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AD 99-CE-61

September 28, 1999

Complete Document

PREVENT FATIGUE FAILURE OF THE ELEVATOR AND RUDDER TRIM TAB PIVOT ARMS BECAUSE OF CRACKS\PILATUS AIRCRFT LTD\PC-7



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Product Details:

  • Revision: September 28, 1999
  • Published Date: September 28, 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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