33-5 - Turbine Engine Rotor Blade Containment/Durability
- Date Issued
- June 18, 1990
- Responsible Office
- Provides guidance and acceptable methods, but not the only methods, that may be used by an applicant in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).
- ac33-5.pdf (PDF, 828 KB)