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

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Filter By: Quick Disconnect Coupling Halfs
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Part Number
NSN
NIIN
015032S1-12D Quick Disconnect Coupling Half
005401268
10405343 Quick Disconnect Coupling Half
005401268
12Z6049-11 Quick Disconnect Coupling Half
003301368
155-S5-12D Quick Disconnect Coupling Half
005401268
15525-12D Quick Disconnect Coupling Half
005401268
155S5-12D Quick Disconnect Coupling Half
005401268
155S512D Quick Disconnect Coupling Half
005401268
20773-4F Quick Disconnect Coupling Half
007202000
216-01023-3 Quick Disconnect Coupling Half
005401268
3000SERIES3SB3 Quick Disconnect Coupling Half
003301368
33C472-7075 Quick Disconnect Coupling Half
003301368
3991-017 Quick Disconnect Coupling Half
005401268
3SB3 Quick Disconnect Coupling Half
003301368
405937-1 Quick Disconnect Coupling Half
002775678
44012-12A-N1 Quick Disconnect Coupling Half
005401268
6520-773044 Quick Disconnect Coupling Half
007202000
68A4-D209-3 Quick Disconnect Coupling Half
005401268
9081907 Quick Disconnect Coupling Half
005401268
A-A-59439 Quick Disconnect Coupling Half
002775678
A-A-59439 Quick Disconnect Coupling Half
003301368
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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