What was found
CRACK IN COVE SKIN 29 INCHES FROM END OF NUMBER 9 SLAT. STOPPED DRILLED END OF CRACK. HFEC SURFACE SCAN CONFIRMS CRACK TERMINATION AT STOP DRILL. FABRICATED AND INSTALLED REPAIR PER AARD 57-43-00-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN COVE SKIN 29 INCHES FROM END OF NUMBER 9 SLAT. STOPPED DRILLED END OF CRACK. HFEC SURFACE SCAN CONFIRMS CRACK TERMINATION AT STOP DRILL. FABRICATED AND INSTALLED REPAIR PER AARD 57-43-00-4.