Turbine engine foreign object ingestion and rotor blade containment type certification procedures.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : Department of Transportation, Federal Aviation Administration, [1970]
Series:	Advisory circular ; AC no. 33-1 B
Subjects:	Airplanes > Turbofan engines > Safety measures.
Online Access:	https://purl.fdlp.gov/GPO/LPS106269

Available Online