Steep Turns Flashcards

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1
Q

What angle constitutes a steep turn?

A

45 degrees or more

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2
Q

What is airplane load factor? What is the load factor at the surface at rest?

A

The forces acting on the structure of the aircraft, 1G at the surface of the earth with the airplane at rest

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3
Q

What is the formula for load factor?

A

Total air load / Weight of the airplane

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4
Q

What are the maneuvering limit load factors for a normal aircraft? Utility aircraft? Acrobatic aircraft?

A

3.8 positive Gā€™s, 1.52 negative / 4.4+, 1.76- / 6+, 3-

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5
Q

What is the sole determining variable for load factor on a normal aircraft?

A

Bank Angle, as bank angle increases, load factor does as well

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6
Q

What happens to stall speed as load factor increase?

A

Stall speed also increases

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7
Q

What is the maximum load factor on a stalled aircraft?

A

1 G

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8
Q

Describe the maneuvering speed (Va)

A

The speed at which the airplane stalls before exceeding the design load limits.

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9
Q

What is the relationship between aircraft weight and maneuvering speed?

A

As weight decreases, so does the maneuvering speed, and vice versa

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10
Q

What is the minimum altitude for steep turns?

A

1500ā€™ AGL

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11
Q

At what speed should steep turns be performed?

A

At or below Va (maneuvering speed)

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12
Q

What is a practical steep turn in terms of degrees?

A

A full 360

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13
Q

What is expected of altitude, bank angle, and airspeed during a steep turn?

A

Altitude +/- 100 feet, bank angle +/- 5 degrees, airspeed +/- 10 degrees

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14
Q

When should begin rolling out from a steep turn?

A

25-35 degrees from the reference point

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