Tf-33-p-7 (c-141a/b) Aircraft Engine Parts

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Part Number
NSN
NIIN
477068 Sleeve Bushing
000657922
501370 Sleeve Bushing
009393350
501377 Sleeve Bushing
009423467
512265 Sleeve Bushing
009429308
524112 Sleeve Bushing
011605397
524114 Sleeve Bushing
011625393
667276 Sleeve Bushing
000039484
69-10316-2 Sleeve Bushing
008524453
739773 Sleeve Bushing
005036308
BACB28X5C30 Sleeve Bushing
011449627
JK5604C080 Sleeve Bushing
005036308
NAS72-3-005 Sleeve Bushing
005178629
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Engine, Aircraft, Tf-33-p-7 (c-141a/b)

Picture of Tf-33-p-7 (c-141a/b)  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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