FAA AC 33.70-2 : 2009
Current
The latest, up-to-date edition.
DAMAGE TOLERANCE OF HOLE FEATURES IN HIGH-ENERGY TURBINE ENGINE ROTORS
Hardcopy , PDF
English
01-01-2009
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CHAPTER 1 - ENHANCED LIFE MANAGEMENT PROCESS
CHAPTER 2 - DAMAGE TOLERANCE ASSESSMENTS
CHAPTER 3 - "SOFT TIME INSPECTION" ROTOR LIFE MANAGEMENT
APPENDIX 1 - MANUFACTURING-INDUCED ANOMALY CALIBRATION TEST CASE
APPENDIX 2 - DEFAULT ANOMALY DISTRIBUTION CURVES
APPENDIX 3 - DEFAULT POD APPLICABILITY
APPENDIX 4 - DEFAULT POD CURVES
APPENDIX 5 - DEFINITION OF A HOLE FOR MANUFACTURING ANOMALY
ASSESSMENTS
APPENDIX 6 - MANUFACTURING CREDITS
APPENDIX 7 - SURFACE (MANUFACTURING INDUCTED ANOMALY) DAMAGE
TOLERANCE ASSESSMENT
Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in section 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts.
| DocumentType |
Standard
|
| Pages |
48
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| SAE AIR1537A | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
| FAA AC 33.70-1 : 2009 | GUIDANCE MATERIAL FOR AIRCRAFT ENGINE LIFE-LIMITED PARTS REQUIREMENTS |
| FAA AC 33-3 : 0 | TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES |
| SAE AIR4003 | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
| FAA AC 33.14-1 : 0 | DAMAGE TOLERANCE FOR HIGH ENERGY TURBINE ENGINE ROTORS |
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