FAA AC 25-24 : 0
Current
The latest, up-to-date edition.
SUSTAINED ENGINE IMBALANCE
Hardcopy , PDF
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 |
| SAE ARP 986 : 2015 | GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.