What was found
FUSELAGE SKIN GOUGE AT FRAME 32 BETWEEN STRINGER 38 -39R. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 53-00-11 FIG 240.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN GOUGE AT FRAME 32 BETWEEN STRINGER 38 -39R. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 53-00-11 FIG 240.