What was found
DAMAGE TO FUSELAGE AT APPROX 6 INCHES AFT OF TOP AFT CORNER OF ELECTRICAL CONNECTOR PANEL HOLE APPROX 1' X 4". REPAIRED PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE TO FUSELAGE AT APPROX 6 INCHES AFT OF TOP AFT CORNER OF ELECTRICAL CONNECTOR PANEL HOLE APPROX 1' X 4". REPAIRED PER SRM 53-30-3.