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AD 00-08-19

June 5, 2000

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PREVENT FATIGUE CRACKING OF THE BODY SKIN AT THE FORWARD CORNERS OF THE MID-GALLEY DOOR HINGE CUTOUTS, WHICH COULD RESULT IN REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE AND CONSEQUENT LOSS OF CABIN PRESSURIZATION\BOEING CO\727 SERIES\727C SERIES



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Product Details:

  • Revision: June 5, 2000
  • Published Date: June 5, 2000
  • 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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