What was found
LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.