22.26.12 Explain the requirement to match lateral and directional sta
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22.26.14 Explain the conditions of spiral instability, dutch roll, an
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22.26.18 For a single-engine propeller aircraft, explain the factors
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22.26.20 Describe cross-wind take-off and landing techniques.
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22.26.22 Explain ground effect, and relate it to take-off and landing
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22.28.2 Explain the consideration involved in coping with asymmetric
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22.28.12 Define Vmca and Vmcg.
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22.28.6 Define critical engine.
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22.30.4 State the general conditions for achieving maximum SAR.
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22.28.10 Explain the three modes of constant-heading asymmetric fligh
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22.30.8 Apply performance tables or graphs from an aircraft manual to determine best SAR under given conditions.
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22.30.6 Explain the airframe and engine considerations of flying for range (piston engine)
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22.30.10 Define flying for endurance and differentiate between range
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22.30.12 State the factors affecting endurance and explain practical endurance flying techniques
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Flight paths
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Landing distance available
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Runway surface
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22.32.4 Explain the factors affecting take-off and landing performance
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22.32.6 Given an elevation, QNH and ambient temperature, calculate p
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22.32.8 Express an ambient temperature as a deviation from ISA temperature
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22.32.10 Demonstrate an ability to use wind-component graphs, and to apply runway slope and surface correction factors
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22.32.12 Demonstrate an ability to calculate take-off and landing performance in accordance with CAR Part 135 Subpart D using representative aeroplane take-off and landing performance charts (P-charts)
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22.32.14 Demonstrate an ability to calculate en-route engine inoperative performance using a representative single-engine service ceiling graph
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