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

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Part Number
NSN
NIIN
10108407 Tube Cap
005411207
10108412 Tube Cap
005418296
10108426 Tube Cap
005858770
10167798 Tube Cap
002212127
12C Tube Cap
002212128
2-02813-6 Tube Cap
006183572
21C1595-17 Tube Cap
002212128
21C2201-104 Tube Cap
002212128
29496 Tube Cap
005858770
3100794 Tube Cap
005418296
3111991 Tube Cap
006183572
3C Tube Cap
002212126
418441-5 Tube Cap
010614150
454 289 Tube Cap
002212126
4730006183572 Tube Cap
006183572
4730006189069 Tube Cap
006189069
4730006400632 Tube Cap
006400632
7M626A8D Tube Cap
005418296
8020454 Tube Cap
002212128
8176313 Tube Cap
002212126
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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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