As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF THE FCB AFT CORNER SCUFF PLATE; NOTICED THE SCUFF PLATE WAS CRACKED AND BROKE IN HALF UPON REMOVAL UPON REMOVAL OF THE FCB AFT CORNER SCUFF PLATE NOTICED THE SCUFF PLATE WAS CRACKED AND BROKE IN HALF UPON REMOVAL. APPLIED BMS 10-11 PRIMER. IAW SRM 51-29-010G-0. REPAIRED FCB AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(4).