What was found
LEFT OVERWING TO FUSELAGE PANEL LOWER NUTPLATE SUPPORT FLANGE IS CRACKED AT FRAME 50. REPLACED OVERWING ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT OVERWING TO FUSELAGE PANEL LOWER NUTPLATE SUPPORT FLANGE IS CRACKED AT FRAME 50. REPLACED OVERWING ANGLE IAW SRM 51-40-02.