An aircraft window assembly, comprising: a window frame configured to support a window pane on an aircraft skin around a circumference of a window aperture defined in the aircraft skin and to align the window pane with the window aperture, wherein the window frame comprises: a base formed of a continuous fiber reinforced thermoplastic composite, wherein the base is ring-shaped and defines a central aperture, and wherein the base comprises: a circumferential flange portion defining a radial exterior of the base and configured to support the base on the aircraft skin surrounding the window aperture; a skirt portion extending radially inwardly from the circumferential flange portion and surrounding the central aperture, wherein the skirt portion is non-planar with the circumferential flange portion and comprises a support surface for supporting the window pane of the aircraft window assembly; characterized by: at least one overmolded feature molded to the base; wherein the aircraft window assembly further comprises a plurality of window frame fastener bores extending through and spaced-apart around the circumferential flange portion and configured to receive a respective plurality of window frame fasteners to retain the window frame to the aircraft skin, wherein the at least one overmolded feature comprises a plurality of overmolded protrusions, wherein each overmolded protrusion is molded atop a window frame fastener bore of the plurality of window frame fastener bores, and wherein each overmolded protrusion is configured to receive a window frame fastener receiver, and wherein each window frame fastener receiver is configured to receive and engage a window frame fastener of the plurality of window frame fasteners. a base formed of a continuous fiber reinforced thermoplastic composite, wherein the base is ring-shaped and defines a central aperture, and wherein the base comprises: a circumferential flange portion defining a radial exterior of the base and configured to support the base on the aircraft skin surrounding the window aperture; a skirt portion extending radially inwardly from the circumferential flange portion and surrounding the central aperture, wherein the skirt portion is non-planar with the circumferential flange portion and comprises a support surface for supporting the window pane of the aircraft window assembly; a circumferential flange portion defining a radial exterior of the base and configured to support the base on the aircraft skin surrounding the window aperture; a skirt portion extending radially inwardly from the circumferential flange portion and surrounding the central aperture, wherein the skirt portion is non-planar with the circumferential flange portion and comprises a support surface for supporting the window pane of the aircraft window assembly; characterized by: at least one overmolded feature molded to the base; wherein the aircraft window assembly further comprises a plurality of window frame fastener bores extending through and spaced-apart around the circumferential flange portion and configured to receive a respective plurality of window frame fasteners to retain the window frame to the aircraft skin, wherein the at least one overmolded feature comprises a plurality of overmolded protrusions, wherein each overmolded protrusion is molded atop a window frame fastener bore of the plurality of window frame fastener bores, and wherein each overmolded protrusion is configured to receive a window frame fastener receiver, and wherein each window frame fastener receiver is configured to receive and engage a window frame fastener of the plurality of window frame fasteners. at least one overmolded feature molded to the base; wherein the aircraft window assembly further comprises a plurality of window frame fastener bores extending through and spaced-apart around the circumferential flange portion and configured to receive a respective plurality of window frame fasteners to retain the window frame to the aircraft skin, wherein the at least one overmolded feature comprises a plurality of overmolded protrusions, wherein each overmolded protrusion is molded atop a window frame fastener bore of the plurality of window frame fastener bores, and wherein each overmolded protrusion is configured to receive a window frame fastener receiver, and wherein each window frame fastener receiver is configured to receive and engage a window frame fastener of the plurality of window frame fasteners.