F 16 Air Combat Fighter Parts

(Page 43) End item NSN parts page 43 of 58
Part Number
NSN
NIIN
2715D Plate Insulator
010749126
2740016-2 Aircraft Gearbox Assembly
013431467
2740016-2-1 Aircraft Gearbox Assembly
014506898
2770211-101 Quick Disconnect Coupling Half
010837426
2770211-102 Quick Disconnect Coupling Half
010837426
2775306-101 Valve Seat
011404308
27799-1 Sleeve Bushing
014798445
280-30001-66 Sectiona Terminal Junction Block
010597999
280-30001-9 Sectiona Terminal Junction Block
010672775
2820123-103 Manual Control Lever
011653559
2830157-101 Safety Relief Valve
010592297
2830157-102 Safety Relief Valve
010592297
2846 Power Supply
010788284
2890W12G728 Support Cup Assembly
011650218
28964-1/01 KIT ASSY Sleeve Bushing
014798445
2926-0155 Hub And Pin Assembly
011317216
293-T1909K-3 Electrical Plug Connector
010598038
29416-1 Electrical-electronic Heat Sink
010666015
29416-1A Electrical-electronic Heat Sink
010666015
29416-A Electrical-electronic Heat Sink
010666015
Page: 43 ...

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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