What was found
RIGHT WING LEADING EDGE SUSTAINED DAMAGE AT APPROX XFS 80 AFTER RAMP VEHICLE CAME IN CONTACT. INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING LEADING EDGE SUSTAINED DAMAGE AT APPROX XFS 80 AFTER RAMP VEHICLE CAME IN CONTACT. INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 2.