What was found
LEFT UPPER ATTACH ANGLE FOR OVERWING LATERAL PANEL IS CRACKED AT FUSELAGE FRAME 50. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT UPPER ATTACH ANGLE FOR OVERWING LATERAL PANEL IS CRACKED AT FUSELAGE FRAME 50. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.