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The I-350 prototype of the MiG-19 first flew in September 1953. The initial production day fighter began to enter service with the Soviet air defence force in early 1955, but before long an all-moving tailplane replaced the elevators of early production aircraft. At the same time three 30mm guns replaced the original armament of a 37mm and two 23mm cannon, which had been standard on all MiG jets from the earliest MiG-9; and an attachment was added under each wing for a bomb or an air-to-surface rocket. This new version was designated MiG-19S (for Stabilisator). With the adoption in 1957 of the Tumansky R-9 axial-flow turbojet as the standard engine, the MiG-19SF was produced. At the same time another version appeared with limited all-weather capability as the MiG-19PF, supporting a small Izumrud radar scanner inside its engine air intake and a ranging unit in the intake lip. The later MiG-19PM differed from the PF in having four first-generation Alkali radar-homing missiles instead of guns.
In the Soviet Union the MiG-19 was phased out of production by the end of the 1950s, making way for expanded MiG-21 production. However in 1958 a licence to build the MiG-19 had been agreed with China but, following delivery of knocked-down MiGs for Chinese construction, relations between the two countries deteriorated. Nevertheless the MiG-19 construction went ahead under the Chinese designation F-6 (MiG-19S), the first of which flew in December 1961. F-6 became the standard equipment of the Chinese Air Force of the People's Liberation Army from mid-1962.
Production of the F-6 was stepped up from about 1966 and it is thought that several thousand have been built, including counterparts of the MiG-19PF and SF. China has developed a number of variants of its own design. One is a tactical reconnaissance aircraft, while the TF-6 is a trainer version and the A-5 (formerly referred to as the F-9 and F-6 bis) a strike fighter with different appearance because of its pointed nose radome between the semi-circular side air intakes. The span of the A-5 has also been increased to about 10.2m. Maximum level speed of this version is estimated to be close to Mach 2.
| CREW | 1 |
| ENGINE | 2 x turbo-jet RD-9B(N), 31.9kN |
| WEIGHTS |
| Take-off weight | 8600 kg | 18960 lb |
| DIMENSIONS |
| Wingspan | 9.0 m | 30 ft 6 in |
| Length | 12.5 m | 41 ft 0 in |
| Height | 4.1 m | 13 ft 5 in |
| Wing area | 23.0 m2 | 247.57 sq ft |
| PERFORMANCE |
| Max. speed | 1450 km/h | 901 mph |
| Ceiling | 18600 m | 61000 ft |
| Range w/max.fuel | 2200 km | 1367 miles |
| Range w/max.payload | 1400 km | 870 miles |
| ARMAMENT | 3 x 30mm machine-guns, missiles |
| Bob Lawler, dlawler(@)stny.rr.com, 19.02.2010 This aircraft had engine overheating problems while on the ground. Aircraft were positioned near the ends of runways so that taxi-to-takeoff times were at a minimum. Takeoffs were usually within 5 minutes of engine start. | | Ed, renoed_789(@)hotmail.com, 15.05.2008 Do you have any photos of them the North Vietnmese marking or other Airforces | | Sodad Nima, sodadnima(@)hotmail.com, 25.09.2007 I love this baby because my father use ti fly it, the 21 and the 23. I'd like to have some high resolution photos of them if possible. thank you |
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