As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK - FOUND CHAFE DAMAGE TO RT INBD FLAP LOCATED AROUND INBD FLAP HINGE ARM. BLENDED 2 CHAFED AREAS IAW SRM 51-12-00-001-001-A01. ORIGINAL SKIN THICKNESS IS .063, REMAINING MATERIAL IS.055 AND .057. CHAFES ARE WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. R & R 4 DAMAGED RIVETS IAW SRM 51-42-13-001-001-A01. PREPPED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-01-001-001-A01 AND 51-25-16-001-001-A01.