As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON UPPER CHORD BS 986 RBL45 AND LBL45 AT NUTPLATE LOCATION / ON BS986 UPPER CHORD LBL 45 REPAIRED I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIG 205 DUE TO FOUND OUT LIMIT AND BS 986 UPPER CHORD RBL 45 REMOVED CORROSION ON 2' X 1' AREA ORIGINAL MATERIAL THICKNESS IS 0.150' REMAINING MATERIAL THICKNESS IS. 0.145 FOUND TO BE IN LIMITS. I.A.W SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1