As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE LEFT AND RIGHT FORWARD FUSELAGE II, FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE FRAME AND THE DIRECT VISION WINDOW LOWER BEAM. MAINTENANCE REPLACED THE LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FORWARD FUSELAGE II, FRAME 10 AT THE INTERSECTION OF THE FRAME AND DIRECT VISION WINDOW LOWER BEAM. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.