AIDC F-CK-1 Ching-Kuo
Fighter
The AIDC F-CK-1 Ching-Kuo is a twin-engined one- or two-seat fight jet aircraft produced by AIDC, Aerospace Industrial Development Corporation of the Republic of China (Taiwan). The F-CK-1 is exclusively operated by the Republic of China Air Force.
Propulsion | 2 Turbofan Engines |
Engine Model | Honeywell / ITEC F125-GA-100 (TFE1042-70) |
Engine Power (each) | 42,0 kN | 9450 lbf |
Speed | 1276 km/h | 689 kts 793 mph |
Service Ceiling | 16.800 m | 55.118 ft |
Range | 1.100 km | 594 NM 684 mi. |
Empty Weight | 6.486 kg | 14.300 lbs |
max. Takeoff Weight | 12.247 kg | 27.000 lbs |
Wing Span | 9,46 m | 31 ft 0 in |
Wing Area | 24,2 m² | 260 ft² |
Length | 14,21 m | 46 ft 7 in |
Height | 9,46 m | 31 ft 0 in |
First Flight | 1989 |
Production Status | out of production |
Total Production | 130 |
ICAO Code | CKUO |
Data for (Version) | AIDC F-CK-1 |