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| Kawasaki C-1 Avião japones de transporte . |
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| FS2002 | |
| JRLucariny FSDS V1 Model | |
| Download | |
| 2002/2003 | |
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C-1 FAB The Kawasaki C-1 was designed to replace the C-46. The first prototype flew on November 12, 1970. The second prototype flew on January 16, 1971. The first pre-production aircarft flew in 1972. The second pre-production aircraft flew in 1974. The first production C-1A (number 48-1008) flew in December 1974. By 1981, a total of 31 C-1A had been delivered. |
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The C-1KA, featuring a redesigned nose, upgraded avionics, first flew in 1985. JASDF also has longstanding requirements for new transports to replace 30-year-old Kawasaki C-1s. The indigenous C-1s is likely to be replaced by a Japanese developed aircraft. |
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Country of Origin: Japan Builder: Kawasaki Wing Span: 100.4 ft Length: 95.1 ft Height: 32.8 ft |
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Weight: 52258 lb empty 85113 lb max takeoff Engine: 2 Pratt & Whitney JT80D-M-9A,64.5 kN of thrust each Maximum speed: 506 miles/hour |
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Range: 1307 miles - maximum515 miles - maximum payload |
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Capacity: 60 troops or 45 paratroopers or 36 stretchers or 11,900 kg of cargo |
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Crew: 5 |
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JRLucariny Kawasaki C-1 FAB Model |
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Kawasaki C-1 Country of Origin: Japan Builder: KAWAZAKI |
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FS2002 FSDS V1 JRLucariny Model |
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Wing Span: 100.4 ft |
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Length: 95.1 ft
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Height: 32.8 ft |
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Weight: 52258 lb empty - 85113 lb max takeoff |
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Engine: 2 Pratt & Whitney JT80D-M-9A,64.5 kN of thrust each |
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Maximum speed: 506 miles/hour |
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JRLucariny Kawasaki C-1 Japonese Air Self-Defence Force Model |
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