FAA AC 91-56 : 2008
Current
The latest, up-to-date edition.
CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES
Hardcopy , PDF
English
01-01-2008
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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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