F 16 Air Combat Fighter Parts

(Page 35) End item NSN parts page 35 of 58
Part Number
NSN
NIIN
178-6126-3 Cable Assembly
015213205
18-1500 Manual Control Lever
011653559
18-5900-1 Quick Disconnect Coupling Half
010837426
183079-1 Thrust Washer Bearing
012695306
183079-12 Thrust Washer Bearing
012695308
183079-13 Thrust Washer Bearing
012695309
183101-2 Special Shaped Spacer
012811031
183103-1 Mounting Bracket
012694940
183220-1 Aircraft Gearbox Assembly
012649870
183315-1 Aircraft Gearbox Assembly
014506898
184-16 Band Pass Filter
010802707
18730/AF16KE-3 Electrical Special Purpose Cable
010854609
18730/AF16KK4 Electrical Special Purpose Cable
010866897
18730/F16KE-3 Electrical Special Purpose Cable
010854609
18730/F16KK4 Electrical Special Purpose Cable
010866897
1881165 Instrument Mounting Bezel
013556184
1881165-920 Instrument Mounting Bezel
013556184
19743-001 Indicator Light Assembly
012480953
19P3103-7 Air Structural Component Support
012034579
2-33SCYX-1 Aircraf Electrostatic Discharger
014348504
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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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