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| The F-16 evolved from a 1972 USAF Lightweight Fighter (LWF) prototype program, which sought a small, lightweight, low cost, air superiority day fighter designed for high performance and ease of maintenance. The YF-16 was selected the winner, over the Northrop YF-17, after the LWF fly-off competition was completed. The basic YF-17 design was used as the basis for the US Navy F-18.
The F-16 achieved combat-ready status in October 1980. Many foreign nations, including Belgium, Denmark, Turkey, Egypt and Israel, have purchased the F-16. SPECIFICATIONS (F16A Block 15): Span: 32 ft. 10 in. Length: 49 ft. 6 in. Height: 16 ft. 6 in. Weight: 29,896 lbs. loaded Armament: One 20mm M-61A1 cannon and various combinations of air-to-air and air-to-ground missiles and bombs Engine: One Pratt & Whitney F100-PW-200 of 23,830 lbs. thrust with afterburner Crew: One Cost: $8,200,000 Serial number: 81-0663 PERFORMANCE (F16A Block 15): Maximum speed: 1,345 mph Cruising speed: 577 mph Range: 1,407 miles Service ceiling: 55,000 ft. |
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| Bibliography: National Museum of the USAF |
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| US Military Tour | ||