As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED A 3.25 INCH LONG CRACK 27.5 INCHES LT OF BELLY CENTERLINE AT APPROXIMATELY STA. F.S. 352. MAINTENANCE REPAIRED THE CRACK IN THE FUSELAGE IAW SRM 51-70 FROM F.S. 351 TO F.S. 354.25. REPAIR DIMENSIONS 7.25 INCHES BY 4 INCHES.