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

(Page 11) End item NSN parts page 11 of 51
Part Number
NSN
NIIN
10107319 Airframe Ball Bearing
000420446
10107325 Airframe Ball Bearing
000424807
10107684 Self-aligning Plain Bearing
010069515
10108317 Tube Tee
002775107
10108407 Tube Cap
005411207
10108412 Tube Cap
005418296
10108419 Hose Clamp
005551352
10108424 Threaded Tube Fitting Plug
005856567
10108426 Tube Cap
005858770
10108438 Boss Reducer
007200233
10108443 Tube Elbow
008072274
10110615 Metallic Tube
002788726
10110616 Metallic Tube
002788727
10111501 Blind Rivet
011335889
10111566 Blind Rivet
011364497
10111712 Blind Rivet
011435075
10112148 Blind Rivet
012044780
10114145 Machine Bolt
000800121
10114162 Machine Bolt
001167790
10114228 Machine Bolt
003083519
Page: 11 ...

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.

Compare Now »
Clear | Hide