What was found
RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE NR 2 HAS A 1.5 INCH CRACK ON THE AFT END. REMOVED AND REPACED 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.
RIGHT WING TO FUSELAGE LOWER ATTACH ANGLE NR 2 HAS A 1.5 INCH CRACK ON THE AFT END. REMOVED AND REPACED THE ATTACH ANGLE IAW SRM 51-40-02