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

(Page 34) End item NSN parts page 34 of 51
Part Number
NSN
NIIN
002638034
001358622
002638034
1446-028 O-ring
005805056
1446-140 O-ring
005856632
144682 Tube Coupling Nut
002870291
145-540-90115 Machine Bolt
001510779
145-542-90101 Machine Bolt
006020775
145545 O-ring
002917295
1460-321 Retaining Ring
009037567
146373PC47 Flat Washer
002748768
146374PC3 Flat Washer
002748768
146374PC47 Flat Washer
002748768
146424-1 Cotter Pin
000673871
146424PC1 Cotter Pin
000673871
147-47804-3 Metallic Tube
002788726
14722 Hexagon Head Cap Screw
002693235
Page: 34 ...

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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