FAA AC 25-24 : 0
Current
The latest, up-to-date edition.
SUSTAINED ENGINE IMBALANCE
Hardcopy , PDF
English
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 |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
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