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

(Page 19) End item NSN parts page 19 of 51
Part Number
NSN
NIIN
10301730 O-ring
000794578
10326700 Lug Terminal
001138191
10338603 Fluid Filter Element
002033593
10338991 Packing Retainer
001715042
10346608 O-ring
001675122
10353714 Cotter Pin
001850037
10358 Needle Roller Bearing
002770337
10360536 Machine Bolt
000541438
10361133 Hexagon Slotted Self-locking Nut
001984735
10370042 O-ring
001651949
10370392 Incandescent Lamp
001557786
103896-13 Catch Strike
012914265
10398674 Machine Screw
006140246
103S102 Tapered Roller Bearing Cup
001000544
104011-13 Catch Strike
012914265
10405343 Quick Disconnect Coupling Half
005401268
104223-000 Bearing Ball
000442269
1046 Key Blank
002181776
1046Z106 Fluid Filter Element
002173588
104A114 O-ring
004801853
Page: 19 ...

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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