PPL Principals of Flight 06

Forces acting on an aeroplane

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In steady, straight and level flight, which statement is correct about the four forces acting on the aircraft?

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If the weight reduces, the thrust required for straight and level flight is then:

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If the weight increases, then the thrust required for straight and level flight will:

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In a steady, straight climb, the climb angle will increase with __(1)__, and reduce with __(2)__ (assuming all other factors constant).

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The best rate of climb speed for a SEP/MEP is: __(1)__ and, approximately corresponds to __(2)__.

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The best angle of climb speed for a SEP/MEP is called: __(1)__, and approximately corresponds to __(2)__ in still air.

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In a straight, steady climb, the rate of climb increases with: __(1)__, and reduces with __(2)__ if other factors stay the same.

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What is the speed that results in the longest glide range in still air?

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If using a lower speed below VMD for a steady descent, and assuming that all other factors are constant, then:

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If using a higher speed below VMD for a steady descent, and assuming that all other factors are constant, then:

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What is the speed that results in the longest glide range in a headwind?

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What is the speed that results in the longest glide range in a tailwind?

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What is the effect on the rate of descent if using higher speeds than VMP for a steady descent (assuming that all other factors remain constant)?

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What happens to the take-off distance, when using zero flap deflection for take-off and climb?

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What happens to the take-off distance when using a higher flap setting for take-off and climb?

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What happens if the pilot increases the bank angle during a steady, coordinated turn?

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What does increasing angle of climb have on the load factor?

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How would you reduce the turn radius of a steady, coordinated turn:

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To maintain a rate-one-turn, you should maintain a bank of approximately ..... while flying at 100 KIAS.

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Complete the sentence: The greater the descent angle, the ......

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What does a rate-one-turn mean?

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When using a higher flap deflection angle for both approach and landing, then...

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The straight, steady descent angle increases, if the throttle: