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

End item NSN parts page 1 of 51
Part Number
NSN
NIIN
000001080500000 Blind Rivet
008006278
000001080590000 Blind Rivet
008006275
000001081000000 Blind Rivet
008391124
000004001160000 Machine Screw
007195400
000004001220000 Recessed Washer
001499146
001-236090 Fluid Filter Element
002173588
00213-1011 Tapered Roller Bearing Cup
001000542
0024432957 O-ring
002526056
003-008605-007 Machine Screw
009952117
0030-1064GOVT O-ring
001651972
003274 Tapered Roller Cone And Rollers
001982169
004-003005-041 Lock Washer
009265877
00524K O-ring
002500236
00542B O-ring
005791021
00546C O-ring
002651078
00594C O-ring
002519369
00620F O-ring
002913275
0065216.35.63 O-ring
004060883
006563406-97013 Thermal Insulation Pipe Covering
006563406
007-654134 Tapered Roller Cone And Rollers
001982169
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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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