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

(Page 8) End item NSN parts page 8 of 13
Part Number
NSN
NIIN
10V60-141-130 O-ring
002651086
10V60-141-131 O-ring
002651084
10V60-141-134 O-ring
006410119
10V60-141-135 O-ring
002917336
10V60-141-136 O-ring
002917295
10V60-141-142 O-ring
002526056
10V60-141-235 O-ring
002519369
11-00671-4 Electrical Wire
009391745
110488 Machine Screw
006140245
111-11737 O-ring
001326974
1115312 Nonmetallic Hose
005951089
11176409-3 Hexagon Plain Nut
002085769
112-11737 O-ring
001326976
112-7507 O-ring
007332208
112-C-69 O-ring
007332208
1159 Hexagon Plain Nut
001671344
117-8801 O-ring
001651936
117507 Retaining Ring
008037304
Page: 8 ...

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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