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Guidance material for fatigue limit tests and composite blade fatigue substantiation.
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- Book
- Government document
- Author/Creator:
- United States. Federal Aviation Administration
- Series:
- United States. Federal Aviation Administration. Advisory circular ; AC 35.37-1 A.
- Advisory circular ; AC no. 35.37-1A
- Language:
- English
- Subjects (All):
- Propellers, Aerial--Fatigue--Testing.
- Propellers, Aerial.
- Physical Description:
- 1 online resource (25 pages)
- Place of Publication:
- [Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001]
- Notes:
- "9/17/01."
- AC 35.37-1, Composite Propeller Blade Fatigue Substantiation, dated 5/11/93, and AC 35.37-1, Change 1, dated 9/7/93, are cancelled.
- Title from PDF file caption (viewed December 12, 2008).
- OCLC:
- 281417750
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