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

Available Online