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Aircraft landing gear serves as a mechanism to support weight of the aircraft during landing, takeoff , taxiing and also provide a shock absorbing function. The The hydraulic power system provides a flow of pressurized hydraulic fluid to operate the landing gear system as well as the respective landing gear doors. Aircraft flying to and from the water surface have a landing system with pontoons. Any type of landing gear used, the aircraft shall be viewed as a portion of The gear features pontoons for water landing with extendable wheels for landings on hard surfaces. A similar system is used to allow the use of skis and wheels This paper presents a perspective on various stages of landing gear design and development, current technology landscape and how these technologies are helping Nose Landing Gear System Hydraulic Schematic Diagram (Sheet 1 of 2) . The shock strut is mounted to the aircraft by two trunnion pins that insert into