What was found
AT C-CHECK, LT WING T/E AREA INNER WING FLAP MECHANISM SUPPORT FITTING HAS UPPER PANEL WITH CRACK ON SURFACE. STOP DRILLED END OF CRACK, FABRICATED DOUBLER PER SRM 51-1-8 AND INSTALLED PER 51-1-21, 6.375 X 3.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LT WING T/E AREA INNER WING FLAP MECHANISM SUPPORT FITTING HAS UPPER PANEL WITH CRACK ON SURFACE. STOP DRILLED END OF CRACK, FABRICATED DOUBLER PER SRM 51-1-8 AND INSTALLED PER 51-1-21, 6.375 X 3.5.