| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.8
88.7
|
|
| Height (m) |
0.6
4.1
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
34.7
925
|
|
| Wingspan (Beam) (m) |
0.1
13.7
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,244.0
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
8,618.3
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
538
28,165
|
at 4900 m |
| Сruise Speed (km/h) |
52
465
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
2,300
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
7,193.3
161,544
|
|
| Range (Ferry range) (km) |
4
2,382
40,700
|
|
| Combat | ||
| Guns (qt) |
1
2
18
|
20 mm AN/M2 (.79 in) cannons |
| Torpedoes (qt) |
1
2
4
|
883.1 kg of torpedoes or |
| Bombs weight (kg) |
2
1,450
39,000
|
of bombs in the bomb bay |
| Stat | ||
| Number built (qt) |
0
30
43,000
|
|
| Introduction | 1943 | |
| First flight | 08.04.1943 | |
| Stop production | 1945 | |
