This was the original production single-seat version. First flight of production aircraft occurred on Aug. 7, 1978. It was fitted with the Northrop Grumman APG-66 radar; Sidewinder air-to-air missile; Pratt & Whitney F100-PW-200 engine; and a triplex flight control system. Tip rails and outer wing pylons had a 250-lb (113-kg) capacity; middle pylons had a 2,500-lb (1,134 kg) capacity; and the inner pylons, 3,500-lb (1,588-kg) capacity. The fuselage hardpoint was...
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