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

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Filter By: Hexagon Self-locking Nuts
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Part Number
NSN
NIIN
0740700 Hexagon Self-locking Nut
000599263
10116527 Hexagon Self-locking Nut
000599263
10121221 Hexagon Self-locking Nut
002632862
1803-048 Hexagon Self-locking Nut
000599265
206SS4 Hexagon Self-locking Nut
000599265
27FH-524 Hexagon Self-locking Nut
009824912
39A11817 Hexagon Self-locking Nut
000599265
442826 Hexagon Self-locking Nut
009824912
520924 Hexagon Self-locking Nut
000599265
5310009824912 Hexagon Self-locking Nut
009824912
55746 Hexagon Self-locking Nut
009824912
58FH-1032 Hexagon Self-locking Nut
002632862
59FH-428 Hexagon Self-locking Nut
000599265
59FH428 Hexagon Self-locking Nut
000599265
69949-4 Hexagon Self-locking Nut
000599263
803-5184193-1X-14 Hexagon Self-locking Nut
000599265
803-5184193-2X-14 Hexagon Self-locking Nut
000599265
853848-00 Hexagon Self-locking Nut
009824912
854261-00 Hexagon Self-locking Nut
000599265
859273-00 Hexagon Self-locking Nut
000599263
Page:

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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