What was found
RIGHT WING TO FUSELAGE UPPER ATTACHMENT ANGLE HAS 2 INCH CRACK AT FRAME. REMOVED & REPAIRED RT WING TO FUSELAGE UPPER ATTACHMENT ANGLE AT FRAME 50 IAW SRM 53-23-12 & 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE UPPER ATTACHMENT ANGLE HAS 2 INCH CRACK AT FRAME. REMOVED & REPAIRED RT WING TO FUSELAGE UPPER ATTACHMENT ANGLE AT FRAME 50 IAW SRM 53-23-12 & 51-40-02.