The Utility System Actuators are electromechanical actuators that assist in positioning the hardware/equipment of auxiliary systems in an aircraft based on inputs from the pilot or the flight control system. They can also be manually operated without electrical power, depending on the requirement.
The system utilizes an electromechanical drive mechanism for operation.
The system offers quick and efficient opening and closing times, enabling rapid operation.
The system is equipped with a braking feature that allows for deceleration even in the event of a power loss and can be manually operated in the event of a power failure.
The system is designed to be lightweight and compact, optimizing space and weight considerations.
|Operating Voltage||28 VDC|
|Nominal Power||~ 250 W|
|Maximum Power||~ 400 W|
|Full Stroke Time||~ 10 Sec.|
|Nominal Operating Load||~ 3000 N|
|Stroke Length||230 mm|
|Closed Length||600 mm|
|Open Length||800 mm|
|DAL (ARP 4754A)||C|