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FAA AC 25-24 : 0

Current
Current

The latest, up-to-date edition.

SUSTAINED ENGINE IMBALANCE
Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 RELATED DOCUMENTS
3 DEFINITIONS
4 BACKGROUND
5 EVALUATION OF THE WINDMILLING IMBALANCE CONDITIONS
6 ANALYSIS METHODOLOGY
7 MATHEMATICAL MODELING
8 VALIDATION
9 HIGH POWER IMBALANCE CONDITION

Gives 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.

DocumentType
Standard
Pages
13
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
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FAA AC 25.571-1 : 2011 DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE

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PDF - English
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