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Free Part 107 practice test.

60 questions like the FAA Remote Pilot knowledge test, across all five test topics. Every answer is explained, with the FAA source behind it. No sign-up needed.

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Question 1 of 60Regulations

You acquired a Category 2 sUAS and plan to use it to record video footage at weddings. Can you legally fly over the bride/groom during a private photo session?

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Answer: B. Yes, as long as the aircraft is listed with an FAA-accepted Declaration of Compliance.

(As long as the aircraft has a listed Declaration of Compliance on the FAA website, you’re good to go and fly over small groups of people. Remote ID has not effect here, this requirement would only apply for flights being conducted over open air assembly. A couple does not qualify as open air assembly. While written consent is a good thing to have to cover yourself, it is not part of the regulation and not the most correct answer.)

FAA source: 14 CFR 107.115(a)(2)

Question 2 of 60Regulations

Can a sUAS weighing .35 lbs be flown over an open-air assembly of human beings if it’s equipped with prop guards.

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Answer: B. Yes, as long as the sUAS is equipped with Remote ID.

(According to Part 107 Subpart D, a Category 1 UAS weighing 0.55 lbs or less on takeoff (including the prop guards) can fly over open air assembly as long as it does not have moving rotating parts that can cause laceration, and as long as it is equipped with Remote ID.)

FAA source: 14 CFR 107.110(b)

Question 3 of 60Regulations

Other than the UAS weighing 0.55 lbs or less on takeoff, what are the other requirements to conduct Category 1 operations?

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Answer: A. It must not contain exposed rotating parts that can lacerate.

(According to Part 107 Subpart D, to conduct Category 1 operations, the RPIC must use a small UA that: weighs 0.55 lbs or less on takeoff and throughout the duration of the flight does not contain any exposed rotating parts that would lacerate human skins upon impact.)

FAA source: 14 CFR 107.110(a)(2)

Question 4 of 60Regulations

To conduct Category 2 operations, the remote Pilot in Command must use a small Unmanned aircraft that

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Answer: A. must not cause injury to a human being equivalent to 11 ft-lb of kinetic energy.

(To conduct Category 2 operations, the RPIC must use a small UA that: must not cause injury to a human being equivalent to 11 foot-pounds of kinetic energy upon impact, does not contain any exposed rotating parts that would lacerate human skins upon impact. does not contain safety defects, is labeled as Category 2, is listed with an FAA-accepted Declaration of Compliance)

FAA source: 14 CFR 107.120(a)(1)

Question 5 of 60Regulations

Can a Category 3 aircraft be flown over an open-air assembly of humans while transiting from point to point?

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Answer: B. No, it is not permitted.

(According to Part 107 Subpart D, a Category 3 UAS cannot be flown over open air assembly.)

FAA source: 14 CFR 107.125(b)

Question 6 of 60Regulations

You acquired a Category 2 sUAS and plan to use it to record video footage at weddings. Can you legally fly over the bride/groom during a private photo session?

Show the answer
Answer: C. Yes, as long as the aircraft is listed with an FAA-accepted Declaration of Compliance.

(As long as the aircraft has a listed Declaration of Compliance on the FAA website, you’re good to go and fly over small groups of people. Remote ID has not effect here, this requirement would only apply for flights being conducted over open air assembly. A couple does not qualify as open air assembly. While written consent is a good thing to have to cover yourself, it is not part of the regulation and not the most correct answer.)

FAA source: 14 CFR 107.115(a)(2)

Question 7 of 60Regulations

You purchased a new sUAS that is labeled as Category 3. After checking the FAA website, you verified it is indeed approved to fly over people. You plan to fly over a private race track. What must you do to ensure that the operation is compliant with Part 107?

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Answer: B. Ensure that the area is restricted-access and that everyone inside moving vehicles inside the area are on notice.

(In order to fly over moving vehicles, you must have a sUAS approved under Category 1 through 3, and you must ensure that you either: – Must remain within or over a closed/restricted access site and everyone in moving vehicles inside the area must be on notice, or – The UAS must not maintain sustained flight over moving vehicles.)

FAA source: 14 CFR 107.145(b)(1)

Question 8 of 60Regulations

To conduct Category 4 operations, the RPIC must use a small UA that:

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Answer: B. has an airworthiness certificate issued under Part 21.

(To conduct Category 4 operations, the RPIC must use a small UA that: has an airworthiness certificate issued under Part 21, be operated in accordance with the operating limitations, have maintenance, preventive maintenance, alterations, and inspections There are no requirements for rotating parts or labeling for Category 4.)

FAA source: 14 CFR 107.140(b)(1)

Question 9 of 60Regulations

During a photoshoot for a realtor, you have to cross a busy highway to get to the other side and get a better angle. You own a compliant Category 2 sUAS. Can you complete this mission legally?

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Answer: B. Yes, as long as you are transiting.

(In addition to having a compliant Category 2 (or 1 or 3) sUAS, in order to fly over moving vehicles that are not in a closed/restricted site with everyone on notice, you must ensure that the flight is not sustained (one-way transiting only).)

FAA source: 14 CFR 107.145(b)(2)

Question 10 of 60Regulations

You notice a cruise ship in the distance with people on the deck. You fly out to get a top-down view of the deck while the boat is getting in port. Is this legal under Part 107, assuming you are certified and current?

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Answer: C. No, the people on the deck are not on notice.

(This is tricky. A ship is considered a moving vehicle, so a Category 1 or 2 sUAS is not enough, you must either: – remain within or over a closed/restricted access site and everyone in moving vehicles inside the area must be on notice, or – The UAS must not maintain sustained flight over moving vehicles.)

FAA source: 14 CFR 107.145(b)(1)

Question 11 of 60Regulations

Who must retain maintenance records of Category 4 aircraft?

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Answer: B. The owner of the aircraft.

FAA sources: 14 CFR 107.140(c) · 14 CFR 107.140(c)(2)

Question 12 of 60Regulations

Your company purchased a Category 3-approved sUAS. Because of time constraints, you have not been able to notify everyone on the construction site that you will be flying. What should you do?

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Answer: A. ensure that the human beings who are not participating in the operation are under a covered structure or inside a non-moving vehicle.

FAA source: 14 CFR 107.125(c)(2)(ii)

Question 13 of 60Regulations

Personnel at an outdoor concert venue use an sUAS to drop promotional t-shirts and CDs over the audience. The drone is labeled as Category 3. Is this sUAS operation in compliance with 14 CFR Part 107?

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Answer: C. Not compliant with Part 107.

(According to Part 107 Subpart D, a Category 3 UAS cannot be flown over open air assembly.)

FAA source: 14 CFR 107.125(b)

Question 14 of 60Regulations

According to 14 CFR Part 107, the remote pilot in command (PIC) of a small unmanned aircraft planning to operate within Class C airspace

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Answer: C. is required to receive ATC authorization.

(Operating in controlled airspace is discussed in 14 CFR Part 107.41. The regulation states that approval must be received from ATC. This is currently accomplished either via a LAANC request or via the FAA DroneZone website.)

FAA source: 14 CFR 107.41

Question 15 of 60Regulations

Why is the Mode C Veil of interest to remote pilots?

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Answer: C. Traditional aircraft within the Mode C Veil are required to be ADS-B equipped.

FAA source: 14 CFR 91.225(d)(2)

Question 16 of 60Airspace and charts

What is the base of the outer volume of Class C airspace?

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Answer: A. 1200 feet AGL.

(Class C airspace is composed of two cylinders. The inner cylinder starts at the surface and goes to 4000 feet AGL. The outer cylinder starts at 1200 feet AGL to 4000 feet AGL. Refer to “Class C: Definitions” for more information.)

FAA source: FAA-H-8083-25C ch. 15, Class C Airspace

Question 20 of 60Airspace and charts

What is the base of the outer volume of Class C airspace?

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Answer: B. 1200 feet AGL.

(Class C airspace is composed of two cylinders. The inner cylinder starts at the surface and goes to 4000 feet AGL. The outer cylinder starts at 1200 feet AGL to 4000 feet AGL. Refer to “Class C: Definitions” for more information.)

FAA source: FAA-H-8083-25C ch. 15, Class C Airspace

Question 22 of 60Airspace and charts

When a control tower located on an airport within Class D airspace ceases operation for the day, what happens to the airspace designation?

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Answer: A. The airspace reverts to Class E or a combination of Class E and G airspace during the hours the tower is not in operation.

(The airspace is class D when the tower is in operation but reverts to Class E when not. In some situations, the airspace can be a combination of E and G.)

FAA source: AIM 3-2-5, Class D Airspace

Question 23 of 60Airspace and charts

How is class A Airspace shown on sectional charts?

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Answer: A. Class A is not charted.

FAA source: FAA Chart Users Guide (VFR Terms and Symbols), Airspace

Question 25 of 60Airspace and charts

Airspace at an airport with a part-time control tower is classified as Class D airspace only

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Answer: B. when the associated control tower is in operation.

(The airspace is class D when the tower is in operation but reverts to Class E when not. In some situations, the airspace can be a combination of E and G.)

FAA source: FAA-H-8083-25C ch. 15, Class D Airspace

Question 26 of 60Airspace and charts

If Dallas Executive Tower is not in operation, which frequency should be used as a Common Traffic Advisory Frequency (CTAF) to monitor airport traffic? (Area 3)

FAA testing supplement figure for question 26
Show the answer
Answer: B. 127.25 MHz.

(As seen in this figure, the control tower frequency is 127.25, which also means that when the tower is closed, traffic will be announced on this frequency.)

FAA sources: FAA-H-8083-25C ch. 14, Nontowered Airport · FAA-H-8083-25C ch. 14, Recommended communication procedures (Figure 14-1)

Question 27 of 60Airspace and charts

The correct method of stating 10,500 feet MSL to ATC is

Show the answer
Answer: A. ONE ZERO THOUSAND, FIVE HUNDRED.

(Tens of thousands are always spelled out so 4,500 would FOUR THOUSAND as opposed to FORTY FIVE HUNDRED.)

FAA source: AIM 4-2-8, Figures

Question 28 of 60Airspace and charts

At Coeur D’Alene which frequency should be used as a Common Traffic Advisory Frequency (CTAF) to monitor airport traffic? (Area 2)

FAA testing supplement figure for question 28
Show the answer
Answer: C. 122.8 MHz.

(As seen in this figure, the CTAF frequency (next to the circled C) is 122.8.)

FAA source: FAA-H-8083-25C ch. 14, Nontowered Airport

Question 30 of 60Airspace and charts

The CTAF/UNICOM frequency at Jamestown Airport is (Area 4)

FAA testing supplement figure for question 30
Show the answer
Answer: B. 123.0 MHz.

(As seen in this figure, the CTAF frequency (next to the circled C) is 123.0.)

FAA source: FAA-H-8083-25C ch. 14, Nontowered Airport

Question 31 of 60Operations and human factors

No person may attempt to act as a crewmember of a civil aircraft with

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Answer: A. .04 percent by weight or more alcohol in the blood.

(According to 14 CFR 107.27(a)(4) No person may act or attempt to act as a crewmember of a civil aircraft while having an alcohol concentration of 0.04 or greater in a blood or breath specimen. Alcohol concentration means grams of alcohol per deciliter of blood or grams of alcohol per 210 liters of breath.)

FAA source: 14 CFR 91.17(a)(4)

Question 32 of 60Operations and human factors

A person may not act as a crewmember of a civil aircraft if alcoholic beverages have been consumed by that person within the preceding

Show the answer
Answer: B. 8 hours.

(According to 14 CFR 107.27(a) No person may act or attempt to act as a crewmember of a civil aircraft within 8 hours after the consumption of any alcoholic beverage.)

FAA source: 14 CFR 91.17(a)(1)

Question 33 of 60Operations and human factors

Damaged lithium batteries can cause…

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Answer: B. an inflight fire.

Damaged lithium batteries will lead to thermal runaways, which would cause an inflight fire (followed by the UAS crashing on the ground).

FAA source: AC 107-2A Appendix B, B.5 Battery Fires

Question 34 of 60Operations and human factors

During your preflight inspection, you discover a small nick in the casing of your sUAS battery. What action should you take?

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Answer: C. Follow the manufacturer’s guidance.

You should always dispose of damaged batteries, however it should not be done in your household trash. In this case, follow the manufacturer’s recommendation.

FAA source: AC 107-2A Appendix B, B.5 Battery Fires

Question 35 of 60Operations and human factors

Under what condition should the operator of a small UA establish scheduled maintenance protocol?

Show the answer
Answer: C. When the manufacturer does not provide a maintenance schedule.

Establishing a maintenance protocol should be part of your operation. When available, follow the manufacturer’s recommendation. In the absence of guidance, create your own.

FAA source: AC 107-2A ch. 7, 7.2.1.1

Question 36 of 60Operations and human factors

Scheduled maintenance should be performed in accordance with the:

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Answer: B. Manufacturer’s suggested procedures.

Establishing a maintenance protocol should be part of your operation. When available, follow the manufacturer’s recommendation. In the absence of guidance, create your own.

FAA source: AC 107-2A ch. 7, 7.2.1 Scheduled Maintenance

Question 37 of 60Operations and human factors

Which of the following sources of information should you consult first when determining what maintenance should be performed on an sUAS or its components?

Show the answer
Answer: B. Manufacturer guidance.

You should always check first with the manufacturer’s guidelines when it comes to maintenance.

FAA source: AC 107-2A ch. 7, Maintenance and Inspection, 7.1

Question 38 of 60Operations and human factors

How often is the Remote PIC required to inspect the sUAS to ensure that it is in a condition for safe operation?

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Answer: C. Before each flight.

14 CFR Part 107.49 discusses the responsibilities of the rPIC when it comes to preflight familiarization, inspection, and actions for aircraft operation, including inspecting the sUAS. Inspections should be done prior to each flight.

FAA source: 14 CFR 107.15(a)

Question 39 of 60Operations and human factors

During the preflight inspection who is responsible for determining the aircraft is safe for flight?

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Answer: A. The Pilot in Command.

The remote pilot in command. Under 14 CFR 107.15(a), before each flight the remote pilot in command must check the small unmanned aircraft system to determine whether it is in a condition for safe operation; 14 CFR 107.49 adds the other preflight duties, such as assessing the operating environment, briefing everyone taking part and checking the control links.

FAA source: 14 CFR 107.15(a)

Question 40 of 60Operations and human factors

You are flying commercially and you have an accident where you crash and your battery is ejected. You find a small dent in the bottom of your battery, what do you do?

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Answer: A. Evaluate damage and make repairs.

Two of the answers are rather close and could be correct. While test flying the UAS sounds like a good idea, the fact it says “before your next commercial mission” makes it a suspicious answer. You would want to test flight your UAS prior to ANY mission if you had a crash, not just for a commercial mission. Evaluating damage is a great idea in this situation, however, making repairs to a battery pack can be difficult and could lead to more issues if you don’t have the knowledge. This is however the most appropriate answer for this question.

FAA source: AC 107-2A ch. 7, 7.2.2 Unscheduled Maintenance

Question 41 of 60Operations and human factors

What is the most effective way to use the eyes during night flight?

Show the answer
Answer: C. Scan slowly to permit off-center viewing.

FAA source: FAA-H-8083-25C ch. 17, Aeromedical Factors, Night Vision, Scanning Techniques

Question 42 of 60Operations and human factors

What is one of the requirements for flying an sUAS during twilight?

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Answer: A. The sUAS must be equipped with anti-collision lighting visible from at least 3 statute miles.

FAA source: 14 CFR 107.29(b)

Question 43 of 60Operations and human factors

Can a sUAS be flown at night?

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Answer: A. Yes, as long as the rPIC received the proper training and the aircraft is properly equipped with anti-collision lighting that meet the requirements in 107.29.

FAA sources: 14 CFR 107.29(a)(1) · 14 CFR 107.29(a)(2)

Question 44 of 60Operations and human factors

How can the remote Pilot in Command and Visual Observer(s) avoid autokinesis

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Answer: A. by using proper night scanning techniques and using peripheral vision.

FAA source: FAA-H-8083-25C ch. 17, Aeromedical Factors, Night Vision Illusions, Autokinesis

Question 45 of 60Weather

You are scheduled to conduct aerial inspections of a nearby power plant, what are some of the factors to consider.

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Answer: A. thermal plumes may create turbulence or cause reduced visibility.

(Flying in the vicinity of thermal plumes can cause reduced visibility, create turbulence or generate enough heat to damage your UAS. Refer to “Airport Operations > Other Operational Considerations” for more information”.)

FAA source: AIM 7-6-16, Avoid Flight in the Vicinity of Exhaust Plumes

Question 46 of 60Weather

Absence of the sky condition and visibility on an ATIS broadcast indicates that

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Answer: A. the ceiling is at least 5,000 feet and visibility is 5 miles or more.

(This is a rote memory item.)

FAA source: AIM 4-1-13, Automatic Terminal Information Service

Question 47 of 60Weather

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

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Answer: B. chord line of the wing and the relative wind.

(This is rote memory material. The angle of attack is always defined as the difference between the chord line and the relative wind. The chord line is the line between the leading edge and the trailing edge of the wing. The relative wind is the vector that represents where the airflow that “hits” the wing is coming from. The relative wind is always parallel to the direction of motion of the aircraft, but opposite in direction.)

FAA source: FAA-H-8083-25C ch. 5, Angle of Attack

Question 48 of 60Weather

During your preflight briefing, you realize that the visibility in your area is reported as 4 statute miles. Can you legally fly your mission?

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Answer: B. Yes, as long as you remain 500 feet below clouds and 2000 feet horizontally away from them.

(According to 107.51, the minimum visibility is 3 statute miles and you must remain 500 feet below clouds, and 2000 feet horizontally from them.)

FAA sources: 14 CFR 107.51(c) · 14 CFR 107.51(d)

Question 49 of 60Weather

You have determined that the lowest layer of clouds in your area is at 700 feet above the ground. What is the maximum altitude you will be able to fly at if you are operating below the clouds.

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Answer: A. No higher than 200 feet.

(According to 107.51, the minimum visibility is 3 statute miles and you must remain 500 feet below clouds, and 2000 feet horizontally from them.)

FAA source: 14 CFR 107.51(d)

Question 50 of 60Weather

What clouds have the greatest turbulence?

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Answer: A. Cumulonimbus.

Cumulonimbus are always the worst cloud to get near or into

FAA source: FAA-G-8082-22 ch. 3b, Thunderstorms

Question 51 of 60Weather

Convective circulation patterns associated with sea breezes are caused by

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Answer: A. cool, dense air moving inland from over the water.

Sea breeze happens during the day when warm air over land rises and reaches the colder air over water and sinks.

FAA source: FAA-H-8083-25C ch. 12, Wind patterns

Question 52 of 60Weather

What is meant by the term "Dew Point"?

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Answer: C. The temperature to which air must be cooled to become saturated.

The Dew Point is the temperature at which the air becomes fully saturated.

FAA source: FAA-H-8083-28B ch. 6, 6.5 Dewpoint

Question 53 of 60Weather

The amount of water vapor which air can hold depends on the

Show the answer
Answer: A. air temperature.

The amount of water vapor that an air mass can hold is dependent on its temperature. A warmer air mass can hold more water.

FAA source: FAA-H-8083-28B ch. 6, 6.4 Relative Humidity

Question 54 of 60Weather

An air mass moving inland from the coast in winter is likely to result in

Show the answer
Answer: B. fog.

If an air mass moves inland in the winter, it is likely a moist air mass, and warmer than the land. In which case, it will be cooled off when it moves inland, resulting in fog.

FAA source: FAA-H-8083-25C ch. 12, Fog

Question 55 of 60Loading and performance

To ensure that the unmanned aircraft center of gravity (CG) limits are not exceeded, follow the aircraft loading instructions specified in the

Show the answer
Answer: C. Pilot’s Operating Handbook or UAS Flight Manual.

( There is no such thing as an Aircraft Weight and Balance Handbook. All the information for the aircraft is contained in either the Pilot’s Operating Handbook (POH), which is a manned aircraft term, or the UAS Flight Manual if one is provided by the manufacturer. The Aeronautical Information Manual (AIM) is an FAA document that explains a variety of topics in more details.)

FAA source: FAA-G-8082-22 ch. 4, Small Unmanned Aircraft Loading

Question 56 of 60Loading and performance

When operating an unmanned airplane, the remote pilot should consider that the load factor on the wings may be increased anytime

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Answer: C. the airplane is subjected to maneuvers other than straight and level flight.

Total lift increases when the aircraft is turning or climbing/descending, aka “maneuvers other than straight and level flight”. The gross weight does have a detrimental effect on load factor as well but only when it increases (more weight = more lift = more load factor). Finally, the location of the CG does not have an effect on load factor.)

FAA source: FAA-H-8083-25C ch. 5, Load Factors and Flight Maneuvers

Question 57 of 60Loading and performance

A stall occurs when the smooth airflow over the unmanned airplane’s wing is disrupted and the lift degenerates rapidly. This is caused when the wing

Show the answer
Answer: A. exceeds its critical angle of attack.

While the traditional wisdom dictates that this happens at slow airspeed, when the nose of the aircraft is high, this can happen at any speed. If you apply abrupt pitch-up controls, the angle of attack can reach the critical number where the airflow separates and the aircraft stalls. Remember also that the angle of attack is the difference between the chord line and the relative wind (or direction of motion of the aircraft). When the aircraft reaches maximum speed, the wing will still produce lift, but structural failure can occur (the aircraft wouldn’t be strong enough to go that fast). If the aircraft exceeds its maximum allowable operating weight, structural damage or failure is also a possibility.)

FAA source: FAA-H-8083-25C ch. 5, Stalls

Question 58 of 60Loading and performance

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

Show the answer
Answer: C. does not adversely affect the center of gravity.

So when mounting cameras or other equipment, be sure it doesn’t change the CG to the point where it is out of limits. While the other two answers are rather correct, the “most correct” answer is still “does not adversely affect the center of gravity.)

FAA source: FAA-G-8082-22 ch. 4, Small Unmanned Aircraft Loading

Question 59 of 60Loading and performance

If an unmanned airplane weighs 33 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?

FAA testing supplement figure for question 59
Show the answer
Answer: B. 38 pounds.

(The information needed for this answer is found in the left column of the figure. At 30° of bank, the load factor is 1.154. If the object weighs 33 pounds, then at 30°, the load factor will be 33×1.154=38 pounds.)

FAA source: FAA-CT-8080-2H Appendix 2, Figure 2 Load Factor Chart

Question 60 of 60Loading and performance

The angle of attack at which an airplane wing stalls will

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Answer: B. remain the same regardless of gross weight.

(The angle of attack at which an airplane stalls is defined as the critical angle of attack. Since the angle of attack is defined as the difference between the chord line and the relative wind, it is not affected by weight at all.)

FAA source: FAA-H-8083-25C ch. 5, Stalls

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