Which flight-control arrangement connects the rudder and ailerons with interconnected springs to counteract adverse yaw and can be overridden if a slip is necessary?

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Multiple Choice

Which flight-control arrangement connects the rudder and ailerons with interconnected springs to counteract adverse yaw and can be overridden if a slip is necessary?

Explanation:
When you roll the airplane, the outside wing tends to drag the nose in the opposite direction due to adverse yaw. The arrangement in question uses a mechanical link between the ailerons and the rudder with springs so that as you command a roll, a compensating rudder deflection is automatically produced to counter that yaw. This makes turns more coordinated without extra pilot input, and it can be overridden when a slip is necessary by applying rudder independently. The other options don’t describe this roll-to-yaw interconnection: a trim tab system only adjusts neutral surfaces, spoilerons use spoilers for roll instead of linking to the rudder, and fly-by-wire protection refers to electronic safeguards rather than a physical coupling of control surfaces.

When you roll the airplane, the outside wing tends to drag the nose in the opposite direction due to adverse yaw. The arrangement in question uses a mechanical link between the ailerons and the rudder with springs so that as you command a roll, a compensating rudder deflection is automatically produced to counter that yaw. This makes turns more coordinated without extra pilot input, and it can be overridden when a slip is necessary by applying rudder independently.

The other options don’t describe this roll-to-yaw interconnection: a trim tab system only adjusts neutral surfaces, spoilerons use spoilers for roll instead of linking to the rudder, and fly-by-wire protection refers to electronic safeguards rather than a physical coupling of control surfaces.

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