Qualification testing of turbojet engine thrust reversers.

Bibliographic Details
Corporate Author:	United States. Federal Aviation Administration
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : Federal Aviation Administration, [1966]
Series:	Advisory circular ; AC no: AC 20-18A
Subjects:	Airplanes > Turbojet engines > Testing.
Online Access:	https://purl.fdlp.gov/GPO/LPS102945

Description
Item Description:	Cancels AC 20-18 . Title from PDF file caption (viewed Sept. 24, 2008). Electronic resource.
Physical Description:	3 pages : digital, PDF file.
Format:	Mode of access: Internet at the FAA web site. Address as of 9/24/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/dabaf7e4715bebb9862569ce00751bd3/$FILE/ac20-18a.pdf ; current access available via PURL.