As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C5 CHECK - FUSELAGE SKIN CORROSION UNDER FRAME NR3 BOTTOM STA X882.703. REMOVED LIGHT CORROSION IAW SRM 51-21-00. CONFIRMED CRACK FREE CONDITION REF NTM 51-00-01-250-801. MIN REMAINING THICKNESS OF SKIN .060 REF NTM 51-00-02-250-801. MATERIAL LOSS FOUND WITHIN LIMITS IAW SRM 53-50-31, 53-10-31 REPAIR 1. APPLIED ALODINE AND PRIMER IAW SRM 51-25-10 AND 51-21-10.