ETOPS AVA (1-100) STUDY

ava-1-100-study

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Question 1 of 1

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1 The primary reason the angle of attack must be increased, to maintain a constant altitude during a coordinated turn, is because the

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273418

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2 Which is true regarding the use of flaps during level turns?

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3 Defines VNO as

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4 Airplane wing loading during a level coordinated turn in smooth air depends upon the

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5 The stalling speed of an airplane is most affected by

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6 During the transition from straight-and-level flight to a climb, the angle of attack is increased and lift

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7 Load factor is the lift generated by the wings of an aircraft at any given time

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8 Lift on a wing is most properly defined as the

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9 While holding the angle of bank constant in a level turn, if the rate of turn is varied the load factor would

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10 Which is true regarding the forces acting on an aircraft in a steady-state descent? The sum of all

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11 What performance is characteristic of flight at maximum lift/drag ratio in a propeller-driven airplane? Maximum

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12 The need to slow an aircraft below VA is brought about by the following weather phenomenon:

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13 In theory, if the airspeed of an airplane is doubled while in level flight, parasite drag will become

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14 As airspeed decreases in level flight below that speed for maximum lift/drag ratio, total drag of an airplane

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ETOPS AVA (1-100) STUDY

Question 1 of 1

Time Left

1 The primary reason the angle of attack must be increased, to maintain a constant altitude during a coordinated turn, is because the

Select the correct answer(s).

(0/0)

2 Which is true regarding the use of flaps during level turns?

Select the correct answer(s).

(0/0)

3 Defines VNO as

Select the correct answer(s).

(0/0)

4 Airplane wing loading during a level coordinated turn in smooth air depends upon the

Select the correct answer(s).

(0/0)

5 The stalling speed of an airplane is most affected by

Select the correct answer(s).

(0/0)

6 During the transition from straight-and-level flight to a climb, the angle of attack is increased and lift

Select the correct answer(s).

(0/0)

7 Load factor is the lift generated by the wings of an aircraft at any given time

Select the correct answer(s).

(0/0)

8 Lift on a wing is most properly defined as the

Select the correct answer(s).

(0/0)

9 While holding the angle of bank constant in a level turn, if the rate of turn is varied the load factor would

Select the correct answer(s).

(0/0)

10 Which is true regarding the forces acting on an aircraft in a steady-state descent? The sum of all

Select the correct answer(s).

(0/0)

11 What performance is characteristic of flight at maximum lift/drag ratio in a propeller-driven airplane? Maximum

Select the correct answer(s).

(0/0)

12 The need to slow an aircraft below VA is brought about by the following weather phenomenon:

Select the correct answer(s).

(0/0)

13 In theory, if the airspeed of an airplane is doubled while in level flight, parasite drag will become

Select the correct answer(s).

(0/0)

14 As airspeed decreases in level flight below that speed for maximum lift/drag ratio, total drag of an airplane

Select the correct answer(s).

(0/0)

15 If the airspeed is increased from 90 knots to 135 knots during a level 60° banked turn, the load factor will

Select the correct answer(s).

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