Model: 1993M68G01
Aircraft Tu Turbine Blade DamperProperties:
A device used to reduce high cycle fatigue on a blade, turbine rotor, aircraft gas turbine engine. it also acts as a seal. it may be of various shapes and cross sections.
Part 1993M68G01 NSN 2840-01-590-9067
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsFreight Classification
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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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