Kawasaki C-1
Military Transport Aircraft
The Kawasaki C-1 is a twin-engined short-to medium-range military transport aircraft produced by the Japanese manufacturer Kawasaki Heavy Industries, operated by the Japan Air Self-Defense Force (JASDF).
| Propulsion | 2 Turbofan Engines |
| Engine Model | Pratt & Whitney (Mitsubishi) JT8D-M-9 |
| Engine Power (each) | 64,5 kN | 14500 lbf |
| Speed | 435 km/h | 235 kts
270 mph |
| Service Ceiling | 11.582 m | 38.000 ft |
| Range | 1.300 km | 702 NM
808 mi. |
| Empty Weight | 23.320 kg | 51.412 lbs |
| max. Takeoff Weight | 45.000 kg | 99.208 lbs |
| Wing Span | 30,60 m | 100 ft 5 in |
| Wing Area | 120,5 m² | 1297 ft² |
| Length | 29,00 m | 95 ft 2 in |
| Height | 10,00 m | 32 ft 10 in |
| First Flight | 12.11.1970 |
| Production Status | out of production |
| Total Production | 31 |
| ICAO Code | C1 |
| Data for (Version) | Kawasaki C-1 |
| Variants | Kawasaki C-1, C-1A |
