What was found
FUSELAGE FRAME IS CRACKED FORWARD OF INSTRUMENT PANEL BELOW CAPTAINS WINDSCREEN, DISCOVERED AT C-CHECK. REPLACED FUSELAGE FRAME BELOW CAPTAINS WINDSCREEN 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 IS CRACKED FORWARD OF INSTRUMENT PANEL BELOW CAPTAINS WINDSCREEN, DISCOVERED AT C-CHECK. REPLACED FUSELAGE FRAME BELOW CAPTAINS WINDSCREEN IAW SRM 120 51-10-02 PG 3 SEC 3A.