What was found
FLT 583 - MEX-CUN - WHEN THE AIRCRAFT GETS PLATFORM BY ITSELF THE RIGHT GYRO WAS EXCEEDED AND THE ACTUATORS WERE STUCK. AIRCRAFT WAS SENT TO THE HANGAR AND THE STEERING CONTROL VALVE WAS CHANGED IAW MM 32-52-01. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FLT 583 - MEX-CUN - WHEN THE AIRCRAFT GETS PLATFORM BY ITSELF THE RIGHT GYRO WAS EXCEEDED AND THE ACTUATORS WERE STUCK. AIRCRAFT WAS SENT TO THE HANGAR AND THE STEERING CONTROL VALVE WAS CHANGED IAW MM 32-52-01. (M)