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AD 99-17-03

September 16, 1999

Complete Document

PREVENT FAILURE OF THE FIN SPAR, LOSS OF THE TAIL ROTOR, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\204B\205A-1\205A



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Product Details:

  • Revision: September 16, 1999
  • Published Date: September 16, 1999
  • Status: Active, Most Current
  • Document Language:
  • Published By: US Federal Aviation Administration (FAA)
  • Page Count: 0
  • ANSI Approved: No
  • DoD Adopted: No

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