| Manufacturer |
Douglas Aircraft Corporation |
Société Aérienne Bordelaise |
| Description |
The Douglas DC-5 (Douglas Commercial Model 5) was a 16-to-22-seat, twin-engine propeller aircraft intended for shorter routes than the Douglas DC-3 or Douglas DC-4. |
The SAB AB-80 was a French bomber built in 1934 by the Société Aérienne Bordelaise (SAB) in Bordeaux. |
| First Flight |
1939-02-20 |
1934-06-23 |
| Entry Into service |
1940-01-01 |
|
| Service End |
1949-01-01 |
|
| Designer |
Donald Douglas |
Société Aérienne Bordelaise |
| Type |
Transport |
|
| Length (m) |
18.8976 |
18.52 |
| Height (m) |
5.7912 |
6.1 |
| Cockpit Crew |
3 |
|
| Max Seating |
24 |
|
| Max Speed (km/h) |
370.1491 |
330 |
| Cruise Speed (km/h) |
313.8221 |
|
| Max Ceiling (m) |
7223.76 |
8000 |
| Rate of Climb (m/s) |
8.0518 |
|
| Armament |
|
maximum load 2500 kg |
| Capacity Description |
16-24 passengers |
|
| National Origin |
|
France |
| Number Built |
12 |
1 |
| Powerplant Description |
2 × Wright GR-1820-G102A Cyclone 9-cylinder air-cooled radial piston engine, 671 kW (900 hp) each |
2 × Hispano-Suiza 12Ybrs V-12 water-cooled piston engine, 641 kW (860 hp) each |
| Primary Users |
KNILM, KLM, United States Navy, United States Marine Corps |
|
| Status |
Retired |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Douglas_DC-5 |
en.wikipedia.org/wiki/SAB_AB-80 |
| Flat Wing Span (m) |
23.7744 |
24 |
| Flat Wing Area (m²) |
76.5521 |
81.75 |
| Flat Wing Aspect Ratio |
|
7 |
| Number of Engines |
2 |
2 |