Wing for an aircraft

A wing for an aircraft, comprising:

• a main wing;
• and
• a high lift assembly comprising:
• a high lift body, and
• a connection assembly movably connecting the high lift body to the main wing, such that the high lift body is movable between a retracted position and at least one extended position,
• wherein the connection assembly comprises an elongate track extending along a track longitudinal axis between a first end and a second end and has an intermediate portion between the first and second ends,
• wherein the first end and/or the intermediate portion of the track is mounted to the high lift body,
• wherein the track is mounted to the main wing via a roller bearing such that the track is movable along the track longitudinal axis,
• wherein the roller bearing comprises at least one roller pair comprising a first and a second roller, each of the first and second roller mounted to at least one of the main wing and the track via a respective first and second eccentric connector assembly,
• wherein the first and second eccentric connector assemblies are configured to be engaged simultaneously by a single alignment member for synchronous rigging of the first and second rollers,
• wherein the first and second eccentric connector assemblies each comprises a respective first and second mounting portion for coupling to at least one of the main wing and the track and a respective first and second bearing portion for coupling to the respective first and second roller,
• wherein at least part of each mounting portion is rotatable about a respective first and second connector rotation axis relative to at least one of the main wing and the track, and each of the first and second roller is rotatable about a respective first and second roller rotation axis relative to the respective bearing portion,
• wherein each of the first and second connector rotation axis is offset from the respective roller rotation axis such that engagement and rotation, by the single alignment member, of the first and second mounting portions about the respective connector rotation axis effects corresponding rotation of the respective roller rotation axis about the connector rotation axis and synchronous rigging of the first and second rollers, and
• wherein the first and second connector assemblies each comprises an elongate connector, a mounting sleeve located on the elongate connector to define the mounting portion and a bearing sleeve located on the elongate connector to define the bearing portion, the mounting sleeve being axially offset along the elongate connector from the bearing sleeve.