System for rolling landing gear

A system for rolling landing gear, the system comprising:

• a skid component attached to an aircraft, wherein the skid component further comprises:
• a first skid tube oriented laterally to a longitudinal axis of the aircraft;
• a second skid tube oriented laterally to the longitudinal axis of the aircraft, wherein the second skid tube is parallel to the first skid tube;
• a first wheel journaled on a first rotational fulcrum;
• a second wheel journaled on a second rotational fulcrum;
• a first biasing means attaching the first rotational fulcrum to the first skid tube;
• and
• a second biasing means attaching the second rotational fulcrum to the second skid tube;
• wherein the first biasing means, and second biasing means exert a recoil force resisting upward displacement of the first rotational fulcrum and second rotational fulcrum with respect to the first skid tube and the second skid tube, and wherein each of the first biasing means and the second biasing means further comprise at least a leaf spring.