As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE OUTER SKIN IS CHAFED AT BS 720D+13 INCHES STR 19L. BLENDED CHAFED AREA 1 X 2 X .027 FROM ORIGINAL .064 OUTER SKIN BS 720D+13 INCHES STR 19L. FOUND OUT OF LIMITS PER SRM 53-30-01. REPAIRED CHAFED AREA PER SRM 53-30-03 AND FED EX SR 27-57-056.