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

(Page 45) End item NSN parts page 45 of 51
Part Number
NSN
NIIN
190988 Screw Thread Insert
002862458
191 O-ring
001675144
1923-1INCHID Hose Clamp
005551352
1934-TX-10RED Electrical Wire
000626685
1934TX10-2 Electrical Wire
000626685
194-21 Machine Screw
006140245
194946 Retaining Ring
005982052
194948 Retaining Ring
005982052
195005 Cam Control Shim
002941239
19674-4 Sleeve Bearing
005859305
196A857H06 Dust And Moistur Protective Plug
006875077
196E184-35 Retaining Ring
008037304
197164A37 Retaining Ring
002635877
1979479 Fluid Filter Element
002173588
199059 O-ring
005853346
199064 O-ring
005312230
199783 O-ring
005808059
199994 O-ring
005856632
1A08T1D08J1200R Nonmetallic Hose
008156354
1A6040 Magnetic Machine Thread Plug
014805412
Page: 45

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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