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

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Part Number
NSN
NIIN
10082455 Cotter Pin
002341856
10122590 Cotter Pin
002341861
117935 Cotter Pin
002341856
12Z5056-35 Cotter Pin
002341861
184322 Cotter Pin
002341856
280458PC6 Cotter Pin
002341856
322-02320 Cotter Pin
002341856
393911 Cotter Pin
000531541
401-208 Cotter Pin
002341856
42P6514 Cotter Pin
002341856
5118-80-11 Cotter Pin
002341856
5315-234-1861 Cotter Pin
002341861
5315002341856 Cotter Pin
002341856
5315002341861 Cotter Pin
002341861
5315PL0248815 Cotter Pin
002341861
75F4121 Cotter Pin
002341861
75F6061 Cotter Pin
002341861
863607-1716 Cotter Pin
002341861
A10390 Cotter Pin
002341861
AN380C2-4 Cotter Pin
002341856
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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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