Damage tolerance for high energy turbine engine rotors.

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. 33.14-1
Subjects:	Airplanes > Turbine-propeller engines > Certification.
Online Access:	https://purl.fdlp.gov/GPO/LPS106376

Description
Item Description:	"1/8/01." Title from PDF file caption (viewed Dec. 10, 2008). Electronic resource.
Physical Description:	1 volume (various pagings) : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/fcb8e6cc06307a3c86256a84005b21ba/$FILE/ac33.14-1.pdf ; current access available via PURL.