F 16 Air Combat Fighter Parts

(Page 14) End item NSN parts page 14 of 58
Part Number
NSN
NIIN
16E3102-845 Battery Charger Control
015008281
16E3156-9 Aircraft Access Cover
013415718
16E3157-895 Power Distribution Panel
013154058
16E3167-843 Distribution Box
012660421
16E3634-809 Power Distribution Panel
012959758
16E3634-811 Power Distribution Panel
012941041
16E3634-813 Power Distribution Panel
012941041
16E3641-819 Electrica Power Control Assembly
013751493
16E3646-1 Electrica Power Control Assembly
012825892
16E3646-805 Electrica Power Control Assembly
014589080
16E3647-805 Electrica Power Control Assembly
013193828
16E3648-805 Electrica Power Control Assembly
013211164
16E3678-115 Aircraft Structural Plate
012930219
16E3701-3 Power Distribution Panel
012832330
16E3701-805 Power Distribution Panel
014353078
16E3701-813 Power Distribution Panel
012832330
16F0157-7 Pilot Armrest Slide
010473458
16F0171-11 Aircraft Fairing
012367778
16F0171-59 Aircraft Fairing
012367778
16F0171-77 Aircraft Fairing
012367778
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F 16 Air Combat Fighter

Picture of F 16 Air Combat Fighter

An air superiority fighter, also spelled air-superiority fighter, is a type of fighter aircraft designed for entering and seizing control of enemy airspace as a means of establishing complete dominance over the enemy's air force (air supremacy). Air superiority fighters are designed primarily to effectively engage enemy fighters, more than other types of aircraft, although some may have a secondary role for air-to-ground strikes. They are usually more expensive and procured in smaller numbers, compared to multirole fighters which are designed with a balance between air-to-air and air-to-ground capabilities.

In order to maximize their combat effectiveness and strategic usefulness, air superiority fighters usually operate under the control/co-ordination of an airborne early warning and control (AEW&C) aircraft.

During World War II and through the Korean War, fighters were classified by their role: heavy fighter, interceptor, escort fighter, night fighter, and so forth. With the development of guided missiles in the 1950s, design diverged between fighters optimized to fight in the beyond visual range (BVR) regime (interceptors), and fighters optimized to fight in the within visual range (WVR) regime (air superiority fighters). In the United States, the influential proponents of BVR developed fighters with no forward-firing gun, such as the original F-4 Phantom II, as it was thought that they would never need to resort to WVR combat. These aircraft would sacrifice high maneuverability, and instead focus on remaining performance characteristics, as they presumably would never engage in a dogfight with enemy fighters.

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