What was found
CORROSION ON PREVIOUS REPAIR PLUG AT Y=1000 X=-54. PREVIOUS REPAIR PLUG WAS REPLACED PER SRM 53-05 FIG 4A (SHEET 1) AND SRM 51-30-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON PREVIOUS REPAIR PLUG AT Y=1000 X=-54. PREVIOUS REPAIR PLUG WAS REPLACED PER SRM 53-05 FIG 4A (SHEET 1) AND SRM 51-30-1.