Damage tolerance for high energy turbine engine rotors.

Damage tolerance for high energy turbine engine rotors.

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Bibliographic Details
Corporate author / creator:United States. Federal Aviation Administration.
Imprint:[Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2001]
Description:1 volume (various pagings) : digital, PDF file.
Language:English
Series:Advisory circular ; AC no. 33.14-1
United States. Federal Aviation Administration. Advisory circular ; AC 33.14-1.
Subject:
Airplanes -- Turbine-propeller engines -- Certification.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/7527035
Hidden Bibliographic Details
Notes:"1/8/01."
Title from PDF file caption (viewed Dec. 10, 2008).
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.
GPO item no.:0431-A-27 (online)
Govt.docs classification:TD 4.8/5:33.14-1

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