Aircraft multi-wheel truck beam positioner

An aircraft landing gear, comprising:

• a shock strut including a rod with a first end slidably disposed within a cylinder;
• a torque link assembly located one of forward and aft of the shock strut, the torque link assembly comprising:
• an upper torque link having a first end rotatably coupled to the cylinder;
• and
• a lower torque link having a first end rotatably coupled to the rod and a second end rotatably coupled to a second end of the upper torque link;
• a beam rotatably coupled to a second end of the rod, the beam being configured to have a forward wheel and an aft wheel rotatably mounted thereto;
• and
• a truck beam positioner located one of forward and aft of the shock strut, the truck beam positioner comprising:
• an upper link having a first end rotatably connected to the cylinder;
• a lower link having a first end rotatably connected to the beam, a second end of the lower link being rotatably coupled to a second end of the upper link;
• a limiter configured to limit rotation of the upper link relative to the lower link, wherein the limiter is selectively adjustable to provide a predetermined maximum distance between the first end of the upper link and the first end of the lower link;
• and
• a biasing element configured to bias the second end of the lower link toward the shock strut.