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FAA 8110.42 : 2014

Current

Current

The latest, up-to-date edition.

PARTS MANUFACTURER APPROVAL PROCEDURES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

€35.89
Excluding VAT

CHAPTER 1 - PURPOSE, ADMINISTRATIVE INFORMATION
            AND BACKGROUND
CHAPTER 2 - AIRCRAFT CERTIFICATION OFFICE (ACO)
            RESPONSIBILITIES
CHAPTER 3 - MANUFACTURING INSPECTION DISTRICT
            OFFICE (MIDO) RESPONSIBILITIES
CHAPTER 4 - DESIGNATED ENGINEERING REPRESENTATIVES
            AND ORGANIZATION DESIGNATION AUTHORIZATION
APPENDIX A - PMA PROCESS FLOWCHARTS
APPENDIX B - PART SPECIFIC CERTIFICATION PLAN
APPENDIX C - LIST OF FAA MANUFACTURING INSPECTION
             DISTRICT/SATELLITE OFFICES
APPENDIX D - SAMPLE FAA-PMA SUPPLEMENT FOR IDENTICALITY
             (NON-LICENSING AGREEMENT) OR TEST AND
             COMPUTATION
APPENDIX E - SAMPLE DESIGN REJECTION LETTER
APPENDIX F - SAMPLE NOTIFICATION LETTER OF DESIGN
             APPROVAL
APPENDIX G - FORM 8110-3, TEST AND COMPUTATION
             (GENERAL ANALYSIS)
APPENDIX H - FORM 8110-3, TEST AND COMPUTATION
             (COMPARATIVE ANALYSIS)
APPENDIX I - EXAMPLE OF FAA FORM 8110-3 FOR
             IDENTICALITY
APPENDIX J - LIST OF ACRONYMS
APPENDIX K - DEFINITIONS AND TERMS
APPENDIX L - RELATED PUBLICATIONS AND HOW TO
             GET THEM
APPENDIX M - ADMINISTRATIVE INFORMATION
APPENDIX N - FAA FORM 1320-19 DIRECTIVES FEEDBACK
             INFORMATION

Specifies the responsibilities and procedures for approving replacement and modification articles for installation on type-certificated products.

DevelopmentNote
Supersedes FAA N 8110.54, FAA N 8110.55 and FAA N 8120.17. (07/2003)
DocumentType
Standard
Pages
41
PublisherName
Federal Aviation Administration
Status
Current
Supersedes

FAA N 8110.79 : 0 GUIDELINES FOR THE APPROVAL OF FIELD-LOADABLE SOFTWARE BY FINDING IDENTICALITY THROUGH THE PARTS MANUFACTURER APPROVAL PROCESS
FAA 8110.105 : 2017 SIMPLE AND COMPLEX ELECTRONIC HARDWARE APPROVAL GUIDANCE
FAA AC 21-51 : 2011 APPLICANTS SHOWING OF COMPLIANCE AND CERTIFYING STATEMENT OF COMPLIANCE
FAA AC 20-184 : 2015 GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
FAA AC 33.83-1 : 2009 COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS
FAA AC 21-55 : 2016 PROCESS TO SUPPORT FAA FINDINGS OF UNDUE BURDEN OR NO UNDUE BURDEN FOR PAHS REQUESTING TO USE A MANUFACTURING FACILITY LOCATED OUTSIDE OF THE UNITED STATES
FAA AC 20-161 : 2008 AIRCRAFT ONBOARD WEIGHT AND BALANCE SYSTEMS
FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
FAA IR 01-01 : 0 AIRCRAFT CERTIFICATION GUIDE FOR THE USE OF ELECTRONIC TECHNOLOGY AND ALTERNATIVE METHODS OF STORING INFORMATION
FAA 8110.104 : 2007 RESPONSIBILITIES AND REQUIREMENTS FOR IMPLEMENTING PART 26 SAFETY INITIATIVES
FAA AC 33.19-1 : 2004 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.19, DURABILITY, FOR RECIPROCATING ENGINE REDESIGNED PARTS
FAA AC 20-142 : 2010 ELIGIBILITY AND EVALUATION OF U.S. MILITARY SURPLUS FLIGHT SAFETY CRITICAL AIRCRAFT PARTS, ENGINES, AND PROPELLERS
FAA 8110.4 : 2011 TYPE CERTIFICATION
SAE ARP 1619 : 2016 REPLACEMENT AND MODIFIED BRAKES AND WHEELS
FAA AC 33-8 : 2009 GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION
FAA AC 00-56 : 2015 VOLUNTARY INDUSTRY DISTRIBUTOR ACCREDITATION PROGRAM
FAA AC 43-18 : 2011 FABRICATION OF AIRCRAFT PARTS BY MAINTENANCE PERSONNEL
FAA 8110.54 : 2010 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS
FAA AC 23-27 : 2009 PARTS AND MATERIALS SUBSTITUTION FOR VINTAGE AIRCRAFT
FAA 8100.15 : 2013 ORGANIZATION DESIGNATION AUTHORIZATION PROCEDURES
FAA AC 21-31 : 2010 QUALITY CONTROL FOR THE MANUFACTURE OF NON-METALLIC COMPARTMENT INTERIOR COMPONENTS
FAA AC 21-23 : 2004 AIRWORTHINESS CERTIFICATION OF CIVIL AIRCRAFT, ENGINES, PROPELLERS, AND RELATED PRODUCTS IMPORTED TO THE UNITED STATES
FAA AC 33.87-2 : 2009 COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS

MIL-STD-1916 Base Document:1996 DOD PREFERRED METHODS FOR ACCEPTANCE OF PRODUCT

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