LEADER 01081nam  2200313Ka 450 
001 9910697847303321
005 20081210152418.0
035   $a(CKB)5470000002392510
035   $a(OCoLC)277712162
035   $a(EXLCZ)995470000002392510
100   $a20081210d2004      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTurbine rotor strength requirements of 14 CFR 33.27$b[electronic resource]
210  1$a[Washington, D.C.] :$cU.S. Dept. of Transportation, Federal Aviation Administration,$d[2004]
215   $a7 pages $cdigital, PDF file
225 1 $aAdvisory circular ;$vAC no. 33.27-1
300   $a"9/27/04."
300   $aTitle from PDF file caption (viewed Dec. 10, 2008).
606   $aAirplanes$xTurbine-propeller engines$xCertification
615  0$aAirplanes$xTurbine-propeller engines$xCertification.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697847303321
996   $aTurbine rotor strength requirements of 14 CFR 33.27$93195503
997   $aUNINA