Establishes informations for motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque. Primary and secondary function motors are covered. Actuators with internal rotation angle limits and low-speed motors are not covered. Shall be used in conjunction with the detail specification particular to each application.
Status : WithdrawnPublication date : 1990-02
Edition : 1Number of pages : 18
Technical Committee:Aerospace fluid systems and components