Turbo Prop Engines/(t56) Parts

End item NSN parts page 1 of 9
Part Number
NSN
NIIN
032505J0086 Nonmetallic Hose Assembly
002589949
032505J0086F Nonmetallic Hose Assembly
002589949
090V999021J0150 Nonmetallic Hose Assembly
000047015
10-0008-001 Pressure Temperature Sensor
013126226
102-736 Pump Diaphragm Assembly
008773760
110563 Fueling Manifold
013262415
11452 Check Valve
005929949
118586 Oil Filter Plug
003325312
124002-10CR0086 Nonmetallic Hose Assembly
002589949
124012E0150C150 Nonmetallic Hose Assembly
001488638
1241102-4CR0077 Nonmetallic Hose Assembly
004431521
1241102-6CR0126 Nonmetallic Hose Assembly
006142502
1241706E-0161C90 Nonmetallic Hose Assembly
002270457
1241706E0161C90 Nonmetallic Hose Assembly
002270457
124F002-10CR-0086 Nonmetallic Hose Assembly
002589949
124F003-4CR0084 Nonmetallic Hose Assembly
002582655
13000204-0077 Nonmetallic Hose Assembly
004431521
13000206-0126 Nonmetallic Hose Assembly
006142502
190585-1 Solenoid Valve
005402106
1X12HG-227 Turnbuckle
014289935
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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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