As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C FUSELAGE FRAME AT STA 1020, S15L HAS CHAFE DAMAGE NEAR FRAME RADIUS CUT AND TRIMMED DAMAGED AREA IAW SRM 51-70-12 FIGURE 1. PERFORM HFEC NO CRACKS NOTED. FABBED REPAIR ANGLES AND FILLER/SHIM. TREATED/PRIMED STRINGER CLIPS. INSTALLED ALL REPAIR PARTS PER EA 757-5342-27-A1543 SECT "C" (STEPS 1&2). NO SHIMS REQUIRED. APPLIED CIC PER EA 757-5342-27-A1543.