What was found
AT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.