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

(Page 17) End item NSN parts page 17 of 51
Part Number
NSN
NIIN
10163240 O-ring
002638035
10163241 O-ring
002651074
10163243 O-ring
002651076
10163255 O-ring
002799322
10163261 O-ring
002881976
10163267 O-ring
002913073
10163282 O-ring
003378593
10163287 O-ring
003770921
10163323 O-ring
007592010
10163324 O-ring
007592022
10163325 O-ring
007592113
10163859 O-ring
001326974
10163863 O-ring
001661041
10163865 O-ring
002500222
10163867 O-ring
002519367
10163882 O-ring
007651948
10163903 Dust And Moistur Protective Plug
006821857
10164315 Metal Sheet
002320583
10167798 Tube Cap
002212127
101715-75 Flat Washer
001670842
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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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