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

(Page 2) End item NSN parts page 2 of 51
Part Number
NSN
NIIN
00881-0008 Cotter Pin
002368362
0097843 Electrical Insulation Sleeving
008715779
0097843-FH00 Electrical Insulation Sleeving
008715779
0097843-FH00-001 Electrical Insulation Sleeving
008715779
0097845 Electrical Insulation Sleeving
009909911
0097845-FH00 Electrical Insulation Sleeving
009909911
01-236090 Fluid Filter Element
002173588
01-2395-52 O-ring
002651076
0106937 Inter Reel Assembly
014370396
0106937-1 Inter Reel Assembly
014370396
0109-0250 Time Totalizing Meter
000898842
0120-002-601 Electrical Plug Connector
006860447
014-0552-000 Electrical Insulation Tape
008127387
014-0816-000 Electrical Insulation Tape
008127387
Page: 2 ...

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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