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

(Page 23) End item NSN parts page 23 of 51
Part Number
NSN
NIIN
10V60-141-235 O-ring
002519369
10V60-141-261 O-ring
002913275
10V60-141-920 O-ring
002638035
11-00671-4 Electrical Wire
009391745
002651076
11-1313 Sole Cleaning Unit Insert
009738428
11-261 O-ring
002913275
11-3706-11 Tapered Roller Cone And Rollers
001982169
11-392880 Metallic Tube
002783294
110126-5 Dust And Moistur Protective Plug
002923292
11031106-1 Tapered Roller Bearing Cup
001000542
110354 Electrical Wire
008173597
110488 Machine Screw
006140245
11069835 Electrical Special Purpose Cable
008392119
111-11737 O-ring
001326974
111115221 Packing Retainer
001716758
1112-15 Retaining Ring
009037567
112-0579-016 Socket Head Cap Screw
000556294
112-1055-070 Machine Screw
007092013
Page: 23 ...

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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