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

(Page 22) End item NSN parts page 22 of 51
Part Number
NSN
NIIN
10V60-141-117 O-ring
002500222
10V60-141-121 O-ring
003378593
10V60-141-123 O-ring
005791021
10V60-141-124 O-ring
002651074
10V60-141-126 O-ring
002651076
10V60-141-127 O-ring
002651078
10V60-141-129 O-ring
002651097
10V60-141-134 O-ring
006410119
10V60-141-135 O-ring
002917336
10V60-141-136 O-ring
002917295
10V60-141-139 O-ring
002526052
10V60-141-141 O-ring
005278555
10V60-141-142 O-ring
002526056
10V60-141-151 O-ring
009359226
10V60-141-16 O-ring
002638034
10V60-141-215 O-ring
002500235
10V60-141-217 O-ring
002651090
10V60-141-227 O-ring
002609338
10V60-141-231 O-ring
002913073
10V60-141-234 O-ring
002519367
Page: 22 ...

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