As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS INITIALLY CRACKED AT STA 1095.9 OUTBOARD OF STR 1. THE DAMAGE WAS REPAIRED WITH A TIME LIMITED DOUBLER. WHEN THE PERMANENT REPAIR WAS BEING INSTALLED, TWO ADDITIONAL DAMAGE LOCATIONS WERE FOUND. A NEW PERMANENT REPAIR DOUBLER WAS INSTALLED IN ACCORDANCE WITH S/B 727-53A0204.