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001 ocn277395381;

003 OCoLC;

005 20081210091438.0;

006 m d f ;

007 cr c||||||||||;

008 081210s2006 dcu o f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

074 a| 0431-A-27 (online);

086 0 a| TD 4.8/5:33-83 A;

110 1 a| United States.b| Federal Aviation Administration.=| ^A69774;

245 10 a| Turbine engine vibration test.;

260 a| [Washington, D.C.] :b| Federal Aviation Administration,c| [2006];

300 a| 8 p. :b| digital, PDF file;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| Advisory circular ;v| AC no. 33-83A;

500 a| "9/29/06.";

500 a| AC 33.83, dated February 14, 1997, is cancelled.;

538 a| Mode of access: Internet at the FAA web site. Address as of 12/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/0a7175bc942a34088625720b00584ad1/$FILE/AC33.83A.pdf; current access available via PURL.;

500 a| Title from PDF file caption (viewed Dec. 10, 2008).;

500 a| GPO Cataloging Record Distribution Program (CRDP).;

810 1 a| United States.b| Federal Aviation Administration.t| Advisory circular ;v| AC 33-83 A.=| ^A500611;

856 40 u| https://purl.fdlp.gov/GPO/LPS106315;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 1451315;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| MQ2799970l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 1/29/2009x| EDOCUMENTz| JERESOURCEo| .STAFF. 0;

Turbine engine vibration test.

Author/creator	United States
Format	Electronic
Publication Info	[Washington, D.C.] : Federal Aviation Administration, [2006]
Description	8 p. : digital, PDF file
Supplemental Content	https://purl.fdlp.gov/GPO/LPS106315
Subjects	Airplanes--Turbine-propeller engines. --Vibration. --Testing.

Series	Advisory circular ; AC no. 33-83A United States. Federal Aviation Administration. Advisory circular ; AC 33-83 A. ^A500611
General note	"9/29/06."
General note	AC 33.83, dated February 14, 1997, is cancelled.
General note	Title from PDF file caption (viewed Dec. 10, 2008).
General note	GPO Cataloging Record Distribution Program (CRDP).
Technical details	Mode of access: Internet at the FAA web site. Address as of 12/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/0a7175bc942a34088625720b00584ad1/$FILE/AC33.83A.pdf; current access available via PURL.
GPO item number	0431-A-27 (online)
Govt. docs number	TD 4.8/5:33-83 A

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	Electronic Resources	Access Content Online	✔ Available

Turbine engine vibration test.

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