What was found
INSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2.