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

(Page 38) End item NSN parts page 38 of 51
Part Number
NSN
NIIN
156372A Dial Indicating Pressure Gage
008129169
157618232 O-ring
008163546
157680A Compressor D Spacer
001030838
157680CLA Compressor D Spacer
001030838
157708 Fuel Drain Valve Assembly
003937878
158001-104 Machine Screw
009399189
158206 Dust And Moistur Protective Plug
002923292
158244 Ear Cushion
007156158
159-1102-005 Lug Terminal
001141300
160-19357 O-ring
000050482
1603169 Retaining Ring
009037567
1604-73 Dust And Moistur Protective Plug
006875077
1604-73Y Dust And Moistur Protective Plug
006875077
1604756 Sector And Shaft Assembly
007235848
1604756-1 Sector And Shaft Assembly
007235848
160497 Plug Cock
003267134
1618302 Annular Ball Bearing
008013140
1618380 Lug Terminal
001141300
161K0228-3 O-ring
004060883
Page: 38 ...

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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