FAA AC 33-8 : 2009
Current
The latest, up-to-date edition.
GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION
Hardcopy , PDF
English
01-01-2009
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1. Purpose
2. Applicability
3. Related References
4. Background
5. Part Criticality
6. Comparative Test and Analysis Method
7. Reverse Engineering Considerations
8. Continued Operational Safety
9. Part Numbering
APPENDIX 1 - FAILURE MODES AND EFFECTS ASSESSMENT
APPENDIX 2 - TEMPLATES
APPENDIX 3 - REVERSE ENGINEERING DESIGN PROCESS
APPENDIX 4 - CONTINUED OPERATIONAL SAFETY
Gives guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval (PMA).
| DocumentType |
Standard
|
| Pages |
161
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33-10 : 2014 | STATISTICAL ANALYSIS CONSIDERATIONS FOR COMPARATIVE TEST AND ANALYSIS BASED COMPLIANCE FINDINGS FOR TURBINE ENGINE AND AUXILIARY POWER UNIT REPLACEMENT, REDESIGN AND REPAIRED PARTS |
| FAA AC 21-9 : 2010 | MANUFACTURERS REPORTING FAILURES, MALFUNCTIONS, OR DEFECTS |
| FAA AC 39-8 : 0 | CONTINUED AIRWORTHINESS ASSESSMENTS OF POWERPLANT AND AUXILIARY POWER UNIT INSTALLATIONS OF TRANSPORT CATEGORY AIRPLANES |
| FAA AC 21-1 : 0 | PRODUCTION CERTIFICATES |
| FAA 8110.42 : 2014 | PARTS MANUFACTURER APPROVAL PROCEDURES |
| FAA 8110.37 : 2011 | DESIGNATED ENGINEERING REPRESENTATIVE (DER) HANDBOOK |
| FAA 8120.2 : 2010 | PRODUCTION APPROVAL AND CERTIFICATE MANAGEMENT PROCEDURES |
| FAA 8150.1 : 2017 | TECHNICAL STANDARD ORDER PROGRAM |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
| FAA AC 33.75-1 : 2007 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS |
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