Guidance material for fatigue limit tests and composite blade fatigue substantiation.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001]
Series:	Advisory circular ; AC no. 35.37-1A
Subjects:	Propellers, Aerial > Fatigue > Testing.
Online Access:	https://purl.fdlp.gov/GPO/LPS106486

Description
Item Description:	"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 Dec. 12, 2008). Electronic resource.
Physical Description:	25 pages : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/12/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/e11577f6cfa979ba86256acd00707c57/$FILE/ac35.37-1a.pdf ; current access available via PURL.