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

(Page 44) End item NSN parts page 44 of 51
Part Number
NSN
NIIN
182941PIECE256D Fluid Filter Element
002173588
1850-915BS-3 Reciprocating Pump
000866940
185762 Retaining Ring
002056566
1865950 Electrical Connector Cover
002386419
1866-1346 ITEM 32 Packing Retainer
001715042
187-17222 Bearing Ball
001519206
189331 Tube Coupling Nut
000373100
189561 Machine Screw
001509212
18C614 Hexagon Head Cap Screw
002693235
18GA246338 Electrical Wire
006359867
190000 PC 12 O-ring
001651943
190000 PC 5 O-ring
001675115
19012 O-ring
003303307
190518195 Packing Retainer
001716758
190572 Socket Head Cap Screw
002074017
190772 Machine Bolt
007543049
190927 Socket Head Cap Screw
000680543
190939 Serrated Lock Ring
004057576
Page: 44 ...

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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