What was found
LEFT AND RIGHT AFT FUSELAGE SKIN HAS CRACKS AT FASTENERS LOCATED AT FRAMES 77 THRU 79. REAMED HOLES TO REMOVE CRACKS INSTALLED BUSHING AND RIVETS IAW EC5330-02203.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AND RIGHT AFT FUSELAGE SKIN HAS CRACKS AT FASTENERS LOCATED AT FRAMES 77 THRU 79. REAMED HOLES TO REMOVE CRACKS INSTALLED BUSHING AND RIVETS IAW EC5330-02203.