35.37-1B - Propeller Fatigue Limits and Evaluation
- Date Issued
- March 24, 2011
- Responsible Office
- ANE-111, Aircraft Certification Service Engine & Propeller Directorate - Rulemaking & Policy
This advisory circular (AC) provides guidance and describes methods, but not the only methods, for demonstrating compliance with § 35.37, Propeller fatigue limits and evaluation, of Title 14 of the Code of Federal Regulations (14 CFR).
- AC 35.37-1B (PDF, 87 KB)