A bearing for a hinge in a hinged raked aircraft wing tip , the bearing comprising: an outer member having an interior area defined by a concave inner surface ; an inner member assembly having a first inner segment and a second inner segment , the first inner segment having a first base and a first bearing section extending axially from the first base, the second inner segment having a second base and a second bearing section extending axially from the second base, and the first bearing section and the second bearing section together forming a convex outer surface that is complementary in shape to the concave inner surface ; a preload feature positioned between and engaging at least a portion of the first bearing section and the second bearing section; a lubricous liner positioned between the concave inner surface and the convex outer surface ; at least a portion of the first bearing section and the second bearing section are positioned in the interior area so that the preload feature is compressed at least one of radially and axially inward and is biased at least one of radially and axially outward to limit axial movement between the outer member and the inner member assembly to a predetermined magnitude; and the preload feature is adapted to flex at least one of radially and axially outward as a result of wear to the liner to maintain the axial movement to the predetermined magnitude. an outer member having an interior area defined by a concave inner surface ; an inner member assembly having a first inner segment and a second inner segment , the first inner segment having a first base and a first bearing section extending axially from the first base, the second inner segment having a second base and a second bearing section extending axially from the second base, and the first bearing section and the second bearing section together forming a convex outer surface that is complementary in shape to the concave inner surface ; an inner member assembly having a first inner segment and a second inner segment , the first inner segment having a first base and a first bearing section extending axially from the first base, the second inner segment having a second base and a second bearing section extending axially from the second base, and the first bearing section and the second bearing section together forming a convex outer surface that is complementary in shape to the concave inner surface ; a preload feature positioned between and engaging at least a portion of the first bearing section and the second bearing section; a lubricous liner positioned between the concave inner surface and the convex outer surface ; at least a portion of the first bearing section and the second bearing section are positioned in the interior area so that the preload feature is compressed at least one of radially and axially inward and is biased at least one of radially and axially outward to limit axial movement between the outer member and the inner member assembly to a predetermined magnitude; and the preload feature is adapted to flex at least one of radially and axially outward as a result of wear to the liner to maintain the axial movement to the predetermined magnitude. <EOS>