As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERIOR SKIN CHAFED AT LAP SEAM STA 720D 15" STR 19L. CUT-OUT DAMAGE AREA SIZE: 2.7500" X 3.7500" AT LAP SEAM IAW SRM 53-30-3, FIG 6. FABRICATED REPAIR DOUBLER AND 2 EA, TAPER FILLER FROM 2024T3 .071 SIZES: 11.5 X 8.7500" AND 2 EA 1" X 6" AND 2 EA FILLERS FROM 2024T3 .063 SIZES: 6.1250" X 10.5" AND 3.7500" X 2.7500". INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 6.