What was found
LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PANEL 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, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PANEL ANGLE IAW SRM 51-20-02 AND ETN-EM-53-142.