What was found
DURING SCHEDULED STRUCTURAL INSP, DISCOVERED RT HEAVY ANGLE CRACKED AT FORWARD END, APPROX 2.0 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED STRUCTURAL INSP, DISCOVERED RT HEAVY ANGLE CRACKED AT FORWARD END, APPROX 2.0 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.