Tf33-100 (e3a/b/c) Aircraft Engine Parts

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Part Number
NSN
NIIN
0407-388 Machine Screw
009399148
10114639 Machine Screw
008892997
10114742 Machine Screw
009583409
103426CPSCH Machine Screw
008892997
10388353 Machine Screw
009844977
110488 Machine Screw
006140245
132636 Machine Screw
008892997
177004PC221 Machine Screw
009399187
178554-6 Machine Screw
006140245
17877R Machine Screw
006140245
19024 Machine Screw
008892997
19024ADX Machine Screw
008892997
19029 Machine Screw
009844977
19029ADX Machine Screw
009844977
194-21 Machine Screw
006140245
2011132 Machine Screw
009583409
220 0102 Machine Screw
008892997
3038-9029PC5 Machine Screw
008892997
328C155D0440C06 Machine Screw
008892997
3871-0024 Machine Screw
008892997
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Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  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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