As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 'C' CHECK, THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B AND THE LEFT OVERWING SLIDE PACK WAS FOUND CRACKED. THE CRACK EMANATES FROM THE FORWARD MOST EDGE TO THE SECOND FASTENER HOLE APPROXIMATELY 4 INCHES AFT OF THE FORWARD EDGE. REPAIRED PER NWA EA 32-97835.