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

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Part Number
NSN
NIIN
10086153 Boss Nipple
006843578
10086154 Boss Nipple
007025377
10086170 Boss Nipple
008259396
2-01238 Boss Nipple
006843578
2-01238J6 Boss Nipple
006843578
3110014 Boss Nipple
006407213
4730006400461 Boss Nipple
006400461
8317X4 Boss Nipple
007025377
AS18280 Boss Nipple
006400461
AS18280 Boss Nipple
006843578
AS18280 Boss Nipple
008259396
AS21902 Boss Nipple
006400461
AS21902 Boss Nipple
006843578
AS21902 Boss Nipple
007025377
AS21902 Boss Nipple
008259396
AS21902J4 Boss Nipple
007025377
AS21902J6 Boss Nipple
006843578
AS4841 Boss Nipple
007025377
MS21902-4 Boss Nipple
006400461
MS21902-6C Boss Nipple
006843578
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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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