UH-60 Systems 1 Study Guide – Flashcards
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The UH-60 (Blackhawk) is a _____, single rotor, semi-monocoque stressed skin constructed fuselage, rotary wing helicopter.
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Twin turbine engine
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The _____ is a fully articulated, four blade, main rotor head, consisting of four subsystems; main rotor blades, hub, flight controls and the bifilar vibration absorber.
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Main rotor
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A rigid crossbeam, two blade, four paddle tail rotor system provides _____.
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Anti-torque action and directional control
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The helicopter has a conventional, ______ landing gear consisting of two main gear assemblies and a tail wheel assembly.
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Non-retractable
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The __________ canted tail rotor also provides _____ of the total lifting force in a hover.
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20 degrees, 2.5%
