As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT FUSELAGE FRAME AT STA 1340 BETWEEN STRINGERS 25R AND 26R DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 RPR 5. PER SRM 53-00-07 RP R 5 TABLE II THIS RPR REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE AFTER THIS IS A CAT B RPR. INSPECTIONS ARE BOTH VISUAL AND NDT.