E-3a Awacs Aircraft Parts

(Page 69) End item NSN parts | Download PDF   page 69 of 74
Part Number
NSN
NIIN
429R113H02 Sleeve Spacer
010898504
429R490H02 Transmitter Plate Orifice
010177428
42D6594-3 Wheel-track Chock
002943696
42D92 Pressure Switch
007124030
42ND16-054 Spline Self-locking Nut
005829549
42P14141-8 Plain Tapered Pin
001873218
4301EG-400 Grooved Clamp Coupling
004557464
4303 Drainage Pipe Tee-y
010698146
433051 Oil Pressure R Seat
008018252
434 Metal Sheet
008446812
434563-4 Motor Bracket
009943465
43606N406 Tube To Hose Straight Adapter
000518568
4376 Psychrometer
008561485
438596 Average Press Probe
008863920
439-0032-000 Electrical Wire
006432494
439-0033-000 Electrical Wire
006432490
439-1145-500 Electrical Special Purpose Cable
000062653
439-4044-000 Electrical Wire
005786975
439-4825-000 Electrical Wire
008252071
4390033-000 Electrical Wire
006432490
Page: 69

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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