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

(Page 6) End item NSN parts page 6 of 13
Part Number
NSN
NIIN
10159961 O-ring
002317701
10159972 O-ring
001651972
10160158 Retaining Ring
005978487
10163210 O-ring
001668396
10163211 O-ring
001668398
10163216 O-ring
001675137
10163287 O-ring
003770921
10163334 O-ring
008094365
10163859 O-ring
001326974
10163863 O-ring
001661041
101715-75 Flat Washer
001670842
10183828 Retaining Ring
008049734
10186254 O-ring
001668397
10186314 O-ring
001661055
10200133 O-ring
001668395
102696PC37 Nonelectrical Wire
000768640
103049-05 Loop Clamp
002903637
10321064 Electrical Insulation Tape
004801329
10340905 Electrical Connector Cable Clamp
011795430
103426CPSCH Machine Screw
008892997
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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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