What was found
DURING WALK AROUND, FOUND SKIN CORROSION AT LT LOWER AFT FUSELAGE, BETWEEN FRAME 2160 & 2180, AT STRINGER 33, L=49MM & W=39MM. PERMANENT REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 & EO 4453B152 PART 1, FOUND SATISFACTORY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING WALK AROUND, FOUND SKIN CORROSION AT LT LOWER AFT FUSELAGE, BETWEEN FRAME 2160 & 2180, AT STRINGER 33, L=49MM & W=39MM. PERMANENT REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 & EO 4453B152 PART 1, FOUND SATISFACTORY.