What was found
RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK APPROX 1 INCH LONG. R & R ATTACH ANGLE IAW SRM 51-40-02 & ETN EM-53-142.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. CRACK APPROX 1 INCH LONG. R & R ATTACH ANGLE IAW SRM 51-40-02 & ETN EM-53-142.