Federal Aviation Administration

AC 35.37-1A (Cancelled) - Guidance Material for Fatigue Limit Tests and Composite Blade Fatigue Substantiation

Document Information

35.37-1A - Guidance Material for Fatigue Limit Tests and Composite Blade Fatigue Substantiation (Cancelled)

Cancellation Notes
35.37-1B
Date Cancelled
March 24, 2011
Date Issued
September 17, 2001
Responsible Office
ANE-110
Description

Provides guidance and describes methods, but not the only methods, for demonstrating compliance with 35.37. The AC also provides methods for the fatigue evaluation of propellers and the fatigue substantiation of composite propeller blades.

Cancels

Page Last Modified: 06/17/10 15:21 EDT

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