E-3a Awacs Aircraft Parts

(Page 12) End item NSN parts | Download PDF   page 12 of 74
Part Number
NSN
NIIN
10123803 Pin-rivet
006583842
10123881 Solid Rivet
009008946
10129876 Diode Semiconductor Device
011987030
10130038 Transistor
014224818
10131401 Electrical Receptacle Connector
010447534
10131520 Electrical Receptacle Connector
010870307
10134-2001 Structural Angle
010718248
10135134 Electrolytic Fixed Capacitor
013257396
10135638 Electrical Plug Connector
011283615
10138206 Electrical Connector Cover
012146153
10139417 Electrical-electron Mounting Pad
009293729
10139485 Heat Sink-insulator
011220470
10149769 Electrical Wire
004879174
10149908 Electrical Lead
010346492
10150462 Plastic Sheet
005405673
10150681 Nonelectrical Wire
010078936
10154145 Retaining Ring
005505176
10154280 Electrolytic Fixed Capacitor
003295928
10159664 Machine Bolt
001133769
10159804 O-ring
001727187
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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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