What was found
DURING HMBV INSPECTION, FOUND RT WING TO FUSELAGE PANEL LOWER NUT PLATE SUPPORT ANGLE IS CRACKED AT FRAME 47. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMBV INSPECTION, FOUND RT WING TO FUSELAGE PANEL LOWER NUT PLATE SUPPORT ANGLE IS CRACKED AT FRAME 47. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02.