Tf33-100 (e3a/b/c) Aircraft Engine Parts

(Page 11) End item NSN parts page 11 of 13
Part Number
NSN
NIIN
130-C-69 O-ring
002651086
131-C-69 O-ring
002651084
131916 O-ring
001668428
13217E4291-1 O-ring
005312070
13219E3019-2 Electrical Connector Cover
002218620
132636 Machine Screw
008892997
133591 Tube Coupling Nut
002221912
134 O-ring
006410119
134-C-69 O-ring
006410119
134B46A O-ring
006410119
135-C-69 O-ring
002917336
13503 Hexagon Slotted Plain Nut
002641240
1355-096 O-ring
001668397
136-C-69 O-ring
002917295
137-004-9016 Needle Roller Bearing
002274710
1376-01-125P O-ring
001675144
139AS105 Wire Rope Swaging Sleeve
001329163
140-21323 Tube Coupling Nut
002221912
1410-0023 Annular Ball Bearing
002938120
142001120 Nonelectrical Wire
000768640
Page: 11

Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  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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