FAA AC 23.629-1 : 2004
Current
The latest, up-to-date edition.
MEANS OF COMPLIANCE WITH TITLE 14 CFR, PART 23, SECTION 23.629, FLUTTER
Hardcopy , PDF
English
01-01-2004
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CHAPTER 1 METHODS OF SUBSTANTIATION
1 Ground Tests for Dynamically Similar Aircraft
2 Rational Analysis with Flight Flutter Tests
3 Rigidity and Mass Balance Criteria (Simplified
Criteria) with Flight Flutter Test
4 Whirl Mode
CHAPTER 2 MODIFICATIONS TO AIRCRAFT ALREADY CERTIFICATED
5 Re-evaluation
CHAPTER 3 CONTROL SURFACES AND TABS
6 Response
7 Balance
8 Vibratory Modes
9 Analyses
10 Fail Safe Requirements
CHAPTER 4 DIVERGENCE AND CONTROL REVERSAL
11 General
12 Airfoil Divergence
13 Control Reversal
APPENDIXES
APPENDIX 1 GROUND TESTING
APPENDIX 2 FLIGHT FLUTTER TESTING
APPENDIX 3 ACKNOWLEDGMENTS, REFERENCES, BIBLIOGRAPHY
Provides information and guidance to provide one means, but not the only means of complying with section 23.629, Flutter (including divergence, and control reversal) of part 23 of the Federal Aviation Regulations.
| DocumentType |
Standard
|
| Pages |
32
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 23-19 : 2007 | AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 20-73 : 2006 | AIRCRAFT ICE PROTECTION |
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