As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVING ACCESS PANEL 132AL, FOUND 4 HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR19R-20R. PERFORMED A MAJOR REPAIR BY OPENING UP HOLES TO REMOVE DAMAGE, FABRICATED AND INSTALLING FREEZE PLUGS. OPENED HOLES IN FREEZE PLUGS USING NR 10 DRILL BIT. ALL WORK DONE IAW REO 601R-53-11-162.