The ignition system generally used for small aircrafts is a:4
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In general, in twin-engine aeroplanes with 'constant speed propeller'4
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The power of a piston engine decreases during a climb with a constant power lever setting because of the decreasing:4
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The power output of a piston engine can be calculated by:4
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The useful work area in an ideal Otto engine indicator diagram is enclosed by the following gas state change lines4
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For a given type of oil, the oil viscosity depends on the:4
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When applying carburettor heating:4
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Load shedding means:4
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The primary purpose of the reverse current relay is to:4
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Regarding Ohm's law:4
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