What was found
CORROSION DETECTED AT ATTACH ANGLES, BS 116 STRINGER 24L. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-05 AND SRM 51-40-07.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION DETECTED AT ATTACH ANGLES, BS 116 STRINGER 24L. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-05 AND SRM 51-40-07.