As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE PER BEECH 1900D SRM 51-70 AND TC 8.2.1.