As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN SEAT TRACK IS CORRODED FROM FRAME 55 TO FRAME 56, RBL 38. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL THICKNESS IS 0.140 IAW SRM 51-31-20. REMAINING THICKNESS 0.105. MATERIAL LOSS 0.035 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. PAINTED IAW SRM 51-75-10.