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.
Текущий статус : WithdrawnДата публикации : 1990-02
Версия : 1
Технический комитет:Aerospace fluid systems and components