As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN FR35-FR36 STRG 1L-STRG 1R DRILLED FASTENER HOLE THROUGH CHEM-MILLED STEP ON UPPER FUSELAGE, PERFORMED SECTION I PERMANENT REPAIR AT FUSELAGE SKIN FR35-FR36 STRG 1L STRG 1R. AS PER PRI 562500-14 REV. 0 AND REV. 1 AND ER/A 562500-14. REV. ORIGINAL.