F 16 Air Combat Fighter Parts

(Page 54) End item NSN parts page 54 of 58
Part Number
NSN
NIIN
6011094-002 Audio Frequency Amplifier
010982822
6011195-001 Power Supply
010900631
6012301-001 Counter Universal Timer
014086026
601825-00 Cable Assembly
011435277
602584-1 Electrical Connector Inserter
014764083
606BOPT28,93,95 MOD ZA Coordinate Data Monitor
011997586
606BOPT28MODZA Coordinate Data Monitor
011997586
60840 Safety Relief Valve
010592297
61078-4 Manual Control Lever
011653559
615860 AND HDC58 Ground Rod
001875292
624-1 Test Unit
011195290
627146-1 Temperature Cabin And S Selector
004338833
627146-1-1 Temperature Cabin And S Selector
004338833
641-105-42 Amplifier-power Supply Subassemb
010779265
641-105-45 Amplifier-power Supply Subassemb
010779265
646R652G02 Terminal Board
010879703
64M1011-3 Coupling Cover Insulating
010500017
65-0908-1 Indicator Light Assembly
010718437
65-0908-3 Indicator Light Assembly
010718437
65-0908-5 Indicator Light Assembly
010718437
Page: 54

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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