As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE DIRECT VISION WINDOW LOWER BEAM. MAINTENANCE REPLACED THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE DIRECT VISION WINDOW LOWER BEAM. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.