E-3a Awacs Aircraft Parts

(Page 62) End item NSN parts | Download PDF   page 62 of 74
Part Number
NSN
NIIN
381-1724-340 Non Wire Wound Variable Resistor
010275459
382 Tapered Roller Bearing Cup
001000300
382955-1 Semiconductor Device Set
000574959
384030 Shaf Turbine Spacer
007659939
38479 Transistor
001114347
3852Z-B23-501AL Nonwire Wound Variable Resistor
010193655
3872-150PC19 O-ring
002313261
387736B Memory Board
011007637
387736C Memory Board
011007637
387736D Memory Board
011007637
3889-1 Threaded Rod End
000517054
39-02728 Machine Thread Plug
000719301
39-27018-1 Access Hinge Assembly
010050662
39067 Filler Opening Cap
013701749
390771 Tapered Roller Bearing Cup
001000575
391-452-9011 Bow Handle
009523091
392033 Float Carburetor
010181929
3974-5R Steering Tie Rod End
004954342
39DD Annular Ball Bearing
001448865
39FF Annular Ball Bearing
001448865
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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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