What was found
AT C-CHECK, R/H FILLET PANEL 262K HAS SKIN SEPARATION AT CORNER AND CORROSION ON INTERIOR. CLEANED AND REBONDED PER SRM 51-1-9. REMOVED LEVEL 1 CORROSION PER SRM 51-1-8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, R/H FILLET PANEL 262K HAS SKIN SEPARATION AT CORNER AND CORROSION ON INTERIOR. CLEANED AND REBONDED PER SRM 51-1-9. REMOVED LEVEL 1 CORROSION PER SRM 51-1-8.