What was found
AFTER ACCESS PANEL 521BL REMOVAL , CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER ACCESS PANEL 521BL REMOVAL , CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --