What was found
RIGHT LOWER ATTACH ANGLE FOR THE OVERWING PANEL IS CRACKED BETWEEN FUSELAGE FRAMES 47 AND 48. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, AND ETN -EM-53-142.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT LOWER ATTACH ANGLE FOR THE OVERWING PANEL IS CRACKED BETWEEN FUSELAGE FRAMES 47 AND 48. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, AND ETN -EM-53-142.