E-3a Awacs Aircraft Parts

(Page 27) End item NSN parts | Download PDF   page 27 of 74
Part Number
NSN
NIIN
1500-06-036-005 Heat Exchanger
011415989
150066 Diode Semiconductor Device
004009899
1501-33-5 Ceramic Dielectr Fixed Capacitor
004709169
1503-24 Nonmetallic Hose
009542641
150682-0001 Diplexer
003606529
150682-1 Diplexer
003606529
150701-5 O-ring
005592663
151-0221-00 Transistor
004016209
151-0268-00 Unitized Semiconductor Devices
002476846
1518-6 Wire Rope
010747917
151D346 Generator Control
002228246
152-0552-00 Diode Semiconductor Device
010639270
1523 Cable Strain Relief Bushing
000686767
152459 Plate Assembly
009688236
152459-1 Plate Assembly
009688236
15268 Pinion Ay Drive
010263860
153-300 Unitized Semiconductor Devices
005406376
153061-182 Self-locking Stud
009340293
153223 Shouldered And Recessed Washer
002291236
1536103 Fixed Moun Mechanical Tachometer
005300557
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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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