What was found
TOP SKIN PANEL FRONT SPAR BETWEEN RIB 1 AND 14 CORROSION AROUND SEVERAL FASTENER BOLTS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TOP SKIN PANEL FRONT SPAR BETWEEN RIB 1 AND 14 CORROSION AROUND SEVERAL FASTENER BOLTS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270