12.30.2(a) fuel tank, sump, drain point, supply line standpipe, vents, overflow drain;
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12.30.2(c) fuel tank construction and associated limitations.
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12.30.4 Describe the procedure to be used for a fuel drain check.
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12.30.6 State the general rules for fuelling of aircraft, including the special precautions for the use of drum stock, and plastic containers.
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* * * Lubrication Systems - Engines * * *
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12.32 Lubrication Systems - Engines
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12.32.4 Explain the term viscosity.
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12.32.6 Explain the effect of temperature on the lubricating qualities of oil.
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12.32.8 Briefly describe the function of the following components of an oil system:
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12.32.2 State the functions of an engine lubrication system.
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12.32.8(a) wet sump;
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12.32.8(b) dry sump, scavenge pump, tank; Sub Topic Syllabus Item
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12.32.8(c) engine-driven pump, pressure relief valve;
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12.32.8(d) oil lines, passages and galleries;
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12.32.8(e) oil cooler, bypass valves and filters;
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12.32.8(f) oil pressure and temperature gauges.
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12.32.10 Explain the importance of:
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12.32.10(b) checking the correct oil quantity before flight.
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12.32.10(a) using the correct type and grade of oil for a particular aircraft;
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12.32.12 Identify the possible oil system malfunctions indicated by:
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12.32.12(a) low/zero oil pressure;
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12.32.12(b) high oil pressure;
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12.32.12(c) fluctuating oil pressure;
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12.32.12(d) low oil temperature;
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