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 940, S15L HAS CHAFE DAMAGE NEAR FRAME RADIUS. REMOVED 15 FASTENERS FROM FRAME STA 940 LT S15L -S16L FOR ACCESS IAW SRM 51-40-02. CUT OUT DAMAGE AREA IAW SRM 51-70-12-06. DIMENSIONS OF CUTOUT 1.10L BY 0.030W. COMPLIED WITH FINAL EA NR 757-5342-27-A154Z AND UPS EO NR B757-5310-20559A.