Part 107 Loading and Weather

Part 107 Loading and Weather

11th Grade

12 Qs

quiz-placeholder

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Part 107 Loading and Weather

Part 107 Loading and Weather

Assessment

Quiz

Specialty

11th Grade

Practice Problem

Hard

Created by

Diane McPherson

Used 2+ times

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12 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

The term "angle of attack" is defined as the angle between the

chord line of the wing and the relative wind.

airplanes longitudinal axis and that of the air striking the airfoil.

airplane's centerline and the relative wind.

2.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?

Lift equals weight and thrust equals drag.

Lift, drag, and weight equal thrust.

Lift and weight equal thrust and drag.

3.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

The amount of excess load that can be imposed on the wing of an airplane depends upon the

position of the CG.

speed of the airplane.

abruptness at which the load is applied.

4.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?

Climbs.

Turns.

Stalls.

5.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

What effect does high density altitude, as compared to low density altitude, have on propeller efficiency and why?

Efficiency is increased due to less friction on the propeller blades.

Efficiency is reduced because the propeller exerts less force at high density altitudes than at low density altitudes.

Efficiency is reduced due to the increased force of the propeller in the thinner air.

6.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

What is density altitude?

The height above the standard datum plane.

The pressure altitude corrected for non-standard temperature.

The altitude read directly from the altimeter.

7.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

What effect does high density altitude have on aircraft performance?

It increases engine performance.

It reduces climb performance.

It increases takeoff performance.

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