FAA AC 33.19-1 : 2004
Current
The latest, up-to-date edition.
GUIDANCE MATERIAL FOR 14 CFR SECTION 33.19, DURABILITY, FOR RECIPROCATING ENGINE REDESIGNED PARTS
Hardcopy , PDF
English
01-01-2004
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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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