As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A .375 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AND UNDERLYING GUSSET AT THE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW (UPPER END OF THE C-D POST). THE CRACK WAS ROUTED OUT AND A STEEL REPAIR DOUBLER AND ALUMINUM REPAIR TRIPLER WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365155-14, REV B.