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

(Page 10) End item NSN parts page 10 of 51
Part Number
NSN
NIIN
10075088 O-ring
002259054
10076636 O-ring
001651936
002500236
10082395 Flat Washer
001499126
10082396 Recessed Washer
001499146
10082436 Flat Washer
002090295
10086125 Tube Fitting Locknut
001596339
10086141 Tube Fitting Locknut
004536187
10086153 Boss Nipple
006843578
10086154 Boss Nipple
007025377
10086170 Boss Nipple
008259396
10086590 O-ring
001661086
10086591 O-ring
001675115
10086601 O-ring
002638034
10086602 O-ring
003303307
10086608 O-ring
010103371
10087193 Electrical Plug Connector
006860447
10087753 Machine Screw
009272068
10087991 Flat Washer
001670754
10105736-5 Electrical Insulation Sleeving
009909911
Page: 10 ...

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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