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

(Page 42) End item NSN parts page 42 of 51
Part Number
NSN
NIIN
1793-139 O-ring
002526052
1793-141 O-ring
005278555
1793-142 O-ring
002526056
1793-151 O-ring
009359226
1793-16 O-ring
002638034
1793-215 O-ring
002500235
1793-217 O-ring
002651090
1793-227 O-ring
002609338
1793-23 O-ring
000076143
1793-231 O-ring
002913073
1793-234 O-ring
002519367
1793-235 O-ring
002519369
1793-261 O-ring
002913275
1793-912 O-ring
002638033
1793-920 O-ring
002638035
17D6703H10 Electrical Receptacle Connector
005572054
17KP370 O-ring
001651936
17N8D0860 Fire Detector Sy Sensing Element
014483059
17P8D2000-501 Fire Detector Sy Sensing Element
014483059
17X136 Tapered Roller Cone And Rollers
001982169
Page: 42 ...

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.

Compare Now »
Clear | Hide