What was found
THE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505.