E-3a Awacs Aircraft Parts

(Page 66) End item NSN parts | Download PDF   page 66 of 74
Part Number
NSN
NIIN
40P1547-2 Light Lens
010355273
410-0481-160 Reed Relay
000257232
41004-012 Quick Disconnect Coupling Half
005558402
410178-2 Turnlock Fastener Receptacle
007279734
410966-602 Clinch Self-locking Nut
008004715
410976-403 Clinch Self-locking Nut
005966462
411040 Cartridge Fuse
002803478
411402-2459 Electrical Wire
008252071
4116R-001-821 Film Fixed Resistor Network
011308160
411R Indicating Vacuum Gage
008067222
411R483H01 Externally Relieved Body Screw
000433780
411R665H01 Nonmetallic Bushing
005758662
411R665H02 Nonmetallic Bushing
005758660
411R803H01 Torsion Helical Spring
000497855
412A07878-54030 Earphone Shell
005202686
414-0664-001 Tip Plug
002018965
414121 Preformed Packing
009800732
414121WE Preformed Packing
009800732
417-0393 Electrical Connector Cover
009058316
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Aircraft, Awacs, E-3a

Picture of E-3a  Awacs Aircraft

The Boeing E-3 Sentry, commonly known as AWACS, is an airborne early warning and control (AEW&C) aircraft developed by Boeing as the prime contractor. Derived from the Boeing 707, it provides all-weather surveillance, command, control, and communications, and is used by the United States Air Force, NATO, Royal Air Force, French Air Force, and Royal Saudi Air Force. The E-3 is distinguished by the distinctive rotating radar dome above the fuselage. Production ended in 1992 after 68 aircraft had been built.

In the mid-1960s, the US Air Force (USAF) was seeking an aircraft to replace its piston-engined Lockheed EC-121 Warning Star, which had been in service for over a decade. After issuing preliminary development contracts to three companies, the USAF picked Boeing to construct two airframes to test Westinghouse Electric and Hughes's competing radars. Both radars used pulse-Doppler technology, with Westinghouse's design emerging as the contract winner. Testing on the first production E-3 began in October 1975.

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