|
|
Conversion of one C-119B to meet USAF requirement for an experimental detachable-fuselage transport; C-119B wings and tail surfaces combined with new upper fuselage component with a flat surface; lower component with flat upper surface, and incorporating cargo compartment, could be mated with the Packplane; flight deck in upper component; the type could be flown with or without pack and it was intended that various packs for different military operations would be provided; first flown on 11 August 1950; no production contract followed military evaluation.
| MODEL | XC-120 |
| CREW | 5 |
| PASSENGERS | 66 |
| ENGINE | 2 x Pratt & Whitney R-4360-20, 2435kW |
| DIMENSIONS |
| Wingspan | 33.3 m | 109 ft 3 in |
| Length | 25.3 m | 83 ft 0 in |
| Height | 7.6 m | 24 ft 11 in |
|
Do you have any comments about this aircraft ?
|
| |