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

(Page 37) End item NSN parts page 37 of 51
Part Number
NSN
NIIN
155-S5-12D Quick Disconnect Coupling Half
005401268
155090 Packing Retainer
001715074
155172-102 Socket Head Cap Screw
000685398
15524 Tapered Roller Cone And Rollers
001982169
15525-12D Quick Disconnect Coupling Half
005401268
155643 Packing Retainer
001715889
1557052-25 O-ring
005840150
155S5-12D Quick Disconnect Coupling Half
005401268
155S512D Quick Disconnect Coupling Half
005401268
156 ITEM 2 Tube Fitting Clinch Sleeve
005547398
156-4 Nonmetallic Hose
005419281
156/102 Boss Reducer
007200233
156/16 Tube Fitting Clinch Sleeve
002898619
156/2 Tube Fitting Clinch Sleeve
005547398
156/6 Hexagon Plain Nut
006382605
15600-02 Plate Self-locking Nut
007280945
156080A Electrical Insulation Tape
008127387
15635-118 Ear Cushion
007156158
156372 Dial Indicating Pressure Gage
008129169
Page: 37 ...

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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