E-3a Awacs Aircraft Parts

(Page 21) End item NSN parts | Download PDF   page 21 of 74
Part Number
NSN
NIIN
1221-88R Landing Gear Crank
003934766
122450-01 Paper Dielectric Fixed Capacitor
006135230
1226 Transistor
000088405
1228-Q-641 Tapered Roller Bearing Cup
001000575
123001 Electrical Clip
001771700
124-133 Ammeter
010340207
1240 Wire Braid
010166571
124392-5CR-0160 Air Breathing Hose Assembly
009565456
124392-5CR-16 Air Breathing Hose Assembly
009565456
1245442 Structural Angle
002881145
12484-019 Cap Self-locking Nut
003081245
1250449-3 Wire Rope Swaging Sleeve
004891849
1251-0055 Electrical Receptacle Connector
006237199
12551-1 Structural Angle
002881145
1258301-1 Transistor
007554349
125X2 Tapered Roller Bearing Cup
001000300
1260214-1 Externally Threaded Ring
005590119
12610-048 Plate Self-locking Nut
007738642
127033 Eye Wash Station Bottle
012942118
12715946 Electrical Connector Shell
010891671
Page: 21 ...

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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