FAA AC 91-81 : 2008
Current
The latest, up-to-date edition.
FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE
Hardcopy , PDF
English
01-01-2008
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. PURPOSE
2. CANCELLATION
3. RELATED REGULATIONS
4. DEFINITIONS
5. APPLICABILITY
6. RELATED PUBLICATIONS (current editions)
7. BACKGROUND
8. APPLICATION OF CERTIFICATION REQUIREMENTS TO UNSAFE
CONDITIONS
9. OVERVIEW OF FATIGUE MANAGEMENT SYSTEM
10. DEVELOPING AN FMP
11. COORDINATION AND APPROVALS
12. IMPLEMENTING AN FMP
13. LIST OF ACRONYMS
APPENDIX 1. DETERMINATION OF DEMONSTRATED RISK OF CATASTROPHIC
FAILURE DUE TO FATIGUE
APPENDIX 2. METHODOLOGY FOR DETERMINING REPEAT INSPECTION
INTERVALS
Provides guidance on developing and implementing a Fatigue Management Program (FMP).
| DevelopmentNote |
Supersedes FAA AC 91-60. (05/2008)
|
| DocumentType |
Standard
|
| Pages |
38
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| Supersedes |
| FAA AC 43-18 : 2011 | FABRICATION OF AIRCRAFT PARTS BY MAINTENANCE PERSONNEL |
| FAA AC 23-13 : 2005 | FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| FAA AC 21-40 : 2007 | GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE |
| FAA AC 43-4 : A | CORROSION CONTROL FOR AIRCRAFT |
| FAA AC 91-56 : 2008 | CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
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.