AC 33-11
Current · Issued 2014-09-23 · OPR ANE-111 · Series 33
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
Sections this AC references
Document overview FAA Dynamic Regulatory System (DRS) fields · full body text 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
- Office
- AIR-620: Technical Innovation Policy Branch
- Referenced 14 CFR Parts
- Part 33
- Referenced sections
- Sec. 33.15