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

(Page 16) End item NSN parts page 16 of 51
Part Number
NSN
NIIN
10159804 O-ring
001727187
10159806 O-ring
001675138
10159817 O-ring
001661041
10159818 O-ring
002455611
10159921 O-ring
005827475
10159961 O-ring
002317701
10159963 O-ring
013970829
10159969 O-ring
001675135
10159972 O-ring
001651972
10159989 O-ring
010050515
10159993 O-ring
004801853
10160009 Dust And Moistur Protective Plug
002923292
10160101 Serrated Lock Ring
004057576
10160158 Retaining Ring
005978487
10163190 O-ring
000076143
10163208 O-ring
001661101
10163211 O-ring
001668398
10163214 O-ring
001675125
10163226 O-ring
002483850
10163229 O-ring
002500236
Page: 16 ...

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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