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AD 97-SW-38

April 21, 1998

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CRACKS ON A TAIL ROTOR SHAFT FLAPPING HINGE RETAINER (RETAINER) THAT COULD LEAD TO HIGH TAIL ROTOR VIBRATIONS, LOSS OF TAIL ROTOR CONTROL, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\SA330F\SA330G\SA330J



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Product Details:

  • Revision: April 21, 1998
  • Published Date: April 21, 1998
  • Status: Active, Most Current
  • Document Language: English
  • Published By: US Federal Aviation Administration (FAA)
  • Page Count: 0
  • ANSI Approved: No
  • DoD Adopted: No

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