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

(Page 28) End item NSN parts page 28 of 51
Part Number
NSN
NIIN
1237-10-2218FTS Fluid Filter Element
002773274
124-4 Nonmetallic Hose
008571732
124-4322603 PC 127 Flat Washer
001499126
124-C-69 O-ring
002651074
124135-003 Annular Ball Bearing
007202336
124135-3 Annular Ball Bearing
007202336
12490-100 O-ring
002500236
12490-127 O-ring
002526052
12490-22 O-ring
002651090
125-19962-12 Machine Screw
005825807
12531-2 Actuator Cover
006727898
126-C-69 O-ring
002651076
12619165 Clinch Plain Nut
008787111
12619466-2 O-ring
010460627
1264M12P01 Aircraft Fluid Manifold
011989265
1264M12P02 Aircraft Fluid Manifold
011989265
1264M12P03 Aircraft Fluid Manifold
011989265
1264M12P04 Aircraft Fluid Manifold
011989265
1265M63 Metal Tube Assembly
012122680
Page: 28 ...

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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