An aircraft undercarriage is provided (1). The undercarriage (1) includes a rocker lever (2) having a first end zone (2a) for fastening to at least one point of the structure of the aircraft and a second end zone (2b) connected via a swivel (3) to twin wheels (4) including a wheel axle (9) connecting together two landing wheels (R1, R2). The swivel (3) includes a first portion (3b) that is fastened to the second end zone (2b) of the rocker lever (2) and a second portion (3c) being free to swivel relative to the first portion (3b) about a swivel axis (A1, A2) of the swivel (3). the second portion (3c) is connected to the wheel axle (9) of the twin wheels (4). In addition, the connection between the second portion (3c) of the swivel (3) and the wheel axle (9) includes a hinge (6).
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