What was found
DURING HEAVY MAINTENANCE, FUSELAGE SKIN HAD A DENT WITH 2 GOUGES AT FRAME 23 + 10, STRINGERS 42-43R. REPAIRED IAW SRM 53-00-11-300-029, PARA 2(A)(3), & 53-00-11-300-029 PARA 2(A)(7-17).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY MAINTENANCE, FUSELAGE SKIN HAD A DENT WITH 2 GOUGES AT FRAME 23 + 10, STRINGERS 42-43R. REPAIRED IAW SRM 53-00-11-300-029, PARA 2(A)(3), & 53-00-11-300-029 PARA 2(A)(7-17).