FAA · Advisory Circular
Oxidation, Hot Corrosion, Thermal Fatigue, and Erosion Characteristics Testing to Support 14 CFR, Part 33, § 33.15, Compliancefor Turbine Engines
14 CFR Parts this AC applies to
Derived from the AC's subject series via the FAA's published numbering scheme.
Sections this AC references
Sections explicitly named in the AC number or title — round-trip back to each one.
Document overview
Structured fields from the FAA Dynamic Regulatory System (DRS). Full body text lives in the linked PDF.
- Subject
- Oxidation, Hot Corrosion, Thermal Fatigue, and Erosion Characteristics Testing to Support 14 CFR, Part 33, 33.15, Compliance for Turbine Engines
- Status
- Current
- Office
- AIR-620: Technical Innovation Policy Branch
- Referenced 14 CFR Parts
- Part 33
- Referenced sections
- Sec. 33.15