As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER CROWN FWD OF TCAS, BS 427 BETWEEN BL 0 AND STR 1R HAS STATIC DISCHARGE. DRILLED OUT DAMAGE, PERFORMED HFEC I NSPECTION, NO CRACK NOTED. PERFORMED FHSR OF HOLE PER NDTM 51-00-16, PART 6 NO CRACKS NOTED INSTALLED SOLID FASTENER PER SRM.