As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY OUR BY OUR INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT FWD FITTING JUST BELOW THE UPPER MOST AFT HOLE ON THE VERTICAL OTBD FLANGE.