22.14.8 Describe the effects of airspeed and slipstream on control effectiveness
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22.14.10 Explain the basic principles of trim tabs, and describe the correct method of using trim controls
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22.14.12 Explain the reason for aerodynamic balancing of control surf
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22.14.14 Describe the main methods for achieving control balance.
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22.14.16 Differentiate between a balance tab and an anti-balance tab.
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22.14.18 Explain the purpose for mass balancing.
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22.14.20 Describe and explain flexural and torsional flutter.
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22.14.22 Describe the methods of providing mass balance.
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22.16.2 Explain the stalled condition of an aerofoil.
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22.16.4 Explain basic stall speed and relate it to the lift formula.
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22.16.6 Describe typical symptoms and other indications of the approach to the stall.
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22.16.8 Describe the changes in the airflow over the wing, movement of the CP, and aircraft attitude as the point of stall is reached.
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22.16.12 Describe how the following factors affect stalling speed:
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22.16.16 Explain the design measures taken to reduce the tendency for wing-drop.
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22.16.18 Explain the caution against using aileron near or at the stalling angle
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22.16.20 Describe the standard technique for recovery:
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22.16.22 Explain the process of autorotation (leading to the spin).
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22.16.24 Describe the characteristics of the upright spin, and explain:
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22.18.4 For a conventional aeroplane configuration, describe:
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22.18.8 For unaccelerated level flight:
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22.18.10 Given typical power available and power required curves, exp
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22.20.2 Identify the forces acting in a steady climb.
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22.20.4 Given typical power required and power available curves, exp
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22.20.6 State what the Vx and Vy speeds are and differentiate betwee
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