Calibration test endurance test and teardown inspection for turbine engine certification ([sections] 33.85, 33.87, 33.93).

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : Federal Aviation Administration, [2006]
Series:	Advisory circular ; AC no. 33.87-1
Subjects:	Airplanes > Turbine-propeller engines > Stability > Certification.
Online Access:	https://purl.fdlp.gov/GPO/LPS106474

Description
Item Description:	"4/13/06." Title from PDF file caption (viewed Dec. 12, 2008). Electronic resource.
Physical Description:	1 volume (various pagings) : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 12/12/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/d38be5d0c09c0a868625716b00668044/$FILE/33.87-1.pdf ; current access available via PURL.