As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING B-CHECK, LEFT AFT FUSELAGE SKIN HAS 2 DEEP GOUGES LOCATED AT BS 1151.5 AND RIGHT BELOW STRINGER 21L. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM .080, 2024T3 ALUMINUM SHEET AND REPAIR DOUBLER FROM .090 2024T3. INSTALLED REPAIR WITH SOLID FASTENERS PER SRM 53-30-3. APPLIED FINISH COAT PER MM 51-20-00. (M)