A camber condition is caused by the tire being out of perpendicular plane to the ground and the aircraft landing gear. In this condition, the tire footprint becomes trapezoidal in shape causing an asymmetric pressure distribution from one shoulder of the tire to the other. The higher footprint pressure along the extended shoulder contact generates accelerated wear in the tire. This can be seen in the tire as a slope wear from one shoulder to the other or as a rapid wear on one shoulder only, as is seen in Figure 10 below.