25-24 - Sustained Engine Imbalance
- Date Issued
- August 02, 2000
- Responsible Office
- ANM-100, Aircraft Certification Service, Transport Airplane Directorate
- Sets forth an acceptable means, but not the only means, of demonstrating compliance with the provisions of 14 CFR Part 25 related to the aircraft design for sustained engine rotor imbalance conditions. While these guidelines are not mandatory, they are derived from extensive Federal Aviation Administration (FAA) and industry experience in determining compliance with the pertinent Federal Aviation Regulations (FAR).
- AC 25-24 (PDF, 58 KB)