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LEADER 01883cam 2200397Ia 4500

001 ocn277237601;

003 OCoLC;

005 20081209144316.0;

006 m d f ;

007 cr m||||||||||;

008 081209s1990 dcua o f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

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

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

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

245 10 a| Turbine engine rotor blade containment/durability.;

260 a| Washington, D.C. :b| U.S. Dept. of Transportation, Federal Aviation Administration,c| [1990];

300 a| 5 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. 33-5;

500 a| "06/18/90.";

538 a| Mode of access: Internet at the FAA web site. Address as of 12/9/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/eab0330a3c7a22eb862569b3005d6ace/$FILE/ac33-5.pdf; current access available via PURL.;

500 a| Title from PDF file caption (viewed Dec. 9, 2008).;

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

650 0 a| Airplanesx| Turbine-propeller enginesx| Design and construction.=| ^A439489;

650 0 a| Airplanesx| Turbojet enginesx| Blades.=| ^A452517;

776 0 a| United States. Federal Aviation Administration.t| Turbine engine rotor blade containment/durabilityh| 5 p.w| (OCoLC)29643011;

810 1 a| United States.b| Federal Aviation Administration.t| Advisory circular ;v| AC 33-5.=| ^A500611;

856 40 u| https://purl.fdlp.gov/GPO/LPS106292;

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

596 a| 1;

998 a| 1451300;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| MQ2799955l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 1/29/2009x| EDOCUMENTz| JERESOURCEo| .STAFF. 0;

Turbine engine rotor blade containment/durability.

Author/creator	United States
Format	Electronic
Publication Info	Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, [1990]
Description	5 p. : digital, PDF file
Supplemental Content	https://purl.fdlp.gov/GPO/LPS106292
Subjects	Airplanes--Turbine-propeller engines. --Design and construction. Airplanes--Turbojet engines. --Blades.

Series	Advisory circular ; AC no. 33-5 United States. Federal Aviation Administration. Advisory circular ; AC 33-5. ^A500611
General note	"06/18/90."
General note	Title from PDF file caption (viewed Dec. 9, 2008).
General note	GPO Cataloging Record Distribution Program (CRDP).
Technical details	Mode of access: Internet at the FAA web site. Address as of 12/9/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/eab0330a3c7a22eb862569b3005d6ace/$FILE/ac33-5.pdf; current access available via PURL.
Issued in other form	United States. Federal Aviation Administration. Turbine engine rotor blade containment/durability 5 p.
GPO item number	0431-A-27 (online)
Govt. docs number	TD 4.8/5:33-5

Turbine engine rotor blade containment/durability.

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