As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .75 INCH AND .1093 INCH CRACK IN RT WING LOWER TRAILING EDGE OF INBOARD MIDFLAP, 34 INCHES FROM INBOARD END. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 57-50-4, FIGURE 1.