Turbine engine continued rotation and rotor locking.

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, [2003]
Series:	Advisory circular ; AC no. 33.74/92-1A
Subjects:	Airplanes > Turbine-propeller engines > Safety regulations.
Online Access:	https://purl.fdlp.gov/GPO/LPS106427

Description
Item Description:	"07/23/03." Title from PDF file caption (viewed Dec. 11, 2008). Electronic resource.
Physical Description:	6 pages : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/11/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/c3a93f3072f4f18486256d730043fb00/$FILE/AC33.74-92-1A.pdf ; current access available via PURL.