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

(Page 7) End item NSN parts page 7 of 51
Part Number
NSN
NIIN
0900988-7 Hexagon Slotted Plain Nut
009980608
093-58807-7 Sealing Plug Assembly
009869445
098374 O-ring
001675122
0BT15123 Tapered Roller Cone And Rollers
001982169
0N509111-3 Lug Terminal
001138190
0RS906B70M O-ring
010460627
0S020176 Packing Retainer
001715069
0S026479 O-ring
000076143
0T65237.53.69 O-ring
002920578
1-2093 Fluid Filter Element
002173588
1-210761-6 Annular Ball Bearing
001419561
1-2956-1 Fluid Passage Bolt
002780375
1-331418-1 Lug Terminal
001138190
1-4D1AX5-8LG Headless Straight Pin
009265761
1-4DIAX5-8LG Headless Straight Pin
009265761
1-501-2-210 O-ring
004060883
1-97164A37 Retaining Ring
002635877
1-PDR-134A-10 Blind Rivet
008006275
Page: 7 ...

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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