What was found
LT FUSELAGE SKIN DENTED AT FRAME 26 STRINGER 34 - 35. REPAIR DOUBLER INSTALLED IAW SRM 53-00-11 FIG 240, SRI 53-00-11-2-017-00 TBL 223.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE SKIN DENTED AT FRAME 26 STRINGER 34 - 35. REPAIR DOUBLER INSTALLED IAW SRM 53-00-11 FIG 240, SRI 53-00-11-2-017-00 TBL 223.