E-3a Awacs Aircraft Parts

(Page 40) End item NSN parts | Download PDF   page 40 of 74
Part Number
NSN
NIIN
210241 Tapered Roller Bearing Cup
001000300
2105-5 Amplifier-power Supply
002335901
21072 Tapered Roller Bearing Cup
001000575
211 Annular Ball Bearing
001565446
211-1214 Fluid Filter
002443610
211-24 Nonmetallic Hose
009542641
211-250B Oxygen Mask Valve
002265334
211-250C Oxygen Mask Valve
002265334
211-250D Oxygen Mask Valve
002265334
2110-0005 Packing With Retainer
008059386
2110-0275 Cartridge Fuse
002803478
211146CL6 Counterbalance Weight
003965097
212 3/4IN WIDE Electrical Insulation Tape
005431597
212-103 Tip Plug
002018965
212BLACK Tip Plug
002018965
213692-4D Pipe To Boss Straight Adapter
002405905
2139258G001 Electrical-electron Mounting Pad
009293729
214-8-1 Housing Cable Assembly
005205598
21422 Air Engine Starter
010843484
2144040-1 Electrical Contact
001388286
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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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