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Part 107 Loading and Performance II

Total questions: 29

Worksheet time: 15mins

Name
Class
Date
1.

In what way will the performance of a sUAS be affected by high density air?

a)

Slight change in performance

b)

Decreased performance

c)

Increased performance

2.

In what way can high humidity affect aircraft performance?

a)

Inceases performance

b)

Does not affect performance

c)

Decreases performance

3.

Density altitude can be defined as...

a)

the height relatively above standard datum plane

b)

the pressure altitude corrected for non-standard temperature

c)

the altitude that reads directly from an altimeter

4.

In what way does a high density altitude affect an aircraft performance?

a)

Reduces climb performance

b)

Increases engine performance

c)

Increases takeoff performance

5.

The volume of excess load which can be attached to the wing of an aircraft depends upon...

a)

how abrupt such load is applied

b)

the center of gravity position

c)

the speed of the aircraft

6.

Which of these atmospheric conditions will reduce the takeoff and climb performance of an aircraft?

a)

High temperature, high density altitude, and high relative humidity

b)

Low relative humidity, low density altitude, and high temperature

c)

low temperature, low density altitude, and low relative humidity

7.

In the diagram shown, if the weight of an unmanned airccraft is 33 pounds, what is the approximate weight required of the airplane structure to support during a 30° banked turn while still maintaining altitude?

a)

47 pounds

b)

38 pounds

c)

34 pounds

8.

Which of these factors would increase the density altitude at a particular airport?

a)

Ambient temperature increases

b)

Barometric pressure increases

c)

Relative humidity decreases

9.

When an aircraft is inherently stable it will...

a)

move slowly

b)

be very difficult to stall

c)

require less effort to control

10.

When an aircraft is operated outside of its weight and balance limit...

a)

performance will automatically decline

b)

loss of control of the aircraft is likely

c)

performance will increase

11.

When the outside air temperature (OAT) at a particular altitude is warmer than the standard, then the density altitude can be said to be...

a)

equal to the pressure altitude

b)

higher than the pressure altitude

c)

lower than the pressure altitude

12.

In what condition will density altitude and pressure altitude be the same value?

a)

When there is no installation error in the altimiter

b)

At standard temperature

c)

At sea level with 0°F

13.

An unmanned aircraft has been loaded so the center of gravity is located aft of the aft center of gravity limit. What flight characteristics will a remote pilot experience?

a)

Difficulty in recovering from stalled conditions

b)

A longer takeoff run

c)

Stalling at a higher-than-normal speed

14.

Regarding the diagram shown, if the weight of an unmanned aircraft is 20 pounds, how much weight must the airplane structure support during a 60° banked turn while still maintaining altitude?

a)

40 pounds

b)

28 pounds

c)

23 pounds

15.

A change in a wing's center of pressure will affect the aircraft's...

a)

lifting capacity

b)

aerodynamic controllability and balance

c)

lift/drag ratio

16.

In calculating weight and balance, arm is he...

a)

weight at the moment

b)

distance between items

c)

distance from the datum line to the item

17.

How does high density altitude affect the efficiency of a UAS propeller?

a)

Increased propeller efficiency

b)

No effect on the efficiency of the propeller

c)

Decreased propeller efficiency

18.

When comparing higher density altitude to a lower density altitude, how does the difference affect propellers and why?

a)

Efficiency is reduced because the propellers exert less force at high density altude than they do at low density altitudes

b)

Efficiency is increased due to less friction on the blades of the propellers

c)

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

19.

Overloading an aircraft causes problems such as...

a)

reduced climb rate, shortened cruising range, and excessive structural loads

b)

increased service ceiling, increased crusing speed, and increased angle of climb

c)

increased maneuverability, shorter takeoff roll, and slower takeoff speed

20.

A setting at minimum power, maximum endurance can be obtained to maintain an aircraft...

a)

in a steady flight level

b)

in long range descent

c)

in steady range descent

21.

How can the center of gravity be calculated?

a)

Multiplying arm times weight

b)

Dividing the total weight by the total moment

c)

Dividing the total moment by the total weight

22.

The term that describes an aircraft's ability to easily maneuver and cope with the stresses that come with maneuvers is called..

a)

controllability

b)

maneuverability

c)

aircraft flexibility

23.

The term for an aircraft's capability to respond to the pilot's control in a flight operation is...

a)

controllability

b)

aircraft flexibility

c)

maneuverability

24.

The two significant areas of stability in an aircraft performance are...

a)

aircraft flexibility and maneuverability

b)

controllability and maneuverability

c)

aircraft ability and controllability

25.

On a fixed-wing aircraft, which of these could increase the load factor?

a)

Power off stall

b)

Steady state climb

c)

Level turn

26.

During an accident, the battery of your UAS gets dislodged. What do you do when you notice a dent in the battery?

a)

Perform a test operation to ensure everything is functionng properly

b)

Cautiously access the battery's condition and follow the manufacturer's recommendations

c)

Regardless of condition, discard the battery

27.

Which of these results is most likely when the center of gravity on an aircraft is far aft?

a)

Aircraft will experience inreased high-speed

b)

Aircraft will not be able to maintain a constant turn

c)

Aircraft will experience difficulty when recovering from a stalled position

28.

What does AOA stand for?

a)

Automated Operational Angle

b)

Aeronautical Operational Angle

c)

Angle of Attack

29.

What is used to determine load factor in a given radius banked turn?

a)

Sectional Chart

b)

Angle of Attack

c)

Load Factor Chart