Aircraft Systems: Section 1

Aircraft Systems: Section 1

University

23 Qs

quiz-placeholder

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Aircraft Systems: Section 1

Aircraft Systems: Section 1

Assessment

Quiz

Other

University

Easy

Created by

gray b

Used 15+ times

FREE Resource

23 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

On an aircraft that utilizes flight spoilers, rotating the control wheel to the right will cause

the spoiler on the right wing to extend

the spoiler on the left wing to extend

an increased amount of adverse yaw towards the left

an increased amount of adverse yaw to the right

2.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

An antiservo tab is

a secondary flight control designed to decrease the effect of pilot control pressures

a primary flight control designed to decrease the effect of pilot control pressures

a secondary flight control designed to increase the effect of pilot control pressures

a primary flight control designed to increase the effect of pilot control pressures

3.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

For straight and level flight, an aircraft with additional weight

weight has negligible effect on angle of attack

will not need as much angle of attack

will require additional angle of attack

4.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

The "G" letter in the GUMP-CC or GUMPS checklist is used to describe which component?

Gear

Generator

Gauges

Gas

5.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

Adverse yaw is caused by

parasite drag

induced drag

a lack of longitudinal stability

6.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

Stabilators are typically

used for longitudinal control

located behind a fixed vertical stabilizer

used for lateral control

located behind a fixed horizontal stabilizer

7.

MULTIPLE CHOICE QUESTION

15 mins • 1 pt

An aft cg aircraft can have

decreased longitudinal stability

cg location has negligible effect on longitudinal stability

increased longitudinal stability

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