Spoiler actuator loft alleviation mechanisms

An aircraft wing, comprising:

• an upper wing structure and a lower wing structure joined by a spar;
• a rib coupled to the spar;
• an upper spoiler having a first end and a hinge end pivotally coupled to the rib at a first fixed axis;
• a door coupled to the lower wing structure and movable between a closed position and an open position;
• and
• an actuator pivotally mounted within the aircraft wing between the upper spoiler and the door, the actuator having an extendable first end coupled to the upper spoiler and an opposite second end;
• wherein extension of the first end of the actuator rotates the upper spoiler to a deployed position and rotates the actuator such that the second end of the actuator induces downward movement of the door from the closed position to the open position in which the second end of the actuator extends below the lower wing structure during spoiler deployment.

A wing spoiler actuator mechanism, comprising:

• an upper spoiler having a free end and a hinge end pivotally coupled to a wing structure at a first fixed axis;
• a fairing movably coupled to the wing structure;
• and
• an actuator pivotally mounted to the wing structure between the upper spoiler and a door, the actuator having an extendable first end coupled to the upper spoiler and an opposite second end;
• wherein extension of the first end of the actuator rotates the upper spoiler to a deployed position and rotates the actuator such that the second end of the actuator induces translation of the fairing from a first position to a second position and the second end of the actuator extends outside the wing structure during spoiler deployment.