As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 24P HAS CORROSION BS 584.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS REMAINING NOTED .044, REF NTM 51-00-04-910-801 PT 1. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. DAMAGE FOUND TO BE WITH IN LIMITS IAW RD 8/4-53-5040. APPLIED ALODINE, PRIMER, TOP COAT AND CPC IAW RD 8/4-53-5040. COMPLIED WITH TC RD 8/4-53-5040.