| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
34.2
88.7
|
|
| Height (m) |
0.6
9.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
146.8
925
|
|
| Wingspan (Beam) (m) |
0.1
38.9
95
|
|
| Weights | ||
| Empty weight (kg) |
8
33,004.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
64,863.7
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
5
112
|
2 Pilots, 1 Flight Engineer, 4 Flight attendants |
| Capacity passengers (per.) |
1
105
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
653
28,165
|
|
| Сruise Speed (km/h) |
52
578
3,087
|
|
| Stall Speed (km/h) |
40
156
257.7
|
|
| Power | ||
| Total Power (hp) |
0.4
13,600
60,000
|
4 powerplants 3400 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
8,656.3
161,544
|
|
| Range (Ferry range) (km) |
4
9,012
40,700
|
|
| Stat | ||
| Number built (qt) |
0
343
43,000
|
|
| Introduction | 1953 | |
| First flight | 18.05.1953 | |
