As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED MX, DAMAGE WAS DISCOVERED ON THE AFT CARRY THROUGH SPAR STRUCTURE. DAMAGE INCLUDES FORWARD UPPER SPAR WEB FLANGE CRACKS EXTENDING FROM FASTENER LOCATIONS TO EDGE OF WEB FLANGE AND ALSO IN THE FLANGE RADIUS. UPON DISCOVERY OF DAMAGE, ACFT WAS SUBMITTED TO MRO FOR REPAIRS. MRO SUBMITTED AND RECEIVED EO. REPAIRS ARE IN PROCESS.