As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MX THE SKIN OF FUSELAGE WAS FOUND CRACKED AROUND TWO RIVETS ONE ON EACH SIDE OF STRINGER ONE AT F.S. 150.60. MAINTENANCE REMOVED CRACKS BY .750” DIAMETER CUT OUTS. FABRICATED FILLERS FOR LT AND RT SIDE. FABRICATED EXTERNAL PATCH.