LEADER 01759oam  2200529Ia 450 
001 9910699342603321
005 20230902161818.0
035   $a(CKB)5470000002402491
035   $a(OCoLC)227912412
035   $a(EXLCZ)995470000002402491
100   $a20080513d2006      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFailure analysis of a CH-47 horizontal hinge pin assembly, P/N 114RS226$b[electronic resource] /$fMarc Pepi, Gary Wechsler
210  1$aAberdeen Proving Ground, MD :$cArmy Research Laboratory,$d[2006]
215   $a1 online resource (viii, 28 pages) $cillustrations (some color)
225 1 $aARL-TR ;$v4011
300   $aTitle from title screen (viewed on June 28, 2011).
300   $a"December 2006."
320   $aIncludes bibliographical references (page 26).
410  0$aARL-TR (Aberdeen Proving Ground, Md.) ;$v4011.
606   $aChinook (Military transport helicopter)
606   $aHinges
606   $aPins (Engineering)
606   $aMetals$xFracture
606   $aMetals$xFatigue
615  0$aChinook (Military transport helicopter)
615  0$aHinges.
615  0$aPins (Engineering)
615  0$aMetals$xFracture.
615  0$aMetals$xFatigue.
700   $aPepi$b Marc S$01393897
701   $aWechsler$b Gary$01395002
712 02$aU.S. Army Aviation and Missile Command.
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bBUF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910699342603321
996   $aFailure analysis of a CH-47 horizontal hinge pin assembly, P$93529935
997   $aUNINA