A system for aircraft lavatory touchless water control, comprising: a touchless manifold system having a cold conduit, a hot conduit, a mixing chamber, and a mixed conduit, the touchless manifold system including a cold inlet coupled with the cold conduit and configured to couple with an aircraft cold water supply; a hot inlet coupled with the hot conduit and configured to couple with an aircraft hot water supply; an aircraft data connection; a faucet data connection; a manifold microcontroller operatively coupled with the aircraft data connection and the faucet data connection; a cold thermal sensor proximal with the cold inlet and configured to measure a temperature of a cold fluid within the cold conduit, the cold thermal sensor operatively coupled with the manifold microcontroller; a hot thermal sensor proximal with the hot inlet and configured to measure a temperature of a hot fluid within the hot conduit, the hot thermal sensor operatively coupled with the manifold microcontroller; a cold solenoid operatively coupled with the manifold microcontroller and a cold solenoid valve, the cold solenoid valve configured to control a flow of the cold fluid within the cold conduit; a hot solenoid operatively coupled with the manifold microcontroller and a hot solenoid valve, the hot solenoid valve configured to control a flow of the hot fluid within the hot conduit; the mixing chamber proximal with each of the cold solenoid valve, the hot solenoid valve, and the mixed conduit, the mixing chamber configured to receive an output from each of the cold and hot solenoid valves and deliver a mixed flow to the mixed conduit; the manifold microcontroller configured for: receiving a temperature command via the aircraft data connection; receiving a cold temperature reading from the cold thermal sensor and a hot temperature reading from the hot thermal sensor; receiving a faucet data signal via the faucet data connection configured to be associated with a touchless faucet, the faucet data signal including a faucet valve signal from a faucet valve sensor; a cold selection signal from a faucet cold selection sensor; a hot selection signal from a faucet hot selection sensor; mixing the cold flow with the hot flow via a timing command of the cold solenoid and the hot solenoid based on 1) the temperature command, 2) the cold and hot temperature reading, and 3) the faucet data signal. a touchless manifold system having a cold conduit, a hot conduit, a mixing chamber, and a mixed conduit, the touchless manifold system including a cold inlet coupled with the cold conduit and configured to couple with an aircraft cold water supply; a hot inlet coupled with the hot conduit and configured to couple with an aircraft hot water supply; an aircraft data connection; a faucet data connection; a manifold microcontroller operatively coupled with the aircraft data connection and the faucet data connection; a cold thermal sensor proximal with the cold inlet and configured to measure a temperature of a cold fluid within the cold conduit, the cold thermal sensor operatively coupled with the manifold microcontroller; a hot thermal sensor proximal with the hot inlet and configured to measure a temperature of a hot fluid within the hot conduit, the hot thermal sensor operatively coupled with the manifold microcontroller; a cold solenoid operatively coupled with the manifold microcontroller and a cold solenoid valve, the cold solenoid valve configured to control a flow of the cold fluid within the cold conduit; a hot solenoid operatively coupled with the manifold microcontroller and a hot solenoid valve, the hot solenoid valve configured to control a flow of the hot fluid within the hot conduit; the mixing chamber proximal with each of the cold solenoid valve, the hot solenoid valve, and the mixed conduit, the mixing chamber configured to receive an output from each of the cold and hot solenoid valves and deliver a mixed flow to the mixed conduit; the manifold microcontroller configured for: receiving a temperature command via the aircraft data connection; receiving a cold temperature reading from the cold thermal sensor and a hot temperature reading from the hot thermal sensor; receiving a faucet data signal via the faucet data connection configured to be associated with a touchless faucet, the faucet data signal including a faucet valve signal from a faucet valve sensor; a cold selection signal from a faucet cold selection sensor; a hot selection signal from a faucet hot selection sensor; mixing the cold flow with the hot flow via a timing command of the cold solenoid and the hot solenoid based on 1) the temperature command, 2) the cold and hot temperature reading, and 3) the faucet data signal. receiving a temperature command via the aircraft data connection; receiving a cold temperature reading from the cold thermal sensor and a hot temperature reading from the hot thermal sensor; receiving a faucet data signal via the faucet data connection configured to be associated with a touchless faucet, the faucet data signal including a faucet valve signal from a faucet valve sensor; a cold selection signal from a faucet cold selection sensor; a hot selection signal from a faucet hot selection sensor; a faucet valve signal from a faucet valve sensor; a cold selection signal from a faucet cold selection sensor; a hot selection signal from a faucet hot selection sensor; mixing the cold flow with the hot flow via a timing command of the cold solenoid and the hot solenoid based on 1) the temperature command, 2) the cold and hot temperature reading, and 3) the faucet data signal.