As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STR 26R SKIN LAP HAS BLEND AREA OF 60 PERCENT MATERIAL LOSS .875 INCH LENGTH AND .250 INCH WIDTH BETWEEN 2ND AND 3RD ROW RIVETS FROM UPPER ROW AND CENTER OF BLEND IS AT BS 204 OR 26 INCHES AFT OF STA 178 BULKHEAD. MAJOR REPAIR: ACCOMPLISHED REPAIR PER SRM 53-10-01, DETAIL XIV.