Actuator

The Moritz Aerospace Actuator is designed to control the rudder trim tab position in general aviation applications. The actuator provides a position feed back signal.

A small electric motor drives a push-rod to drive a bell crank actuating the aircraft rudder trim tab. A cam within the actuator operates a micro switch preventing the actuator from running past full trim tab deflection.

Different variations of this unit can be designed to meet any specific applications

Specification:

• Weight: 2.0 LBS max.
• Operating Temperature: - 62° C to +82 ° C
• Dimensions: 2.72(H) x 2.7(W) x 4.3(L)
• Stroke: 0.13 to 0.99 from mounting surface with 0.070 over travel at either end
• Load capacity: 50 LBS max tension and compression 100 LBS max static
• Operating speed: 15 seconds max full stroke, no load
• Signal output: 900 +/- 100O to 9.10 +/-0.30 KO for 0.13 to 0.99 stroke.
• Altitude: 30,000 feet
• Environmental testing: RTCA-DO-160D