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100   $a20051102d2004      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe temperature distribution within solid metal cylinders subjected to a standard aircraft engine fire$b[electronic resource] $edata report /$fJohn W. Reinhardt, Dung Do, Jason Fayer
210  1$aWashington, D.C. :$cU.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,$d[2004]
215   $a1 volume $cdigital, PDF file
300   $aTitle from title screen (viewed on Nov. 2, 2005).
300   $a"April 2004."
517   $aTemperature distribution within solid metal cylinders subjected to a standard aircraft engine fire 
606   $aAirplanes$xMotors$xTesting
606   $aMetals$xFatigue
606   $aAirplanes$xParts$xTesting
606   $aAirplanes$xFires and fire prevention$xTesting
615  0$aAirplanes$xMotors$xTesting.
615  0$aMetals$xFatigue.
615  0$aAirplanes$xParts$xTesting.
615  0$aAirplanes$xFires and fire prevention$xTesting.
700   $aReinhardt$b John W$01381974
712 02$aUnited States.$bFederal Aviation Administration.$bOffice of Aviation Research.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910694680503321
996   $aThe temperature distribution within solid metal cylinders subjected to a standard aircraft engine fire$93432690
997   $aUNINA