As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN STATIC DISCHARGE BETWEEN BS 540 AND 555 STR 26R AND 28R. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED RIVETS AND ACP HFEC WITH NO CRACKS INDICATED PER NDT MANUAL 51-00-11 PT 6 BY QC 400. INSTALLED BLIND FASTENER PER SRM 51-40-02 AND MM 53-30-95 PG 602. PER MM 53-30-95 PG 602 CHERRY MAX FASTENERS MUST BE REINSPECTED AT EACH C-CK AND REPLACED WITH SOLID FASTENER AT NEXT HMV.