FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2008

Publisher

Federal Aviation Administration

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 91-60 : 0

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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

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FAA AC 91-81 : 2008

FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE

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Abstract

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