GUIDANCE MATERIAL FOR 14 CFR SECTION 33.19, DURABILITY, FOR RECIPROCATING ENGINE REDESIGNED PARTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2004

Publisher

Federal Aviation Administration

1 PURPOSE
2 APPLICABILITY
3 RELATED REGULATIONS (CFR) AND READING MATERIAL
CHAPTER 1 INTRODUCTION
CHAPTER 2 GENERAL
CHAPTER 3 COMPLIANCE METHODS
APPENDIX 1 MATERIAL AND PROCESS CHANGES ON REDESIGNED
PARTS
APPENDIX 2 NOTES ON MATERIAL STRENGTH EVALUATION

Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate that redesigned parts for reciprocating engines comply with the requirements of section 33.19 of Title 14 of the Code of Federal Regulations (14 CFR).

DocumentType	Standard
Pages	19
PublisherName	Federal Aviation Administration
Status	Current

FAA 8110.4 : 2011	TYPE CERTIFICATION
FAA 8110.42 : 2014	PARTS MANUFACTURER APPROVAL PROCEDURES

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FAA AC 33.19-1 : 2004

GUIDANCE MATERIAL FOR 14 CFR SECTION 33.19, DURABILITY, FOR RECIPROCATING ENGINE REDESIGNED PARTS

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Abstract

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