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

End item NSN parts
Filter By: Tube Fitting Clinch Sleeves
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Part Number
NSN
NIIN
156 ITEM 2 Tube Fitting Clinch Sleeve
005547398
156/16 Tube Fitting Clinch Sleeve
002898619
156/2 Tube Fitting Clinch Sleeve
005547398
21922-6C Tube Fitting Clinch Sleeve
006187621
44005B Tube Fitting Clinch Sleeve
002898619
4710-289-8619 Tube Fitting Clinch Sleeve
002898619
4730002898619 Tube Fitting Clinch Sleeve
002898619
4730005547398 Tube Fitting Clinch Sleeve
005547398
900798-4 Tube Fitting Clinch Sleeve
002898619
AS18280 Tube Fitting Clinch Sleeve
002898619
AS18280 Tube Fitting Clinch Sleeve
006187621
AS21922 Tube Fitting Clinch Sleeve
002898619
AS21922 Tube Fitting Clinch Sleeve
006187621
AS21922-6 Tube Fitting Clinch Sleeve
005547398
AS21922-6C Tube Fitting Clinch Sleeve
006187621
MIL-F-18280E Tube Fitting Clinch Sleeve
005547398
MILF18280 Tube Fitting Clinch Sleeve
005547398
MILF18280 Tube Fitting Clinch Sleeve
006187621
MS21918-6 Tube Fitting Clinch Sleeve
005547398
MS21918-6A Tube Fitting Clinch Sleeve
005547398
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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