As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SCRATCH ON LOWER FUSELAGE SKIN, AFT OF STA X424.124, ALONG STA 31P. BLENDED AND POLISHED TO REMOVE DAMAGE TO THE LIMITS STATED IN RD 8-53-15536, INSPECTED THE ENTIRE REPAIR AREA FOR CRACK AND DIS-BONDS(NONE PERMITTED), REMOVED AND REPLACED BLENDED FASTENERS AND RE-PROTECTED METAL WITH CORROSION INHIBITING COMPOUNDS. ALL WORK WAS DONE IAW ECO 008.53-18.07.