LEADER 01378nam  2200337Ka 450 
001 9910697739903321
005 20081110143921.0
035   $a(CKB)5470000002391575
035   $a(OCoLC)270761695
035   $a(EXLCZ)995470000002391575
100   $a20081110d2005      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes$b[electronic resource]
210  1$aWashington, DC :$cU.S. Dept. of Transportation, Federal Aviation Administration :$cFor sale by the Supt. of Docs., U.S. G.P.O.,$d[2005]
215   $a1 volume (various pagings) $cdigital, PDF file
225 1 $aAdvisory circular ;$vAC 23-13A
300   $a"September 29, 2005."
300   $aAC 23-13, dated April 15, 1993, is cancelled.
300   $aTitle from title screen (viewed Nov. 10, 2008).
320   $aIncludes bibliographical references (page [34]).
606   $aAirframes$xFatigue
615  0$aAirframes$xFatigue.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697739903321
996   $aFatigue, fail-safe, and damage tolerance evaluation of metallic structure for normal, utility, acrobatic, and commuter category airplanes$93129642
997   $aUNINA