AIRCRAFT LANDING GEAR

The invention relates to an aircraft landing gear comprising an axle (3) intended to receive a wheel (4) comprising a rim (6) mounted to rotate on the axle (3) by means of at least one bearing (8), said bearing (8) comprising an inner ring (11) mounted around the axle (3) and an outer ring (12) rotationally fixed to the rim (6) of the wheel (4), the landing gear further comprising measuring means (21) intended to perform measurements of at least one operating parameter of the landing gear. The measuring means (21) are integrated into the bearing (8) by being fixed to one of the inner or outer rings of the bearing (8).