What was found
AT C-CHECK, RIGHT WING L/E INTERNAL PART ACCESS PANEL 518A CRACKED .25 INCH AT XFS 720. FABRICATED AND INSTALLED DOUBLER 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, RIGHT WING L/E INTERNAL PART ACCESS PANEL 518A CRACKED .25 INCH AT XFS 720. FABRICATED AND INSTALLED DOUBLER PER SRM 57-2-0.