Turbine and compressor rotors type certification substantiation procedures.

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, [1968]
Series:	Advisory circular ; AC no. 33-3
Subjects:	Airplanes > Turbine-propeller engines > Design and construction > Certification.
Online Access:	https://purl.fdlp.gov/GPO/LPS106279

Description
Item Description:	"9/9/68." AC 20-26 effective July 22, 1964, and Changes 1 and 2 effective September 18, 1964, and July 8, 1965, respectively, are cancelled. Title from PDF file caption (viewed Dec. 9, 2008). Electronic resource.
Physical Description:	8 unnumbered pages : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/9/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/df1cf66a78bff89b862569b300547d71/$FILE/AC33-3.pdf ; current access available via PURL.