Model: 1-190-008-02
Aircraft Gas Turbine Rotor BladeSpecial Features:
Nickel alloy m3602 fscm 91547, rockwell c scale 35 min, 40 max hardness, 0.988 in. Min, 0.991 in. Max o/a w
Properties:
An item mounted on a disk, turbine, aircraft gas turbine engine. it is designed to create the flow of air in the turbine section of an engine, gas turbine, aircraft.
Part 1-190-008-02 NSN 2840-00-971-6287
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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