Cabin attendant aircraft seat leg rest with foot support

1. A cabin attendant aircraft seat comprising:

a support system including a seatback frame and a seat pan frame;

a seat pan cover including at least one surface configured to conform to a corresponding surface of the support system;

a seatback cover including at least one surface configured to conform to a corresponding surface of the support system; and

a leg rest with foot support assembly configured to couple to a portion of the seat pan frame, the leg rest with foot support assembly comprising:

a support sub-assembly configured to provide at least one of leg support or foot support, the support sub-assembly comprising:

a panel; and

a support cushion, the support cushion configured to couple to a portion of the panel, the support cushion including a cavity defined by one or more surfaces of the support cushion, wherein the cavity of the support cushion is configured to receive a portion of a user's foot to translate the leg rest with foot support assembly; and

a translation sub-assembly configured to translate the leg rest with foot support assembly between a first position and one or more additional positions, the translation sub-assembly comprising:

one or more translation arms configured to couple to one or more portions of the support sub-assembly, the one or more translation arms further configured to couple to one or more portions of the seat pan frame;

one or more guide rails configured to couple to the one or more translation arms;

one or more linear bearings configured to engage with the one or more guide rails, the one or more linear bearings slideable along a length of the one or more guide rails; and

one or more translation devices configured to translate the support sub-assembly between the first position and the one or more additional positions when the one or more linear bearings slide along the length of the one or more guide rails.

2. The cabin attendant aircraft seat of claim 1 , wherein the panel includes one or more flanges, the one or more flanges configured to couple to one or more portions of the support cushion to align the support cushion with the panel.

3. The cabin attendant aircraft seat of claim 1 , wherein the support sub-assembly further comprises:

one or more side caps.

4. The cabin attendant aircraft seat of claim 1 , wherein at least one of the one or more surfaces of the support cushion is angled.

5. The cabin attendant aircraft seat of claim 1 , wherein the support sub-assembly further comprises:

a rub strip configured to reversibly couple to a portion of the support cushion.

6. The cabin attendant aircraft seat of claim 1 , wherein the one or more translation devices includes one or more bungee cords.

7. The cabin attendant aircraft seat of claim 6 , wherein the translation sub-assembly further comprises:

a plurality of bungee clamps configured to couple the one or more bungee cords to the leg rest with foot support assembly.

8. The cabin attendant aircraft seat of claim 7 , wherein the plurality of bungee clamps include a first set of one or more bungee cords configured to couple the one or more bungee cords to one or more portions of the support sub-assembly, the plurality of bungee clamps further include a second set of one or more bungee cords configured to couple the one or more bungee cords to one or more portions of the translation sub-assembly.

9. The cabin attendant aircraft seat of claim 1 , wherein the one or more guide rails include one or more travel limiters, the one or more travel limiters configured to prevent the one or more linear bearings from disengaging with the one or more guide rails.

10. The cabin attendant aircraft seat of claim 1 , wherein the one or more translation devices are configured to stow the leg rest in the first position, the first position including an un-extended position.

11. The cabin attendant aircraft seat of claim 1 , wherein the support sub-assembly is configured to translate between the first position and the one or more additional positions when pressure is applied by the user's foot in a direction outward from the cavity of the support cushion.

12. The cabin attendant aircraft seat of claim 11 , wherein the first position includes an un-extended position, the one or more additional positions including one of an extended position or one or more intermediate positions.

13. The cabin attendant aircraft seat of claim 11 , wherein the support sub-assembly is configured to automatically retract to the first position when pressure is released from the cavity of the support cushion, the first position including an un-extended position.

14. A leg rest with foot support assembly comprising:

a support sub-assembly configured to provide at least one of leg support or foot support, the support sub-assembly comprising:

a panel; and

a support cushion, the support cushion configured to couple to a portion of the panel, the support cushion including a cavity defined by one or more surfaces of the support cushion, wherein the cavity of the support cushion is configured to receive a portion of a user's foot to translate the leg rest with foot support assembly; and

a translation sub-assembly configured to translate the support sub-assembly between a first position and one or more additional positions, the translation sub-assembly comprising:

one or more translation arms configured to couple to one or more portions of the support sub-assembly, the one or more translation arms further configured to couple to one or more portions of a seat pan frame of an aircraft seat;

one or more guide rails configured to couple to the one or more translation arms;

one or more linear bearings configured to engage with the one or more guide rails, the one or more linear bearings slideable along a length of the one or more guide rails; and

one or more translation devices configured to translate the support sub-assembly between the first position and the one or more additional positions when the one or more linear bearings slide along the length of the one or more guide rails.