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

(Page 12) End item NSN parts page 12 of 51
Part Number
NSN
NIIN
10114339 Machine Bolt
006020775
10114363 Machine Bolt
007543049
10114380 Shear Bolt
008083795
10114442 Shear Bolt
009174609
10114454 Shear Bolt
009176170
10114606 Machine Screw
008393437
10114701 Machine Screw
009321737
10114723 Machine Screw
009472169
10114957 Machine Screw
010739162
10114990 Close Tolerance Screw
010822048
10115721 Shear Bolt
011065220
10115989 Shear Bolt
011429400
10116563 Assembled Washer Plain Nut
001265753
10116574 Hexagon Plain Nut
001413010
10116583 Recessed Washer
001499119
10116667 Hexagon Plain Nut
001991028
10117050 O-ring
001232829
10117051 O-ring
001651935
10117052 O-ring
001651951
10117053 O-ring
001651962
Page: 12 ...

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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