F 16 Air Combat Fighter Parts

(Page 52) End item NSN parts page 52 of 58
Part Number
NSN
NIIN
584R046H02 Semiconductor Device Assembly
010832745
584R070H03 Directional Coupler
011601083
584R206H01 Quartz Crystal Unit
010792557
584R206H09 Quartz Crystal Unit
010792559
584R395H01 Ceramic Dielectr Fixed Capacitor
010810759
584R457H01 Ceramic Dielectr Fixed Capacitor
010803789
584R619H03 Radio Frequency Cable Assembly
011174474
585R100H01 Rotary Pump Unit
011541521
585R100H02 Rotary Pump Unit
011541521
585R100H03 Rotary Pump Unit
011541521
585R237H01 Electrical Power Cable Assembly
011544090
585R651H01 Air Duct Hose
011548775
585R911G01 Torque Motor
011548955
585R912G01 Torque Motor
011548956
585R951H01 Pressure Switch
011569911
586R533H01 Electrical Power Cable Assembly
011544090
586R815H01 Aircraft Ground Servicing Cover
011230095
586R825H01 Identification Plate
012518284
588R318H01 Power Supply
013444471
5902511 Sleeve Bushing
011034809
Page: 52

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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