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

(Page 4) End item NSN parts page 4 of 13
Part Number
NSN
NIIN
1002199-P3 Tapered Roller Cone And Rollers
001003537
10076636 O-ring
001651936
10082455 Cotter Pin
002341856
10086129 Tube Fitting Locknut
002776372
10086153 Boss Nipple
006843578
10086154 Boss Nipple
007025377
10086170 Boss Nipple
008259396
10087983 Lock Washer
001596209
10107357 Bearing Ball
001839164
10114639 Machine Screw
008892997
10114742 Machine Screw
009583409
101151 O-ring
005312068
10116000 Shear Bolt
011442206
10116527 Hexagon Self-locking Nut
000599263
10116563 Assembled Washer Plain Nut
001265753
10116583 Recessed Washer
001499119
10116605 Flat Washer
001670807
10116652 Flat Washer
001849001
10116655 Flat Washer
001872354
10117050 O-ring
001232829
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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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