gas path / gas path parts / base metal integrity / turbine section gas path parts / base metal structure / combustion device / chemical mechanisms / gas streams / temperature measuring devices / diluted and atomized sea salt solution / hot gas stream / actual part processing / gas stream / continuous chemical reaction / turbine devices / exhaust gas / gas flow constituents / turbine section gas path replacement parts / coated metal / chemical reaction / engine core gas stream / exhaust gas temperature / gas path constituents / internal gas pressure / base metal surface / base metal degradation / manufacturing processes / base metal / exhaust gas velocity / /
Organization
Federal Aviation Administration / National Aeronautics and Space Administration / Propeller Directorate Aircraft Certification Service / U.S. Department of Transportation / /
Person
Turbine Engine / / /
Position
representative / D’Alessandro Assistant Manager / AIR Directives Management Officer / Colleen M. D’Alessandro Assistant Manager / /
AC[removed]Oxidation, Hot Corrosion, Thermal Fatigue, and Erosion Characteristics Testing to Support 14 CFR, Part 33, § 33.15, Compliance for Turbine Engines