EverySpec Standards
Home > Library > FAA > FAA-AC-PUBS > AC 20-128A PART-2 APPENDIX

AC 20-128A (PART-2, APPENDIX), ADVISORY CIRCULAR: DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE (25-MAR-1997)

AC 20-128A (PART-2, APPENDIX), ADVISORY CIRCULAR: DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE (25-MAR-1997).

AC 20-128 Rev. A

    

Version:
a03-19973.83 MB AC_20-128A
A03-19974.09 MB AC_20-128A_PART-2_APPENDIX

Simple Search
MilSpec Search



About Us   |   Terms of Use   |   DMCA   |   Privacy   |   EverySpec LLC © 2009 - 2024   All rights reserved.