As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE WAS FOUND AT F.S. 405.5 LEFT OF STRINGER 14L APPROXIMATELY 1.5 INCHES. HOLE SIZE APPROXIMATELY .375 X .125. MAINTENANCE REMOVED DAMAGE, HOLE .875” CIRCLE, INSTALLED COVER PATCH. COVER PATCH ALODINED AND INSTALLED USING AC240 B1/2. PATCH PAINTED TO MATCH AIRCRAFT. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.