The fuel system is designed to provide an uninterrupted flow of clean fuel from the fuel tanks to the engine. The fuel must be available to the engine under all conditions of engine power, altitude, attitude, and during all approved flight maneuvers. Two common classifications apply to fuel systems in small airplanes�gravity-feed and fuel-pump systems.
The gravity-feed system utilizes the force of gravity to transfer the fuel from the tanks to the engine�for example, on high-wing airplanes where the fuel tanks are installed in the wings. This places the fuel tanks above the carburetor, and the fuel is gravity fed through the system and into the carburetor. If the design of the airplane is such that gravity cannot be used to transfer fuel, fuel pumps are installed�for example, on low-wing airplanes where the fuel tanks in the wings are located below the carburetor.
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