What was found
FUSELAGE SKIN GOUGED AT FS 258, WL 80. DAMAGE DETERMINED TO BE BEYOND LIMITS. DAMAGE REPAIRED BY TRIMMING, INSPECTING AND RESTORING PROTECTIVE FINISH IAW SRM 51-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN GOUGED AT FS 258, WL 80. DAMAGE DETERMINED TO BE BEYOND LIMITS. DAMAGE REPAIRED BY TRIMMING, INSPECTING AND RESTORING PROTECTIVE FINISH IAW SRM 51-20.