |
|
0.1
15.4
95
|
spread | |
| Weights | ||
| Empty weight (kg) |
8
9,264.6
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
16,079.9
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,100
28,165
|
|
| Сruise Speed (km/h) |
52
1,017
3,087
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.2
2.1
|
|
| Thrust (kN) |
1.5
30.2
1,914
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
13,960
161,544
|
|
| Range (Ferry range) (km) |
4
2,670
40,700
|
|
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1952 | |
| First flight | 19.05.1952 | |
