12.22.8 Describe the operation and correct handling of ignition/starter switch systems.Sub Topic Syllabus Item
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12.24.2 State the safety precautions to be taken before starting the engine.
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12.24.4(c) starting a hot engine;
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12.24.4(d) controlling an engine fire on start-up;
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12.24.4(e) checking oil pressure after start;
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12.24.4(f) stopping the engine.
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12.24.6 Explain the reasons for avoidance of rapid power changes.
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12.24.8 Explain the need for monitoring and cross-checking engine instrument indications.
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12.24.10 State the possible causes for rough running or excessive engine vibration.
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12.24.14 State the possible causes of a sudden engine failure in flight, and the remedies which may be available to a pilot during subsequent trouble checks.
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12.24.12 State the actions that the pilot may take to identify and rectify rough running or excessive engine vibration.
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* * * Electrical System - DC * * *
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12.26 Electrical System - DC
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12.26.4 Explain the function of the following components in a typical light aircraft electrical system:
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12.26.4(a) battery;
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12.26.2 Describe the types of systems which are typically electrically operated in a light aircraft.
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12.26.4(b) alternator and generator;
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12.26.4(c) bus bar;
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12.26.4(d) voltage regulator, voltmeter, or over voltage light;
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12.26.4(e) ammeter;
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12.26.4(f) master switch and battery/alternator switches;
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12.26.4(g) fuses and circuit breakers.
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12.26.6 Explain the precautions to take during normal operation of the electrical system,including:
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12.26.6(a) avoiding continuous operation of high-power systems on the ground before start;
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