F 16 Air Combat Fighter Parts

(Page 31) End item NSN parts page 31 of 58
Part Number
NSN
NIIN
16W102-40 Aircraft Skin
012469053
16W1262-21 Air Structural Component Fitting
013181757
16W154-15 Air Structural Component Fitting
010422078
16W158-4 Fitting Hinge
012215362
16W167-802 Flaperon Fitting Assembly
010761624
16W167-805 Flaperon Fitting Assembly
010761624
16W167-806 Flaperon Fitting Assembly
010759680
16W169-5 Air Structural Component Fitting
010753596
16W172-15 Plate Spacer
010460467
16W172-37 Plate Spacer
010460467
16W176-24 Aircraft Structural Plate
013337314
16W177-5 Aircraft Access Cover
013151303
16W177-807 Aircraft Access Cover
013392134
16W177-809 Aircraft Access Cover
013392133
16W177-811 Aircraft Access Cover
013392131
16W252-10 Connector And Throttle Door
010480257
16W254-7 Air Structural Component Fitting
010422078
16W254-9 Air Structural Component Fitting
012689629
16W262-10 Air Structural Component Support
012170152
16W262-16 Air Structural Component Support
012170152
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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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