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005 20140212125249.0
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035   $a(OCoLC)870179063
035   $a(EXLCZ)995470000002444976
100   $a20140207d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aValidation of helicopter gear condition indicators using seeded fault tests /$fPaula Dempsey, E. Bruce Brandon
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2013.
215   $a1 online resource (15 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-217872
300   $aTitle from title screen (viewed on Feb. 7, 2014).
300   $a"April 2013."
300   $a"Prepared for the Joint Machinery Failure Prevention Technology (MFPT) 2013 and 59th International Instrumentation Symposium (IIS) sponsored by the Society for Machinery Failure Prevention Technology and the International Society of Automation, Cleveland, Ohio, May 13-17, 2013."
320   $aIncludes bibliographical references (pages 14-15).
606   $aHelicopter performance$2nasat
606   $aAircraft reliability$2nasat
606   $aSystems health monitoring$2nasat
606   $aHelicopter propeller drive$2nasat
606   $aSpiral bevel gears$2nasat
606   $aFault detection$2nasat
615  7$aHelicopter performance.
615  7$aAircraft reliability.
615  7$aSystems health monitoring.
615  7$aHelicopter propeller drive.
615  7$aSpiral bevel gears.
615  7$aFault detection.
700   $aDempsey$b Paula$01406496
702   $aBrandon$b E. Bruce
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910704875703321
996   $aValidation of helicopter gear condition indicators using seeded fault tests$93485650
997   $aUNINA