What was found
CORROSION FOUND ON FUSELAGE SKIN LAP JOINT BTW FR 23A-23C STR 11L. REMOVED AS PER SRM 51-21-42, SKIN REPAIRED IAW SRM 53-00-00 FIG 424 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.012 OUT OF LIMITS AS PER SRM: 53-31-00 FIG 301.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION FOUND ON FUSELAGE SKIN LAP JOINT BTW FR 23A-23C STR 11L. REMOVED AS PER SRM 51-21-42, SKIN REPAIRED IAW SRM 53-00-00 FIG 424 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.012 OUT OF LIMITS AS PER SRM: 53-31-00 FIG 301.