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 |
