As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION FOUND IN OPEN HOLE FROM FIRST FASTENER HOLE FWD BS 540 S-22R FUSELAGE SKIN. CRACK DIRECTIONS: 1 O`CLOCK AND 11 O`CLOCK APPROXIMATE. PERFORMED REPAIR ON DRAG LINK ON BS 540 STR 22R FUSELAGE SKIN, IAW EO 5331-E-14523 REV 1.