As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN SEAT TRACK CORRODED IN AREAS FROM FRAME 40 TO FRAME 45 RBL 77. REMOVED CORROSION ORIGINAL THICKNESS .145 REMOVED .033 REMAINING MAT IS .112. FOUND TO BE OUT OF LIMITS IAW A300-600 53-10-16 TOOL NR TWS 58329B. REMOVED SEAT TRACK IAW FEDEX A300-600 SRM 51-40-21 PG7. FABRICATED NEW SEAT TRACK IAW ABS5456C580EPART MARKED REF FEDEX GMM 7-0-1000. INSTALLED SEAT TRACK IAW FEDEX A300-600 SRM 51-40-21 PG 6-7.