The Beaver is typically powered by a single Pratt & Whitney R-985 Wasp Junior radial engine. In order to provide the necessary weight balance for optimal loading flexibility, the engine was mounted as far rearwards as possible, resulting in elements intruding into the cockpit space, such as the oil tank being positioned within the center console between the pilot and copilot's feet and the main fuel tank within the forward belly of the aircraft, which also improves accessibility for replenishment. Many Beavers have had wingtip tanks also installed; careful fuel management between the various fuel tanks is required throughout flights in order to maintain the aircraft's center of gravity. The remanufactured DHC-2T Turbo Beaver is equipped with a PT6A-34 turboprop engine.