What was found
INSPECTION FOUND LEADING EDGE OF FORWARD UPPER FUSELAGE SKIN PEELED UP AT RADOME, STA 178. THE DAMAGED SKIN PANEL WAS REMOVED, A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LEADING EDGE OF FORWARD UPPER FUSELAGE SKIN PEELED UP AT RADOME, STA 178. THE DAMAGED SKIN PANEL WAS REMOVED, A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.