Flight Mechanics | PPL(A) Principles of Flight - EASA & UK CAA
Forces acting on an aeroplane
Section titled "Forces acting on an aeroplane"What is the speed that results in the longest glide range in a tailwind?
If using a lower speed below VMD for a steady descent, and assuming that all other factors are constant, then:
How would you reduce the turn radius of a steady, coordinated turn:
Complete the sentence: The greater the descent angle, the ......
What does a rate-one-turn mean?
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)?
To maintain a rate-one-turn, you should maintain a bank of approximately ..... while flying at 100 KIAS.
What is the speed that results in the longest glide range in still air?
What happens if the pilot increases the bank angle during a steady, coordinated turn?
If the weight reduces, the thrust required for straight and level flight is then:
What is the speed that results in the longest glide range in a headwind?
If using a higher speed below VMD for a steady descent, and assuming that all other factors are constant, then:
In a straight, steady climb, the rate of climb increases with: __(1)__, and reduces with __(2)__ if other factors stay the same.
In a steady, straight climb, the climb angle will increase with __(1)__, and reduce with __(2)__ (assuming all other factors constant).
The best angle of climb speed for a SEP/MEP is called: __(1)__, and approximately corresponds to __(2)__ in still air.
The straight, steady descent angle increases, if the throttle:
In steady, straight and level flight, which statement is correct about the four forces acting on the aircraft?
What happens to the take-off distance when using a higher flap setting for take-off and climb?
The best rate of climb speed for a SEP/MEP is: __(1)__ and, approximately corresponds to __(2)__.
When using a higher flap deflection angle for both approach and landing, then...
What happens to the take-off distance, when using zero flap deflection for take-off and climb?
If the weight increases, then the thrust required for straight and level flight will:
What does increasing angle of climb have on the load factor?