As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABI - ACCIDENTAL DAMAGE FROM JACK OCCURRED TO BOTTOM FORWARD FUSELAGE SKIN PANEL AND FRAME 8 STA 4647. CUT OUT DAMAGED AREA OF SKIN AND FRAME. PERFORMED EDDY CURRENT INSPECTION. FABRICATED FRAME FROM AL 7075-T0, HEAT TREATED TO AL 7-7076-T6. FABRICATED SKIN DOUBLER. INSTALLED BOTH. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA983021.