E-3a Awacs Aircraft Parts

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Part Number
NSN
NIIN
019147-2 Plate Self-locking Nut
011583614
12610-048 Plate Self-locking Nut
007738642
13616-048-4 Plate Self-locking Nut
008198384
3M144A4-4 Plate Self-locking Nut
008198384
418463-704 Plate Self-locking Nut
007287713
833635-00 Plate Self-locking Nut
011819346
950322-3 Plate Self-locking Nut
010384137
BACN10GH3A8 Plate Self-locking Nut
011897486
CSP183-4-4 Plate Self-locking Nut
008198384
F1972-4-4 Plate Self-locking Nut
008198384
GN10AB428 Plate Self-locking Nut
007738642
GSM-904M Plate Self-locking Nut
007287713
HS4174-2 Plate Self-locking Nut
011819346
K2000-4 Plate Self-locking Nut
007738642
K2000-428 Plate Self-locking Nut
007738642
M 12600-04 Plate Self-locking Nut
007287713
M 12600-40 Plate Self-locking Nut
007287713
MF1000-3 Plate Self-locking Nut
011819346
MF1001-06 Plate Self-locking Nut
010384137
MILN25027 Plate Self-locking Nut
007738642
Page:

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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