FAA AC 20-66:2011

FAA AC 20-66:2011 Propeller Vibration And Fatigue Gives guidance and describes one method, but not the only method, for demonstrating compliance with Section 23.907 and 25.907 of Title 14 of the Code of Federal Regulations, for the evaluation of vibr

More details

Download

PDF AVAILABLE FORMATS IMMEDIATE DOWNLOAD
$17.60 tax incl.

$40.00 tax incl.

(price reduced by 56 %)

1000 items in stock

Table of Contents

1.Purpose
2.Applicability
3.Cancellation
4.RelatedDocuments
5.Definitions
6.Discussion
7.VibrationTests
8.StressPeaksandResonantConditions
9.PropellerFlutter
10.Similarity
11.Note9VibrationApprovals
12.PropellerFatigueEvaluation
13.AirplaneandPropellerOperatingandAirworthiness
Limitations
Appendix1-TablesandFigures
Appendix2-PropellerVibrationBackgroundInformation
Appendix3-PropellerVibrationEvaluationTestConditions

Abstract

Gives guidance and describes one method, but not the only method, for demonstrating compliance with Section 23.907 and 25.907 of Title 14 of the Code of Federal Regulations, for the evaluation of vibration stresses on propellers installed on airplanes.

Contact us