| CPC B64C 1/1492 (2013.01) | 20 Claims |

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1. An electric aircraft window shade system, comprising:
a frame configured to mount on an outer surface at an outer side of an inner wall of an aircraft at a window opening, the inner wall having an inner side opposite the outer side, wherein no portion of the frame is positioned on the inner side of the inner wall; and
a cassette configured to mount in the frame by being inserted through the window opening into the frame, the cassette having a top, a bottom, a first side and a second side, the cassette further having a shade element that is moveable between a lowered position and a raised position, and a motor to drive the shade element between the raised position and lowered position.
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