Maximum ramp Weight : Maximum weight of the airplane at maximum takeoff weight plus fuel for taxi and run-up Maximum Zero Fuel Weight: Maximum weight of the loaded airplane with zero fuel. Climb - Cruise - Ceiling Useful Load Safety - Two Engines - Redundant Systems Complexity - Dual Systems - Avionics Single Engine Operations Cost Efficiency측면 - Parasite Drag - Fuel Consumption Maintenance측면 - Two engines - Complex SystemĤ Theory Critical Performance is rate of climb in the event of an Engine Failure Misconception: 50% loss of Power would result in 50% loss in climb performance Truth: 50% in loss of horsepower, and reduction of more than 80% climb performance Must consider all the drag and weight on dead engine Presentation on theme: "Multi-Engine과정."- Presentation transcript:ģ Multi Engine 장단점 장 점 (Advantages) 단 점 (Disadvantages) Performance
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