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

(Page 3) End item NSN parts page 3 of 13
Part Number
NSN
NIIN
0713-176 Screw Thread Insert
002862458
0740700 Hexagon Self-locking Nut
000599263
0740717 Electrical Connector Cover
002386419
08-167 Electrical Plug Connector
010123066
080-29123-90 O-ring
001668390
080A05200 Flat Washer
001872354
0855607500 O-ring
002651086
09-04-6559 Toggle Switch
009619920
0900-1001 Toggle Switch
009619920
09083724 O-ring
002483835
0BT24780 Tapered Roller Cone And Rollers
001003537
1-2956-1 Fluid Passage Bolt
002780375
1-97164A37 Retaining Ring
002635877
10-33 Wire Rope Swaging Sleeve
001329163
10-90351-12 O-ring
002483836
10012420 Gasket
011759232
1002-0011-258 Bearing Ball
001839164
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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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