An aircraft mirror assembly comprising: a light source ; a front cover , wherein the front cover is semi-transparent; and a light guide arranged adjacent to the front cover , the light source being arranged adjacent to an edge of the light guide , and the front cover comprising at least one illumination zone (114, 114A-B), and in an activated configuration, the light guide being configured to direct light from the light source to the illumination zone such that light is directed through the illumination zone of the front cover, and a back cover opposite from the front cover , wherein the front cover further comprises at least one indicator (120, 120A-D) controllable between an activated configuration and a deactivated configuration, wherein, in the activated configuration, the at least one indicator (120, 120A-D) is activated on a front surface of the front cover , and wherein, in a deactivated configuration, the at least one indicator (120, 120A-D) is deactivated and concealed on the front surface of the front cover , the at least one illumination zone (114, 114A-B) being controllable between an activated configuration and a deactivated configuration, and wherein the at least one illumination zone (114, 114A-B) and the at least one indicator (120, 120A-D) are independently controllable between the activated configuration and the deactivated configuration, characterised in that the back cover comprises at least one back cover illumination zone, and wherein, in an activated configuration, the light guide is configured to direct light from the light source to the back cover illumination zone such that light is directed through the back cover illumination zone of the back cover . a light source ; a front cover , wherein the front cover is semi-transparent; and a light guide arranged adjacent to the front cover , the light source being arranged adjacent to an edge of the light guide , and the front cover comprising at least one illumination zone (114, 114A-B), and in an activated configuration, the light guide being configured to direct light from the light source to the illumination zone such that light is directed through the illumination zone of the front cover, and a back cover opposite from the front cover , wherein the front cover further comprises at least one indicator (120, 120A-D) controllable between an activated configuration and a deactivated configuration, wherein, in the activated configuration, the at least one indicator (120, 120A-D) is activated on a front surface of the front cover , and wherein, in a deactivated configuration, the at least one indicator (120, 120A-D) is deactivated and concealed on the front surface of the front cover , the at least one illumination zone (114, 114A-B) being controllable between an activated configuration and a deactivated configuration, and wherein the at least one illumination zone (114, 114A-B) and the at least one indicator (120, 120A-D) are independently controllable between the activated configuration and the deactivated configuration, characterised in that the back cover comprises at least one back cover illumination zone, and wherein, in an activated configuration, the light guide is configured to direct light from the light source to the back cover illumination zone such that light is directed through the back cover illumination zone of the back cover . <EOS>