Document Information
- Number
- 33-5
- Title
- Turbine Engine Rotor Blade Containment/Durability
- Status
- Active
- Date issued
- 1990-06-18
- Office of Primary Responsibility
- ANE-110
- Description
- 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).
- Content
-
- AC 33-5 (PDF)