MEANS OF COMPLIANCE WITH TITLE 14 CFR, PART 23, SECTION 23.629, FLUTTER

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2004

Publisher

Federal Aviation Administration

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

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