What was found
AT C-CHECK, LT UPPER WING TO FUSE FILLET PANEL 261G IS DELAMINATED. REPAIRED PANEL PER SRM 57-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LT UPPER WING TO FUSE FILLET PANEL 261G IS DELAMINATED. REPAIRED PANEL PER SRM 57-2-0.