As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER EXTERIOR FUSELAGE SKIN IS DENTED AT BS 972.5 STR S25R + 4 A=2.0 AND Y=.072 A OVER Y IS 27 OUT OF LIMITS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND STRUCTURAL FILLER PER AAR EAI060495 REV IR.