As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE INSPECTION OF THE RIVETS AT THE FORWARD PRESSURE BULKHEAD, TWO SEPERATE CRACKS WERE NOTED IN THE LT DISHPAN JUST FORWARD OF THE PILOTS RUDDER PEDALS. THE CRACKS WERE BETWEEN FASTENERS. THE PN S25-8FN323-1 WAS REMOVED & REPLACED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURAL REPAIR MANUAL (SRM) AND CHAPTER 51-20-41. FAA FORM 337 COMPLETED 1/24/03. NO FURTHER DEFECTS TO LIKE COMPONENTS WAS NOTED.