What was found
LEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE ON WING HAS 1/8 INCH CRACK JUST AFT OF SPAR 2. R & R THE ATTACH ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE ON WING HAS 1/8 INCH CRACK JUST AFT OF SPAR 2. R & R THE ATTACH ANGLE IAW SRM 51-40-02.