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

(Page 41) End item NSN parts page 41 of 51
Part Number
NSN
NIIN
177004PC227 Machine Screw
009399189
177030-126 Annular Ball Bearing
001980975
178554-6 Machine Screw
006140245
17877R Machine Screw
006140245
1788808 Electrical Contact
006366876
1793-02 O-ring
001358622
1793-023 O-ring
000076143
1793-024 O-ring
002500236
1793-111 O-ring
002483839
1793-116 O-ring
002483850
1793-117 O-ring
002500222
1793-121 O-ring
003378593
1793-123 O-ring
005791021
1793-124 O-ring
002651074
1793-126 O-ring
002651076
1793-127 O-ring
002651078
1793-129 O-ring
002651097
1793-134 O-ring
006410119
1793-135 O-ring
002917336
1793-136 O-ring
002917295
Page: 41 ...

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