F 16 Air Combat Fighter Parts

(Page 47) End item NSN parts page 47 of 58
Part Number
NSN
NIIN
3833062-2 Control Valve Assembly
010590512
3833077-1 Voter Number One Valve Assembly
010593779
3833077-3 Voter Number One Valve Assembly
010593779
3833083-2 Voter Valve Assembly
010746645
3833089-2 Monitor Valve Assembly
010593781
3833089-3 Monitor Valve Assembly
010593781
3833095-3 Monitor Valve Cover
010571075
3833103-1 Summing Lever Assembly
010593782
3833116-1 Bearing Gland Assembly
010595045
3833147-1 Helical Compression Spring Seat
010585198
3833156-2 Detent Sleeve And Probe Assembly
010593777
3833177-3 System Modification Piston
010746644
3833180-1 System No1 Mod Piston
010598125
3833232 Mecha Seal Replacement Parts Kit
011712993
3834103-1 Summing Lever Assembly
010593784
391001-303 Liquid Quantity Transmitter
010450334
39109-1 Aircraft Access Cover
010542740
3C3461P31 Headed Shoulder Pin
015019574
3HIL87-8PC Test Adapter
014623659
4-400265-16 Indicator Light
011338700
Page: 47 ...

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.

Compare Now »
Clear | Hide