F 16 Air Combat Fighter Parts

(Page 11) End item NSN parts page 11 of 58
Part Number
NSN
NIIN
16E1081 Power Distribution Panel
010553507
16E1081-3 Power Distribution Panel
010553507
16E1081-801 Power Distribution Panel
010553507
16E1081-805 Power Distribution Panel
010553507
16E1081-807 Power Distribution Panel
014587125
16E1082-3 Electric Light Control
010510952
16E1082-801 Electric Light Control
010510952
16E1082-805 Light Transmitt Indicating Panel
011607247
16E1082-807 Light Transmitt Indicating Panel
011607247
16E1083-821 Electrical-electro Control Panel
015228246
16E1131-815 Aircraft Panel Assembly
012886802
16E1132-837 Lefthand Control Panel Assembly
011354597
16E1132-849 Panel Assembly Lighting
014591508
16E1141 Audio Frequency Switching Group
012668685
16E1141-711 Audio Frequency Switching Group
012731911
16E1141-883 Audio Frequency Switching Group
011827291
16E1141-897 Audio Frequency Switching Group
012668685
16E1144-625 Relay Assembly
013125410
16E1144-877 Relay Assembly
010959685
16E1144-881 Relay Assembly
010964276
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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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