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

(Page 33) End item NSN parts page 33 of 51
Part Number
NSN
NIIN
137564 Dust And Moistur Protective Plug
004333254
1376-01-125P O-ring
001675144
1376-18-515 Boss Nipple
000098259
137618160 Boss Nipple
002896089
138HM10296-1 Rod End Ball Bearing
002323179
1397320 Electrical Plug Connector
006860447
14-656 O-ring
001675138
140-8309 O-ring
005856632
1406AS720-4 Electrical Insulation Sleeving
008715779
003303307
141-19357 O-ring
003303307
1410-0023 Annular Ball Bearing
002938120
1412-634 Annular Ball Bearing
008013140
14149 Dust And Moistur Protective Plug
006875077
1417-526 Self-aligning Plain Bearing
010069515
1417J1-238 O-ring
011469923
142001120 Nonelectrical Wire
000768640
142510-84 Retaining Ring
009037567
143-16207 O-ring
001675125
1441M49G01 Clip-on Nut
013125928
Page: 33 ...

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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