C-47 Military Transport

| General characteristics C-47 | |||
| Primary function | Transport | ||
| Contractor | Douglas Aircraft Co. | ||
| Power plant | Two Pratt&Whitney R-1830-92 Twin Wasp 14-cylinder, twin- row radials engines | ||
| Thrust | 2x 1,250 HP | 2x 932 kW | |
| Wingspan | 85.5 ft | 29.11 m | |
| Length | 63.7 ft | 19.43 m | |
| Height | 17 ft | 5.18 m | |
| Wingarea | 987 sq ft | 91.69 sq m | |
| Weight | empty | 18,201 lb | 8,256 kg |
| max. | 26,000 lb | 11,794 kg | |
| Speed | 229 mph | 368 km/h | |
| Ceiling | 23,294 ft | 7,100 m | |
| Range | 1,491 miles | 2,400 km | |
| Freight | 9,920 lb (4,500 kg) or 28 seats. | ||
| Crew | Three | ||
| First flight | December 17, 1935 | ||
| Date deployed | 1941 | ||
| Cost | $138,000 | ||
| Number built | 10,654 incl. civilian models, plus approx 2,500 aircraft license-built in Japan and the Soviet Union (8,882). | ||