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

(Page 15) End item NSN parts page 15 of 51
Part Number
NSN
NIIN
10124953 Socket Head Cap Screw
000685398
10125514 Machine Screw
008132791
10125515 Machine Screw
008132796
10125755 O-ring
003520321
10129561 O-ring
005840150
10129569 O-ring
002920578
10130560 Bearing Ball
001519206
10130562 Needle Roller Bearing
009021641
10131951 Electrical Connector Cable Clamp
011816652
10132135 Lug Terminal
001138190
10132666 Electromagnetic Relay
012076456
10134041 Electrical Insulation Sleeving
008715779
10138290 O-ring
008223691
10138421 Nonrechargeable Battery
009857846
10139438 Electrical Contact
010413754
10150606 Laminated Shim Stock
005805467
10154150 Retaining Ring
009037567
10158778 Cam Control Shim
002941239
10159518 Self-aligning Plain Bearing
005285336
10159664 Machine Bolt
001133769
Page: 15 ...

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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