E-3a Awacs Aircraft Parts

(Page 42) End item NSN parts | Download PDF   page 42 of 74
Part Number
NSN
NIIN
2226768 Electromagnetic Relay
008110670
22338-51F900-190 Hold Down Fitting
010423052
22380 Sleeve Bushing
006786132
22570 V Belt
010304369
226-7-28 Oxygen Tank Adapter
001794028
2261-24 Nonmetallic Special Shaped Secti
009389351
227032 Plain Stud
002876471
22759/3-16-9 Electrical Wire
012035398
229-8000-020 Torque Motor
010304079
22910 REV C Generator Control
002228246
22NC2-62 Clinch Self-locking Nut
008004715
2300-79020 O-ring
006311342
230079020 O-ring
006311342
23023A62 Clinch Self-locking Nut
008004715
23052-0001 Plug-in Electronic Compon Socket
004393735
23079 Branche Electrical Cord Assembly
010061836
231014 Tapered Roller Bearing Cup
001000575
231104-701 Unitized Semiconductor Devices
005406376
23250 Special Shape Structural Section
010673581
233-1002-01 Aircraft Navigational Light
013589974
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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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