CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2008

Publisher

Federal Aviation Administration

1. PURPOSE
2. APPLICABILITY
3. CANCELLATION
4. RELATED REGULATIONS AND DOCUMENTS
5. BACKGROUND
6. SUPPLEMENTAL STRUCTURAL INSPECTION PROGRAMS
7. REPAIRS, ALTERATIONS, AND MODIFICATIONS
8. MANDATORY MODIFICATION PROGRAM
9. CORROSION PREVENTION AND CONTROL PROGRAM
10. REPAIR ASSESSMENT PROGRAM
11. Widespread Fatigue Damage
APPENDIX 1 - GUIDELINES FOR DEVELOPING A SUPPLEMENTAL
STRUCTURAL INSPECTION DOCUMENT

Provides guidance material to design approval holders and operators for use in developing a damage tolerance based supplemental structural inspection program (SSIP) for older airplanes.

DocumentType	Standard
Pages	13
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 91-81 : 2008	FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE
FAA AC 120-77 : 0	MAINTENANCE AND ALTERATION DATA
FAA AC 129-4 : 2009	MAINTENANCE PROGRAMS FOR U.S.-REGISTERED AIRCRAFT OPERATED UNDER 14 CFR PART 129
FAA AC 120-104 : 2011	ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE
FAA AC 91-82 : 2012	FATIGUE MANAGEMENT PROGRAMS FOR IN-SERVICE ISSUES
FAA AC 25.571-1 : 2011	DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE

FAA AC 120-73 : 0	DAMAGE TOLERANCE ASSESSMENT OF REPAIRS TO PRESSURIZED FUSELAGES
FAA AC 25.571-1 : 2011	DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE

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FAA AC 91-56 : 2008

CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES

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Abstract

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