![]() ![]() The F-5N/Fs are third-generation F-5 fighter aircraft designed for replacement of the F-5A/B/E production models. ![]() In December 1970, Northrop Grumman began development and production on the F-5A-21, an aircraft design that emphasized maneuverability rather than high speed and was officially reclassified as the F-5E. ![]() lightweight fighter, but became extremely popular as an export finding its niche in the overseas market. The F-5 also has anti-skid brakes, initial navigation system (INS), ALR-87 Radar Warning Receivers (RWR), AN/APQ-159 radar and ALE-40 chaff/flare capability.īackground The F-5 was developed by Northrop Grumman for export through the Military Assistance Program (MAP) in February 1965.This aircraft was initially offered as a candidate for a U.S. Full-span leading-edge flaps work in conjunction with trailing-edge flaps and are operated by a control on the pilot's throttle quadrant. ![]() The design places particular emphasis on maneuverability rather than high speed, notably by the incorporation of maneuvering flaps. This aircraft has an upward opening canopy, which is hinged at the rear. The aircraft serves in an aggressor-training role with simulation capability of current threat aircraft in fighter combat mode.Īs a tactical fighter aircraft, the F-5N accommodates a pilot only in a pressurized, heated and air conditioned cockpit and rocket-powered ejection seat while the F-5F is a two-seat combat- capable fighter. The F-5F is a dual-seat version, twin-engine, tactical fighter commonly used for training and adversary combat tactics. The F-5N is a single seat, twin-engine, tactical fighter and attack aircraft providing simulated air-to-air combat training manufactured by Northrop Grumman Corporation. ![]()
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