As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STIFFENER ON AFT SIDE OF 621 BULKHEAD AT BL0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AFT SIDE OF 621 BULKHEAD AT BL0 DAMAGE FOUND TO BE WITHIN LIMITS: MAX DEPTH OF DAMAGE 0.009 IN/ MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61-1523.