F 16 Air Combat Fighter Parts

(Page 2) End item NSN parts page 2 of 58
Part Number
NSN
NIIN
021100-3 Aircraft Navigational Light
014433629
02251000-1 Electrical Cable Assembly-switch
013920590
03-823-40E001 Self-aligning Plain Bearing
010487927
03-829-04E001 Self-aligning Plain Bearing
010592041
031566 Sleeve Nut
011937947
031568 Shoulder Screw
011968636
043-22100(590)1-4INNPTMALEOPT4 Compressed Gas Regulator
010788174
043-22101-590-1/4 NPT MALE OPT 4 Compressed Gas Regulator
010788174
04MR011-007 Electrical Conne Retaining Plate
010668719
05-435070 Sleeve Spacer
010610114
07-0501-3903 Electronic Shielding Gasket
010730657
071-5190-00 Radio Test Set
012984586
07A061-24A Tube Coupling Swage Ferrule
010525210
0950-1671 Power Supply
011823036
0950-1962 Power Supply
013109822
1-1004-48 Coupling
008963930
10-412119-10G Electrical Connector Cover
010885889
1000574 Front Gear Plate
010783233
1000617 Shaft-wiper Assembly
010774140
10080962-101 Radio Frequency Cable Assembly
010797653
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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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