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

(Page 31) End item NSN parts page 31 of 51
Part Number
NSN
NIIN
12Z64PC2 Retaining Ring
002635877
12Z64PC3 Retaining Ring
009037567
12Z9022-11 Packing Retainer
001715889
130-020-3 Pressure Transmitter
000674946
13038987-2 Tubeaxial Fan
010307807
130503H Tapered Roller Bearing Cup
001000544
1306M30 Magnetic Machine Thread Plug
014805412
1306M30P03 Magnetic Machine Thread Plug
014805412
1306M30P05 Magnetic Machine Thread Plug
014805412
13078 Tube Coupling Nut
002870291
130972 Flat Washer
001861295
1311M82 Branched Metal Tube Assembly
012111873
1311M82G01 Branched Metal Tube Assembly
012111873
1311M82G02 Branched Metal Tube Assembly
012111873
131899 Machine Screw
005792139
131916 O-ring
001668428
13215E9649 Electrical Receptacle Connector
005572054
13217E4366 Fluid Filter Element
008498358
Page: 31 ...

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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