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

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Part Number
NSN
NIIN
10114380 Shear Bolt
008083795
10114442 Shear Bolt
009174609
10114454 Shear Bolt
009176170
10115721 Shear Bolt
011065220
10115989 Shear Bolt
011429400
51B464-5A12 Shear Bolt
006194800
BACB30NE4-13 Shear Bolt
002021752
BACB30NE4-3 Shear Bolt
011429400
BACB30NE4-6 Shear Bolt
011065220
BACB30NF4-13 Shear Bolt
002021752
BACB30NF4-6 Shear Bolt
011065220
MS21250H04008 Shear Bolt
007607965
NAS1103-4D Shear Bolt
001362874
NAS1105-12D Shear Bolt
006194800
NAS1106-70D Shear Bolt
009558072
NAS1108-18 Shear Bolt
007817623
NAS1304-5H Shear Bolt
012860870
NAS1305-19H Shear Bolt
007215766
NAS6203-19D Shear Bolt
010740172
NAS6203-2 Shear Bolt
010553789
Page:

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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