What was found
DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.