As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) UPON PREFLIGHT INSPECTION, CRACK WAS DETECTED VISUALLY IN AFT OUTBOARD SADDLE OF LT SIDE TUBE. THE MANUFACTURER PUBLISHED SERVICE INSTRUCTION DRAWING NO.DSI 9150 DATED 99.04.01 TITLED (ADD 206 SADDLE SPACERS) TO PREVENT SADDLE CRACKING. THIS AIRCRAFT HAD COMPLIED WITH THIS SERVICE INSTRUCTION, CORRECT TORQUE WAS FOUND ON ALL FASTENERS.