What was found
FUSELAGE FRAME AND CLEAT CRACKED ON CAPTAINS SIDE JUST BELOW DV WINDOW SUPPORT FRAME, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AND CLEAT CRACKED ON CAPTAINS SIDE JUST BELOW DV WINDOW SUPPORT FRAME, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A.