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

(Page 14) End item NSN parts page 14 of 51
Part Number
NSN
NIIN
10122542 Spring Pin
000589747
10122550 Cotter Pin
000673871
10122561 Headed Straight Pin
000817876
10122589 Cotter Pin
002341846
10122597 Cotter Pin
002368362
10122668 Cotter Pin
005545287
10122683 Cotter Pin
006197976
10122737 Headed Straight Pin
008123759
10122778 Spring Pin
008530681
10122805 Headless Straight Pin
009265761
10122902 Spring Pin
011166789
10123476 Solid Rivet
001176885
10123803 Pin-rivet
006583842
10123844 Blind Rivet
008006275
10123881 Solid Rivet
009008946
10123902 Blind Rivet
009375448
10124028 Blind Rivet
010846090
10124907 Socket Head Cap Screw
000556294
10124921 Socket Head Cap Screw
000582067
10124948 Socket Head Cap Screw
000680543
Page: 14 ...

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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