Minimizing the hazards from propeller blade and hub failures.

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, [2000]
Series:	Advisory circular ; AC no. 25.905-1
Subjects:	Airplanes > Turbine-propeller engines > Risk assessment.
Online Access:	https://purl.fdlp.gov/GPO/LPS106069

Description
Item Description:	"9/27/00." Title from PDF file caption (viewed Dec. 4, 2008). Electronic resource.
Physical Description:	7 pages : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/4/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/0a7294b17805f84e862569b300547865/$FILE/ATTQ3W92/AC25-905-1.pdf ; current access available via PURL.