What was found
TOP SKIN PANEL FRONT SPAR BETWEEN RIB 14 AND 27 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 14 AND 27 CORROSION AROUND SEVERAL FASTENER BOLTS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270