AC 33.70-1 Guidance Material for Aircraft Engine Life-Limited Parts
33.70-1 – Guidance Material for Aircraft Engine Life-Limited Parts Requirements
July 31, 2009
AIR-600, Policy and Innovation Division
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of § 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33). Section 33.70 contains requirements applicable to the design and life management of propulsion system life-limited parts including high-energy rotating parts.
AC 33.70-1 – including Change 1 (PDF, 187 KB)
AC 33.70-1.pdf (PDF, 107 KB)