F 16 Air Combat Fighter Parts

(Page 29) End item NSN parts page 29 of 58
Part Number
NSN
NIIN
16VK053-1 Dry Pressure Seal
013512122
16VK054-1 Dry Pressure Seal
013512120
16VM003006-4 Line Electro-mechanical Actuator
011689396
16VM005001-3 Aircraft Gearbox Assembly
012649870
16VM005001-4 Aircraft Gearbox Assembly
014506898
16VP002-2 Valve
010481792
16VP030-1 Pressure Switch
010478916
16VP031-6 Quick Disconnect Coupling Half
010837426
16VP038-1 Safety Relief Valve
010592297
16VP0384 Safety Relief Valve
010592297
16VP039-1 Liquid Level Switch
010981146
16VP041-7 Quick Disconnect Coupling Half
010837426
16VP100-23 Motor Delay Valve Assembly
010605926
16VP110002-310 Fire Detector Sy Sensing Element
015182473
16VP110005-3 Overheat Detectio Cable Assembly
010600203
16VP110005-4 Overheat Detectio Cable Assembly
010600204
16VP122-1 Heater Engine Inlet Duct Strut
010996738
16VP126-1 Ice Detector
013593208
16VP126-4 Ice Detector
013593208
16VP128 Tube Fitting Brazing Ferrule
012187746
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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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