FAA 8110.52 : 2017
Current
The latest, up-to-date edition.
TYPE VALIDATION AND POST-TYPE VALIDATION PROCEDURES
Hardcopy , PDF
English
01-01-2017
Chapter 1 - General
Chapter 2 - Validation Policy
Chapter 3 - FAA Validation
Chapter 4 - Obtaining Foreign Authority Approval/Acceptance
of U.S. Products and Changes to U.S. Products
Chapter 5 - Continued Airworthiness
Chapter 6 - Administrative Information
Appendix A - Validation Project Flow Charts
Appendix B - Acronyms
Appendix C - Definitions and Terms
Appendix D - Sample Project Specific Validation Plan (PSVP)
Appendix E - Sample Validation Application Rejection Letter
Appendix F - Sample Outbound Project Checklist
Appendix G - Sample Validation Approval Notification Letter
Appendix H - Sample FAA Certifying Statement Letter
Appendix I - Related Publications and How to Get Them
Appendix J - FAA Form 1320-19, Directive Feedback Information
Describes the policy and procedures to issue a validated type certificate (TC) for a product (aircraft, aircraft engine, or propeller) or a validated supplemental type certificate (STC) for a change to a product, as well as approve any follow-on changes to these certificates, when the United States is not the State of Design (SoD).
| DocumentType |
Standard
|
| Pages |
62
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA 8110.106 : 2009 | ASSESSING THE RELATIVE RISK OF TITLE 14 CFR PARTS |
| FAA AC 23-11 : 2009 | 14 CFR PART 23 TYPE CERTIFICATION OF AN AIRPLANE ORIGINALLY CERTIFICATED TO EUROPEAN AVIATION SAFETY AGENCY (EASA) (CS-VLA) STANDARDS OR JOINT AVIATION REQUIREMENTS - VERY LIGHT AIRPLANE (JAR-VLA) |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
| MIL-STD-1916 Base Document:1996 | DOD Preferred Methods for Acceptance of Product |
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