As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD FUSELAGE LWR AREA BETWEEN E&E DOOR AND LT NLG DOOR HAS 2 EACH AREAS OF SKIN DAMAGE AT FASTENERS FROM STATIC BURN. IAW EG REMOVED DAMAGE BY OPENING 1 HOLE TO 1-4 INCH AND SPOTFACING SKIN AT FASTENER REMOVED .050 AND .045 MATERIAL FROM SKIN.