E-3a Awacs Aircraft Parts

(Page 51) End item NSN parts | Download PDF   page 51 of 74
Part Number
NSN
NIIN
2TX-26-19/38WHT/BLK Electrical Special Purpose Cable
010144428
2W1717 Transistor
008247848
2W1721 Transistor
007732412
2X696B Tapered Roller Bearing Cup
001000300
2XE-26-19/38WHT/BLK Electrical Special Purpose Cable
010144428
3-12136-155-1 Positive Drive Belt
009828174
3-13324-1 Shipping And Stora Document Tube
007583727
3-16-6 Loop Clamp
002903637
3-5-8NE Surveying Tripod
002222505
3-533286-5 Electrical Receptacle Connector
013112688
3-8-6 Loop Clamp
002903637
3-86 Loop Clamp
002903637
3-8DDSS Pipe Elbow
004971707
3-93987-1 Door Tube
005583000
3-95685 Steering Plate Pin
003041999
30-1037-1 Aircraft Navigational Light
010202550
30-2492-1 Sleeve Spacer
014680524
30-754-557-02 Electrical-electron Mounting Pad
009293729
300-75 Maintenance Platform Control Box
012945043
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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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