An aircraft comprising: a nose gear; main landing gear (12,14); a main hydraulic system and a remote hydraulic system with a hydraulic load, the remote hydraulic system comprising: a supply pressure accumulator configured to supply hydraulic fluid to the hydraulic load; a pressure sensor configured to detect a hydraulic pressure in the supply pressure accumulator; a pump in fluid communication with the supply pressure accumulator, wherein the pump is configured to switch on in response to the pressure sensor detecting the hydraulic pressure below a threshold value; and a return pressure accumulator configured to store the hydraulic fluid returning from the hydraulic load, wherein the pump is configured to drive fluid from the return pressure accumulator to the supply pressure accumulator, wherein the hydraulic load comprises a hydraulic actuator, wherein the remote hydraulic system is located remotely from the main hydraulic system, the remote hydraulic system being in fluid communication with hydraulic components of the nose gear of the aircraft and being hydraulically isolated from the main hydraulic system that drives the main landing gear (12,14) of the aircraft, wherein the hydraulic actuator is configured for at least one of steering a nose gear, deploying the nose gear, retracting the nose gear, locking a position of the nose gear, deploying a nose gear door, retracting the nose gear door, or locking a position of the nose gear door. a nose gear; main landing gear (12,14); a main hydraulic system and a remote hydraulic system with a hydraulic load, the remote hydraulic system comprising: a supply pressure accumulator configured to supply hydraulic fluid to the hydraulic load; a pressure sensor configured to detect a hydraulic pressure in the supply pressure accumulator; a pump in fluid communication with the supply pressure accumulator, wherein the pump is configured to switch on in response to the pressure sensor detecting the hydraulic pressure below a threshold value; and a return pressure accumulator configured to store the hydraulic fluid returning from the hydraulic load, wherein the pump is configured to drive fluid from the return pressure accumulator to the supply pressure accumulator, a supply pressure accumulator configured to supply hydraulic fluid to the hydraulic load; a pressure sensor configured to detect a hydraulic pressure in the supply pressure accumulator; a pump in fluid communication with the supply pressure accumulator, wherein the pump is configured to switch on in response to the pressure sensor detecting the hydraulic pressure below a threshold value; and a return pressure accumulator configured to store the hydraulic fluid returning from the hydraulic load, wherein the pump is configured to drive fluid from the return pressure accumulator to the supply pressure accumulator, wherein the hydraulic load comprises a hydraulic actuator, wherein the remote hydraulic system is located remotely from the main hydraulic system, the remote hydraulic system being in fluid communication with hydraulic components of the nose gear of the aircraft and being hydraulically isolated from the main hydraulic system that drives the main landing gear (12,14) of the aircraft, wherein the hydraulic actuator is configured for at least one of steering a nose gear, deploying the nose gear, retracting the nose gear, locking a position of the nose gear, deploying a nose gear door, retracting the nose gear door, or locking a position of the nose gear door.