Cessna C-106 Loadmaster
|The P260 demonstrator|
|Role||Military transport monoplane|
|National origin||United States|
The C-106 Loadmaster was a twin-engined high-wing cantilever monoplane with a retractable tailwheel landing gear. It was powered by two 600 hp Pratt & Whitney R-1340 engines. Two company owned P260 demonstrators were built and given the military designation C-106 Loadmaster. An order for 500 was cancelled due to a shortage of plywood.
- Military designation for company owned P260 prototype with two R-1340-S3H1 engines.
- Military designation for company owned P260 prototype with two R-1340-AN-2 engines.
Data from 
- Crew: 4
- Capacity: 2,440 lb
- Length: 51 ft 1 in (15.57 m)
- Wingspan: 64 ft 8 in (19.71 m)
- Empty weight: 9,800 lb (4,445 kg)
- Gross weight: 14,800 lb (6,713 kg)
- Powerplant: 2 × Pratt & Whitney R-1340 air-cooled radial piston engine, 600 hp (450 kW) each
- Maximum speed: 195 mph (314 km/h, 169 kn)
|Wikimedia Commons has media related to Cessna C-106 Loadmaster.|
- Andrade 1979, p. 84
- "American airplanes - Cessna". www.aerofiles.com. 4 April 2009. Retrieved 2009-12-29.
- American Military Transport Aircraft Since 1925: E.R. Johnson, Lloyd S. Jones, p.172
- Note: Aerofile has two Pratt & Whitney R-1830 being used.