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AD 95-NM-216-R1

March 12, 1997

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REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE AND RESTRICTED OPERATION OF THE MAIN LANDING GEAR (MLG) FREE-FALL SYSTEM\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A3 20-233



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Product Details:

  • Revision: March 12, 1997
  • Published Date: March 12, 1997
  • 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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