As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE FRAME 34R FROM STR 13R TO 22R HAS NUMEROUS SMALL GOUGES AND BARE METAL APPROX 4 SQ IN THROUGHOUT ENTIRE FRAME ON INSIDE OF ACFT DEEPEST OF THE GOUGES IS APPROX .005" BLENDED OUT GOUGES ON FRAME 34R BETWEEN STR 13R TO 22R CHECK LIMITS FOUND OUT OF LIMITS IAW SRM 53-14-13 AND 53-10-00. REPAIRED FR 34R IAW SRM 53-10-13 AND SRM 51-73-10.