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FAA AC 33-8 : 2009

FAA AC 33-8 : 2009

Current

Current

The latest, up-to-date edition.

GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2009

Publisher

Federal Aviation Administration

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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Hardcopy - English
PDF - English
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