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LEADER 01930cam a2200397Ka 4500

001 ocn270761695;

003 OCoLC;

005 20081110143921.0;

006 m d f ;

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

008 081110s2005 dcu ob f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

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

086 0 a| TD 4.8/5:23-13 A;

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

245 10 a| Fatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes.;

260 a| Washington, DC :b| U.S. Dept. of Transportation, Federal Aviation Administration :b| For sale by the Supt. of Docs., U.S. G.P.O.,c| [2005];

300 a| 1 v. (various pagings) :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 23-13A;

500 a| "September 29, 2005.";

504 a| Includes bibliographical references (p. [34]).;

500 a| AC 23-13, dated April 15, 1993, is cancelled.;

538 a| Mode of access: Internet at the FAA web site. Address as of 11/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/ccae8a15127d66408625708c00710ba4/$FILE/ac23-13A.pdf; current access available via PURL.;

500 a| Title from title screen (viewed Nov. 10, 2008).;

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

650 0 a| Airframesx| Fatigue.=| ^A489811;

810 1 a| United States.b| Federal Aviation Administration.t| Advisory circular ;v| AC 23-13 A.=| ^A500611;

856 40 u| https://purl.fdlp.gov/GPO/LPS105323;

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

596 a| 1;

998 a| 1444690;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| MQ2770006l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 12/29/2008x| EDOCUMENTz| JERESOURCEo| .STAFF. 0;

Fatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes.

Author/creator	United States
Format	Electronic
Publication Info	Washington, DC : U.S. Dept. of Transportation, Federal Aviation Administration : For sale by the Supt. of Docs., U.S. G.P.O., [2005]
Description	1 v. (various pagings) : digital, PDF file
Supplemental Content	https://purl.fdlp.gov/GPO/LPS105323
Subjects	Airframes--Fatigue.

Series	Advisory circular ; AC 23-13A United States. Federal Aviation Administration. Advisory circular ; AC 23-13 A. ^A500611
General note	"September 29, 2005."
General note	AC 23-13, dated April 15, 1993, is cancelled.
General note	Title from title screen (viewed Nov. 10, 2008).
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. [34]).
Technical details	Mode of access: Internet at the FAA web site. Address as of 11/10/08: http://www.airweb.faa.gov/Regulatory%5Fand%5FGuidance%5FLibrary/rgAdvisoryCircular.nsf/0/ccae8a15127d66408625708c00710ba4/$FILE/ac23-13A.pdf; current access available via PURL.
GPO item number	0431-A-27 (online)
Govt. docs number	TD 4.8/5:23-13 A

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Fatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes.

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