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EASA DGCA Module 3.2Static Electricity and Conduction (3of3)
Sub-Module 02 - LEVEL-2 Static Electricity and Conduction Static electricity and distribution of electrostatic charges; Electrostatic laws of attraction and repulsion; Units of charge, Coulomb's Law; Conduction of electricity in solids, liquids, gases and a vacuum.
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What could happen if an aircraft with static charge lands without proper discharge?
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What phenomenon does the bonding system help to prevent within an aircraft *
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What causes corona discharge on an aircraft? *
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Which part of the aircraft typically has the highest potential for corona discharge? *
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What additional protection is required for aircraft using sophisticated digital computing techniques?
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Why is the bonding of a fuel tanker to the aircraft important during refueling? *
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Why is it undesirable to have a potential difference between the aircraft and the ground after landing? *
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How does the bonding system affect radio and navigational aid signals? *
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What are static discharge wicks used for on an aircraft? 
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What is the purpose of the tungsten needles on static dischargers? *
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What can corona discharge lead to in poor visibility conditions? *
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How are high-performance non-metallic materials advantageous in aircraft?
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What is the role of capacitors in suppressors used in screening systems? *
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Where are static discharge wicks typically located on an aircraft? 
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What materials are used in new technology aircraft to reduce static charge buildup? 
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What is the primary function of the bonding conductors used for flight control surfaces? *
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What is the function of screening in electrical systems of an aircraft? 
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What type of materials is used in the construction of static discharge *
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What is one method to provide a leakage path for static charge dissipation in an aircraft?
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What is one method used to screen cables in an aircraft?
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How can the risk of fire or explosion be minimized during aircraft refueling?
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Why must the metal screens and suppressors be connected to the main earth or ground system?
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