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

(Page 10) End item NSN parts page 10 of 13
Part Number
NSN
NIIN
123-235-1 O-ring
002519369
123-235-5 O-ring
002519369
124027-4CR0136 Tube Fitting Flared Sleeve
005552901
12490-7 O-ring
002483836
127-C-69 O-ring
002651078
127D488 PIECE 14 Bearing Ball
001839164
128-4VM Wire Rope Swaging Sleeve
001329163
128935 Annular Ball Bearing
002938120
12Z1197-29 Socket Head Cap Screw
002074017
12Z3013-22 Flat Washer
001849002
12Z3018-25 Lock Washer
002091235
12Z33460-12 Nonmetallic Hose
005951089
12Z5010-2 Retaining Ring
005978487
12Z5056-35 Cotter Pin
002341861
12Z6049-11 Quick Disconnect Coupling Half
003301368
12Z6353-7 Transistor
001332983
12Z64PC2 Retaining Ring
002635877
12Z9022-11 Packing Retainer
001715889
130-020-3 Pressure Transmitter
000674946
Page: 10 ...

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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