Jelaskan Spesifikasi dari AIDC F-CK-1 Ching-kuo

Type: Single-seat, twin-engined interceptor and air defence fighter with a secondary ground attack and anti-shipping function. The two-seater conversion trainer is fully combat capable, albeit with reduced internal fuel.

Engines: Two ITEC TFE1042-70 afterburning turbofans rated at 9,250 lb (4,196 kg) thrust maximum and 6,300 lb (2,858 kg) thrust military.

Dimensions: Span 30 ft 10.25in (9.42m); length 46 ft 7.75in (14.20m); height 15 ft 6in (4.72m); wing area 260sq.ft (24.20m2).

Weights: Empty 14,300 lb (6,486 kg); normal takeoff 21,0000 lb (9,526 kg); maximum takeoff 27,000 lb (12,247 kg).

Loadings (at normal takeoff weight): Wing 81 lb/sq.ft (394 kg/m2); thrust 0.90.

Performance: Maximum speed (altitude) Mach 1.65; maximum speed (sea level) Mach 1.05; operational ceiling 50.000 ft (15,239m); initial climb rate 50,000 ft/min (254m/sec).

Armament: One 20mm M61A1 cannon with 511 rounds in the port wing root; four Sky Sword I heat-homing AAMs plus two Sky Sword II SARH AAMs; two AGM-65 Maverick or three Hsiung Feng II ASMs; or a variety of conventional air-to-surface weaponry. Maximum weight of stores 8,600 lb (3,901 kg).

History: First flight prototype 28 May 1989; production delivery 10 January 1994 to 2000.

User: Republic of China Air Force (Taiwan)