Turbo Prop Engines/(t56) Parts

(Page 8) End item NSN parts page 8 of 9
Part Number
NSN
NIIN
6799323 Pyrometer And Thermocoupl Tester
008843885
6799327 Aircraft Engine Test Set
009748221
6799449 Engine Adapter
000217164
6799514 Mounting Adapter
000137325
6799535 Spanner Wrench Assembly
010601478
6799537 Dimpling Fixture
010594526
6799596 Aircr Engine Maintenance Fixture
000137420
6799621 Wrench
007571819
6799641 Pusher
007571841
6799642 Bearing And Inserter And Remover
007571851
6799708 Aircr Engine Maintenance Fixture
007522760
6799754 Puller
007571856
6799760 Puller
006861564
6799768 Retaining Plate
000184538
6799819 Aircraft Co Test Set Subassembly
007981346
6799863 Aircraft Maintenance Drill Jig
009391502
6799876 Aircraft Engine Test Set
008687143
6799877 Cable Assembly
008698044
6799878 Cable Assembly
008781248
6799902 Bearing And Puller
009081751
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Turbo Prop Engines/(t56)

Picture of Turbo Prop Engines/(t56)

The General Electric T64 is a free-turbine turboshaft engine that was originally developed for use on helicopters, but which was later used on fixed-wing aircraft as well. General Electric introduced the engine in 1964. The original engine design included technical innovations such as corrosion resistant and high-temperature coatings. Although the compressor is all-axial, like the earlier General Electric T58, the power turbine shaft is coaxial with the HP shaft and delivers power to the front of the engine, not rearwards. Fourteen compressor stages are required to deliver the required overall pressure ratio. Compressor handling is facilitated by 4 rows of variable stators. Unlike the T58, the power turbine has 2 stages.

Later versions of the engine produce from 3,925 to 4,750 shp (2,927 to 3,542 kW).

The engine was designed to accommodate different gearboxes or shaft drives, for helicopter or turboprop fixed-wing applications. The engine could be operated continuously at angles between 100 degrees upward and 45 degrees downward for STOL or helicopter applications.

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