| Type | Aircraft | |
| Company | North American Aviation | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
21.4
88.7
|
|
| Height (m) |
0.6
7.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
77.8
925
|
|
| Wingspan (Beam) (m) |
0.1
21.8
95
|
|
| Wing loading (kg/m2) |
3.1
274
829
|
|
| Weights | ||
| Empty weight (kg) |
8
16,034.5
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
27,759.9
575,000
|
|
| Loaded weight (kg) |
5
21,269
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
726
28,165
|
|
| Сruise Speed (km/h) |
52
640
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
9,961
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
10,070
60,000
|
2 powerplants 5035 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
11,430
161,544
|
|
| Range (Ferry range) (km) |
4
3,508
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
2,078.7
36,000
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
20 mm cannons in tail (never fitted) |
| Bombs weight (kg) |
2
4,763
39,000
|
|
| Stat | ||
| Introduction | 1952 | |
| First flight | 04.01.1952 | |
