What was found
LEFT WING FROM SPAR UPPER ANGLE TOP SURFACE CORRODED AT RIB 13. CORROSION REMOVED IAW SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR MATERIAL THICKNESS: 0.200 MATERIAL REMOVED: 0.003. WITHIN LIMITS AS PER SRM: 51-10-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING FROM SPAR UPPER ANGLE TOP SURFACE CORRODED AT RIB 13. CORROSION REMOVED IAW SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR MATERIAL THICKNESS: 0.200 MATERIAL REMOVED: 0.003. WITHIN LIMITS AS PER SRM: 51-10-10.