Chapter 4 - Loading and Performance Flashcards

1
Q

What must a person who is manipulating the controls of a small unmanned aircraft do if the standard remote identification fails during flight?

A

Land the aircraft as soon as practicable.

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2
Q

Who is responsible for ensuring that there are enough crewmembers for a given sUAS operation?

A

Remote pilot-in-command.

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3
Q

No person may attempt to act as a crewmember of a sUAS with

A

.04 percent by weight or more alcohol in the blood.

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4
Q

(Refer to Figure 75, Area 6.) During preflight planning, you plan to operate in R-2305. Where would you find additional information regarding this airspace?

A

In the Special Use Airspace area of the chart.

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5
Q

What is required to enter an airport SIDA?

A

You must have an airport-issued or approved ID.

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6
Q

Which of the following considerations is most relevant to a remote PIC when evaluating unmanned aircraft performance?

A

Current weather conditions

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7
Q

Which of the following is true regarding weight and balance of small unmanned aircraft?

A

Operations outside weight and balance limitations may result in loss of control.

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8
Q

You are operating an sUAS that does not have GPS or an installed ground speed limiter. How can you determine the speed you are operating?

A

Dead reckoning.

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9
Q

What purpose does a rudder perform on an sUAS airplane?

A

The rudder controls yaw.

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10
Q

When range and economy of operation are the principle goals, the remote pilot must ensure that the sUAS will be operated at the recommended

A

long-range cruise performance.

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11
Q

Maximum endurance is obtained at the point of minimum power to maintain the aircraft

A

in steady, level flight.

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12
Q

The term “angle of attack” is defined as the angle

A

between the wing chord line and the relative wind

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13
Q

What effect does an uphill terrain slope have on launch performance?

A

Increases launch distance.

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14
Q

In a 45 degree banking turn, a small unmanned aircraft will

A

stall at a higher airspeed

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15
Q

A small unmanned aircraft loaded with the most rearward center of gravity is

A

less stable at all speeds.

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16
Q

(Refer to Figure 2.) If an unmanned airplane weighs 33 pounds, what approximate weight would the airplane structure be required to support during a 30 degree banked turn while maintaining altitude?

A

38 pounds.

17
Q

Scheduled maintenance should be performed in accordance with the

A

Manufacturers’ suggested procedures.

18
Q

During your preflight inspection, you discover that the casing of your sUAS battery has expanded beyond its normal dimensions. What action should you take?

A

Follow the manufacturer’s guidance.

19
Q

You are operating an sUAS that does not have GPS or an installed altimeter. How can you
determine the altitude you are operating?

A

Gaining a visual perspective of what 400 feet looks like on the ground before the flight.

20
Q

The most critical conditions of launch performance are the result of some combination of
high gross weight, altitude, temperature, and

A

unfavorable wind.

21
Q

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

A

speed of the airplane.

22
Q

What effect does an uphill terrain slope have on launch performance?

A

Increases launch distance.

23
Q

An increase in load factor will cause an unmanned aircraft to

A

stall at a higher airspeed.

24
Q

When loading cameras or other equipment on an sUAS, mount the items in a manner that

A

does not adversely affect the center of gravity.