As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER OUTBOARD CORNER OF CAPTAIN'S WINDSHIELD CUTOUT AND A .125 INCH CRACK WAS FOUND IN SKIN AT LOWER FORWARD CORNER JUST FORWARD OF CAPTAIN'S SLIDING WINDOW. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-30-3.