As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, RT AFT OVERWING EXIT HATCH HAS CORROSION AT FWD EDGE FRAME AT LOWER STOP PIN 2 INCHES BELOW DATA PLATE. UPON FURTHER INVESTIGATION FOUND AREA TO BE CRACKED APPROX .5 INCH LONG, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED FRAME SEGMENT RECEIVED NEW FRAME SEGMENT AND INSTALLED IAW SRM 51-30-2.