12.58.20 Explain the requirement for using anti-balance tabs on an all-moving tailplane.
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12.58.22 Describe the principle of operation of anti-balance tabs.
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12.58.24 Explain the purpose of wing flaps.
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12.58.26 Describe the principle of operation of wing flaps.
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* * * Straight and Level Flight * * *
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12.60 Straight and Level Flight
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12.60.2 Define the four main forces acting in flight.
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12.60.4 For level flight describe how the four main forces change as IAS is varied.
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12.60.6 Describe the pitching moments in flight, and how longitudinal stability isachieved.
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12.60.8 Given a basic graph of power available (PA) and power required (PR) versus TASin level flight, show the derivation of:
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12.60.8(a) maximum and minimum level flight speed;
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12.60.8(b) maximum-range speed;
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12.60.8(c) maximum endurance speed.
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12.60.10 Explain the basic operational considerations which apply to flying an aeroplanefor range, or endurance.
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* * * Climbing Flight * * *
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12.62 Climbing Flight
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12.62.2 Using a diagram, show and name the forces acting in a steady climb.
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12.62.4 Distinguish between:
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12.62.4(a) maximum angle of climb;
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12.62.4(b) maximum rate of climb; Sub Topic Syllabus Item
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12.62.4(c) cruise climb
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12.62.6 Define the meaning of Vx (max angle) and Vy (max rate).
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12.62.8 Using a PA/PR (power available/power required) graph, show the derivation ofmaximum rate of climb speed.
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12.62.10 Briefly explain the factors which affect climb performance.
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