| Type | Aircraft | |
| Company | Grumman Aerospace Corporation | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
5.9
88.7
|
|
| Height (m) |
0.6
2.1
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
9.1
925
|
|
| Wingspan (Beam) (m) |
0.1
7.5
95
|
|
| Wing loading (kg/m2) |
3.1
72.8
829
|
|
| Weights | ||
| Empty weight (kg) |
8
461.8
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
680.4
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
1
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
222
28,165
|
|
| Сruise Speed (km/h) |
52
208
3,087
|
|
| Stall Speed (km/h) |
40
97
257.7
|
|
| Power | ||
| Total Power (hp) |
0.4
108
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,191
161,544
|
|
| Range (Ferry range) (km) |
4
785
40,700
|
at 2438 m |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
233.2
36,000
|
|
| Stat | ||
| Number built (qt) |
0
680
43,000
|
680 AA-1Bs were produced by Grumman American |
| Price (USD) |
41.5
6,495
750.0 million
|
|
| Introduction | 1963 | |
| First flight | 1963 | |
