As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IN THE COURSE OF PERFORMING POST FLIGHT INSPECTION THE FIELD MAINTENANCE CREW DISCOVERED A CRACKED IN THE LEFT SPLICE FITTING. THE CRACK ORIGINATED AT THE FORWARD HI-LOCK FASTENER ON THE PYLON SIDE FUSELAGE 770 INCH WL 178 LBL 14. THIS CRACK MEASURES .400 INCH IN LENGTH. (M)