As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK IN LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL WAS REPAIRED PER REO 670-53-11-2068 REV --