What was found
FOUND .625 INCH CRACK IN INBOARD MOST RIB OF THE LEFT OUTBOARD MIDFLAP. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAINMENT. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND .625 INCH CRACK IN INBOARD MOST RIB OF THE LEFT OUTBOARD MIDFLAP. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAINMENT. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M)