As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR, UPON ROUTINE INSPECTIONS A FUSELAGE SKIN CRACK AT FS 150.6 AT STRINGER 1. CRACK APPROXIMATELY 1.3 INCHES. MAINTENANCE REPAIRED THE FUSELAGE SKIN CRACK AT BS 150.6 IAW BEECH 1900D SRM 51-70 . RII INSPECTION COMPLIED WITH PER T.C. 8.2.1.