Tf33-100 (e3a/b/c) Aircraft Engine Parts

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Part Number
NSN
NIIN
11176409-3 Hexagon Plain Nut
002085769
1159 Hexagon Plain Nut
001671344
156/6 Hexagon Plain Nut
006382605
20296 Hexagon Plain Nut
001671344
207865 Hexagon Plain Nut
008277023
218330-6 Hexagon Plain Nut
002827817
24098R1 Hexagon Plain Nut
002827817
2428142440 Hexagon Plain Nut
006382605
2439 Hexagon Plain Nut
002686042
25099 Hexagon Plain Nut
006382605
254616 Hexagon Plain Nut
002827817
278-156 Hexagon Plain Nut
001671344
2D4 Hexagon Plain Nut
002686042
3110319 Hexagon Plain Nut
006382605
3111880 Hexagon Plain Nut
002085769
32-57058-19 Hexagon Plain Nut
006382605
404 225 Hexagon Plain Nut
001671344
477 620 Hexagon Plain Nut
006382605
512 Hexagon Plain Nut
002686042
5310002827817 Hexagon Plain Nut
002827817
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Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  Aircraft Engine

The Pratt & Whitney JT3D is an early turbofan aircraft engine derived from the Pratt & Whitney JT3C turbojet. It was first run in 1958 and was first flown in 1959 under a B-45 Tornado test aircraft. Over 8,000 JT3Ds were produced between 1959 and 1985. Most JT3D engines still in service today are used on military aircraft, where the engine is referred to by its USAF designation of TF33.

Aware of the competition from the Rolls-Royce Conway turbofan, Pratt&Whitney decided to develop the JT3D turbofan from the JT3C turbojet for later deliveries of the Boeing 707 and the Douglas DC-8, then nearing entry into service. A 2-stage fan replaced the first 3 stages of the 9-stage JT3C LP compressor. On the LP turbine, the second stage was enlarged and a third stage added.

Unlike GE with the CJ805-23, Pratt & Whitney had not undertaken any transonic fan research prior to designing the JT3D, so they were unable to incorporate a single stage unit into the specification. Instead P&W designed a 2-stage unit based on some research they had done to support the J91 nuclear turbojet.

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