As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, NWW BS 400 STR R44 RIGHT AFT CORNER INTERNAL CIRCUMFERENTIAL SKIN SPLICE FOUND CRACK APPROX .25 INCH LONG RUNNING AFT. THE CRACKED SPLICE REMOVED FOR STOP HOLE DRILLED. THE STOP CONFIRMED NIL CRACK BEYOND THE STOP HOLE. THE AREA REPAIRED PER SRM 53-30-03 FIG 35.