What was found
AFTER ACCESS PANEL 621BR REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV - -
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER ACCESS PANEL 621BR REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV - -