12.72.6(d) thrust and propeller torque.
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12.72.8 For a fixed-pitch propeller at a constant throttle setting, explain the relationshipbetween airspeed, angle of attack and rpm.
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12.72.10 Briefly explain the factors which affect the ability of a fixed-pitch propeller toconvert engine power into useful thrust.
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12.72.12 Explain the basic principle of operation for a constant-speed propeller, and thenormal procedure for changing power settings with the manifold pressure and pitch controls.
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12.72.14 State the principal advantage of a constant-speed versus a fixed-pitch propeller.
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12.72.16 Describe the function and operation of a typical reduction gearbox.
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* * * Control Systems * * *
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12.76 Control Systems
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12.76.2 Explain the common methods of the mechanical operation of the:
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12.76.2(a) primary flight controls;
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12.76.2(b) trim tab;
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12.76.2(c) flap systems.
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12.76.4 Describe the function of control locks and precautions for removal before flight.
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12.76.6 Describe the normal operational use of flaps, including limitations.Performance Sub Topic Syllabus Item
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* * * Performance Factors * * *
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12.100 Performance Factors
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12.100.2 Describe the general effects of altitude on aircraft performance.
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12.100.4 Define pressure altitude.
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12.100.6 Calculate aerodrome pressure altitude, given aerodrome elevation and prevailingQNH.
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12.100.8 Explain how to determine pressure altitude by using an altimeter.
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12.100.10 Explain the general effect of temperature on performance.
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12.100.12 Define density altitude.
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12.100.14 Given a pressure altitude and ambient temperature, calculate the:
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12.100.14(a) ISA deviation;
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