Model: 37C300055P102
Turbine Engine Cooling PlateSpecial Features:
Stage 1
Properties:
An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine.
Part 37C300055P102 NSN 2840-01-532-6325
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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