Model: 6068T36P04
Turbine Engine Cooling PlateSpecial Features:
72-41-00 rotor assembly-stages 1 and 2 low stress gas generator turbine, plate stage 2 turbine aft cooling, this item has replaced 6068t36p01.
Properties:
An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine.
Part 6068T36P04 NSN 2840-01-612-0143
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPricing & Availability Check
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Schedule B and Export
- Schedule B: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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