What was found
LT OVERWING TO FUSELAGE PANEL ATTACH ANGLE BS 449.85 IS CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT OVERWING TO FUSELAGE PANEL ATTACH ANGLE BS 449.85 IS CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.