Turbine engine rotor blade containment/durability.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, [1990]
Series:	Advisory circular ; AC no. 33-5
Subjects:	Airplanes > Turbine-propeller engines > Design and construction. Airplanes > Turbojet engines > Blades.
Online Access:	https://purl.fdlp.gov/GPO/LPS106292

Description
Item Description:	"06/18/90." Title from PDF file caption (viewed Dec. 9, 2008). Electronic resource.
Physical Description:	5 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/eab0330a3c7a22eb862569b3005d6ace/$FILE/ac33-5.pdf ; current access available via PURL.