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008 081204s2000 dcu o f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

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

086 0 a| TD 4.8/5:25.905-1;

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

245 10 a| Minimizing the hazards from propeller blade and hub failures.;

260 a| [Washington, D.C.] :b| U.S. Dept. of Transportation, Federal Aviation Administration,c| [2000];

300 a| 7 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. 25.905-1;

500 a| "9/27/00.";

538 a| Mode of access: Internet at the FAA web site. Address as of 12/4/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/0a7294b17805f84e862569b300547865/$FILE/ATTQ3W92/AC25-905-1.pdf; current access available via PURL.;

500 a| Title from PDF file caption (viewed Dec. 4, 2008).;

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

650 0 a| Airplanesx| Turbine-propeller enginesx| Risk assessment.=| ^A439489;

810 1 a| United States.b| Federal Aviation Administration.t| Advisory circular ;v| AC 25.905-1.=| ^A500611;

856 40 u| https://purl.fdlp.gov/GPO/LPS106069;

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

596 a| 1;

998 a| 1451075;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| MQ2799730l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 1/29/2009x| EDOCUMENTz| JERESOURCEo| .STAFF. 0;

Minimizing the hazards from propeller blade and hub failures.

Author/creator	United States
Format	Electronic
Publication Info	[Washington, D.C.] : U.S. Dept. of Transportation, Federal Aviation Administration, [2000]
Description	7 p. : digital, PDF file
Supplemental Content	https://purl.fdlp.gov/GPO/LPS106069
Subjects	Airplanes--Turbine-propeller engines. --Risk assessment.

Series	Advisory circular ; AC no. 25.905-1 United States. Federal Aviation Administration. Advisory circular ; AC 25.905-1. ^A500611
General note	"9/27/00."
General note	Title from PDF file caption (viewed Dec. 4, 2008).
General note	GPO Cataloging Record Distribution Program (CRDP).
Technical details	Mode of access: Internet at the FAA web site. Address as of 12/4/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/0a7294b17805f84e862569b300547865/$FILE/ATTQ3W92/AC25-905-1.pdf; current access available via PURL.
GPO item number	0431-A-27 (online)
Govt. docs number	TD 4.8/5:25.905-1

Minimizing the hazards from propeller blade and hub failures.

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