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C 17 Flotation Equipment Deployment System

Each C17 winglet spans 9 feet 4 inches Powered Lift STOL Capability A key element of the C17 is the special flap system first developed by a team of researchers at NASALangley in the mid1950s and later demonstrated on the YC15 prototype The externally blownflap or poweredlift system enables the aircraft to make slow steep

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