As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV AT TIMCO LCQ, THE CRADLE SHORING INSTALLED AT FS 680 CAUSED DENTING ON THE FUSELAGE SKIN. DENTING IS JUST ABOVE S-24R TO JUST BELOW S-25R. THE DENT WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED, WITH TIME-LIMITED RESTRICTIONS PER ER/A 459984-14.