E-3a Awacs Aircraft Parts

(Page 54) End item NSN parts | Download PDF   page 54 of 74
Part Number
NSN
NIIN
311-0443-000 Spring Pin
006164736
311-7013-000 Plain Tapered Pin
001873218
3110000424803 Airframe Ball Bearing
000424803
3110858 Pipe To Boss Straight Adapter
002405905
3111157 Tube Tee
002775107
3112389 Tube Tee
002790871
311438-1 Armature Assembly
011238264
3117111004-001 Indicator Light
010423666
3117195 Boss Tee
002782779
3120006786132 Sleeve Bushing
006786132
313-0166-00 Hexagon Plain Nut
008238727
313-0166-000 Hexagon Plain Nut
008238727
313011 Brake Disc
010038538
3130265G002 Transistor
001274268
313036 Tapered Roller Bearing Cup
001000300
31304 Tube
010438281
3137299 Flat Belt
010473670
3137299-03 Flat Belt
010473670
3137299-04 Flat Belt
010473670
314-AG5D-R Plug-in Electronic Compon Socket
004393735
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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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