F 16 Air Combat Fighter Parts

(Page 17) End item NSN parts page 17 of 58
Part Number
NSN
NIIN
16H1703-13 Aircraft Hydraulic Swivel Joint
010446163
16H1703-15 Hydraulic Landing G Swivel Joint
010446162
16H1717-801 Aircraft Hydraulic Swivel Joint
010465583
16H1717-807 Landing Gear Hydraulic Swivel
010533668
16H1717-811 Aircraft Hydraulic Swivel Joint
010894455
16H1717-813 Aircraft Hydraulic Swivel Joint
012995982
16H17177-807 Landing Gear Hydraulic Swivel
010533668
16H1902-86 Metal Tube Assembly
012229583
16H1902-87 Metal Tube Assembly
012264188
16H2507-13 Loop Clamp
010909198
16H2511-15 Nonmetallic Hose Assembly
010433244
16H2511-47 Nonmetallic Hose Assembly
010433244
16H2521-27 Hose Assembly
010455914
16H2521-51 Hose Assembly
010455914
16H302-4 Metal Tube Assembly
011133433
16H302-49 Metal Tube Assembly
012176800
16H303-11 Hydraulic System Access Manifold
010423962
16H303-9 Hydraulic System Access Manifold
010423962
16H305-9 Hydraulic System Access Manifold
010423958
16H607-11 Hydraulic System Access Manifold
010423960
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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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