As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT BULKHEAD FUSELAGE STA 1183 RT LOWER 20 IN FROM RT CORNER FOUND DITCH PAN CRACKED. (BETWEEN RBL 24.7 AND RBL 45.5). REMOVED PAN PER SRM 51-30-2. CLEANED AREA TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW DITCH PAN PER SRM 51-30-2. TREATED AND PRIMED PAN PER SRM 51-10-2.