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60 FAA-published questions · answers explained · free, no signup

Private Pilot Written Test Questions and Answers

The FAA Private Pilot Airplane knowledge test (PAR) has 60 scored questions with three answer choices each, a 2-hour limit and a 70% passing score. Below are 60 questions the FAA itself published, each with the correct answer, a plain-English explanation and the 14 CFR, AIM or handbook source.

The PAR test at a glance

FAA Private Pilot Knowledge Test (PAR)
Test codePAR[1]
Scored questions60 (plus 5 unscored validation questions)[2]
Time allowed2 hours (120 minutes)[1]
Passing score70%[1]
Answer choices3 per question (A, B, C)[3]
Test fee$175 plus tax per attempt (PSI voucher price)[4]
Minimum age to test15[1]
To take the testAn instructor endorsement or a pilot-school graduation certificate (14 CFR 61.35, 61.71).[1]
If you failAn instructor endorsement certifying additional training (14 CFR 61.49). No waiting period.[5]
Result valid for24 calendar months for the practical test (14 CFR 61.39)[6]
Figures bookletFAA-CT-8080-2H[7]
StandardFAA-S-ACS-6C[8]
2025 pass rate89.56% of 44,657 attempts (average score 81.64%)[9]
  1. [1] FAA Airman Knowledge Testing Matrix (revised Sep 25, 2026)
  2. [2] PSI PAR applicant information bulletin
  3. [3] FAA airman knowledge test sample questions (Aug 2021)
  4. [4] PSI: FAA testing programs ($175 per knowledge test voucher)
  5. [5] 14 CFR 61.49: Retesting after failure
  6. [6] 14 CFR 61.39: Prerequisites for practical tests (24 calendar months)
  7. [7] FAA airman knowledge testing supplements
  8. [8] FAA Airman Certification Standards
  9. [9] FAA CY2025 Airman Knowledge Test Volume Report
Where the points are
  • I. Preflight Preparation22%
  • II. Preflight Procedures13%
  • III. Airport and Seaplane Base Operations7%
  • IV. Takeoffs, Landings, and Go-Arounds20%
  • V. Performance and Ground Reference Maneuvers3%
  • VI. Navigation8%
  • VII. Slow Flight and Stalls8%
  • VIII. Basic Instrument Maneuvers7%
  • IX. Emergency Operations7%
  • XI. Night Operations3%
  • XII. Postflight Procedures2%

Share of the 60 scored questions per ACS area of operation (FAA-S-ACS-6C). Area X (multiengine) is not on the PAR. Source: PSI PAR applicant information bulletin.

What the PAR test checks, and where these questions come from

The PAR test takes its topics from the Private Pilot Airman Certification Standards (FAA-S-ACS-6C). The PSI bulletin weights them unevenly: Preflight Preparation, which is where regulations, airspace, weather, performance and systems live, carries 22% of the questions, and Takeoffs, Landings and Go-Arounds another 20%. Questions built on a sectional chart, a METAR, a weight-and-balance table or an airport diagram point to a figure in supplement FAA-CT-8080-2H, the booklet you are handed at the testing center.

The 60 questions on this page are a weighted pick from the 395 the FAA has published for the private certificate: its August 2021 sample test first, then the FAA's 2008 Private Pilot bank, kept only where the answer still holds under today's rules. Regulations and weather lead because they lead the FAA's own bank. The live test uses different, confidential questions on the same knowledge, so learn the reason in each explanation, not the letter.

US airspace classes, in 3D

Heights not to scale. Typical dimensions: the sectional chart shows each airspace's actual floor and ceiling. Sources: 14 CFR 71 and 91, AIM chapter 3.
US airspace classes at a glance
ClassVertical limitsTo fly VFR in it
Class A18,000 ft MSL up to and including FL600IFR only: instrument rating and IFR clearance (14 CFR 91.135)
Class BSurface to 10,000 ft MSL (typical), upside-down wedding cakeATC clearance to enter; private pilot certificate or student endorsement (91.131)
Class CSurface to 4,000 ft AGL in a 5 NM core; 10 NM shelf from 1,200 ft AGL (typical)Two-way radio communication established before entering (91.130)
Class DSurface to 2,500 ft AGL (typical); charted ceiling in feet MSLTwo-way radio communication established before entering (91.129)
Class EFrom the surface, 700 ft AGL or 1,200 ft AGL up to but not including 18,000 ft MSL; and above FL600No ATC contact required for VFR; VFR weather minimums apply (91.155)
Class GFrom the surface up to the floor of the overlying Class ENo ATC contact required; VFR weather minimums apply (91.155)

How to read the sectional chart symbols the test asks about

401240SFC3531501549(304)38RIVERDALE (XRD)CT – 118.3ATIS 124.51340 L 72 122.95C12345Schematic, not for navigation
Schematic sectional excerpt, not for navigation. Symbols per the FAA Aeronautical Chart User's Guide.
  1. Class D ceiling box

    The dashed blue ring is Class D. [38] is its ceiling in hundreds of feet MSL: 3,800 ft MSL, about 2,500 ft above this 1,340 ft field. A minus sign ([-38]) means up to but not including that altitude.

  2. Class C ceilings and floors

    Solid magenta rings are Class C, labeled ceiling over floor in hundreds of feet MSL. 40/SFC: the inner core runs from the surface to 4,000 ft MSL. 40/12: the outer shelf runs from 1,200 to 4,000 ft MSL.

  3. Airport data block

    Blue type means a control tower. CT – 118.3 is the tower frequency, the star marks a part-time tower and the circled C marks 118.3 as the CTAF when the tower is closed. 1340 is the field elevation in feet MSL, L runway lights sunset to sunrise, 72 the longest runway (7,200 ft) and 122.95 the UNICOM.

  4. Maximum Elevation Figure (MEF)

    3⁵ means 3,500 ft MSL: the highest terrain or obstacle in this latitude-longitude quadrangle (here the 3,150 ft peak) plus a safety allowance, rounded up to the next 100 ft.

  5. Obstruction height

    1549 (304): the top of the obstruction is 1,549 ft MSL and 304 ft above the ground. This symbol is used for obstructions under 1,000 ft AGL.

60 Private Pilot questions with answers

Try each one, then open the answer. Grouped by topic; jump to one:

Regulations questions

14 of the 89 the FAA published on this topic for this test.

1

Maintenance records show the last transponder inspection was performed on September 1, 2014. The next inspection will be due no later than

  1. ASeptember 30, 2015.
  2. BSeptember 1, 2016.
  3. CSeptember 30, 2016.
Show answer and explanation

Correct answer: C. September 30, 2016.

Under 14 CFR 91.413(a) a transponder must have been tested and inspected within the preceding 24 calendar months. Calendar months run to the end of the month, so an inspection on September 1, 2014 remains valid through the last day of September 2016: September 30, 2016. September 30, 2015 would be only 12 months, and September 1, 2016 ignores the calendar-month rule.

Source: 14 CFR 91.413(a)ACS PA.I.B.K1b

2

With respect to the certification of airmen, which are categories of aircraft?

  1. AGyroplane, helicopter, airship, free balloon.
  2. BAirplane, rotorcraft, glider, lighter-than-air.
  3. CSingle-engine land and sea, multiengine land and sea.
Show answer and explanation

Correct answer: B. Airplane, rotorcraft, glider, lighter-than-air.

For airman certification, 14 CFR 61.5(b)(1) lists the aircraft category ratings: airplane, rotorcraft, glider, lighter-than-air, powered-lift, powered parachute and weight-shift-control aircraft. Gyroplane, helicopter, airship and free balloon are classes within the rotorcraft and lighter-than-air categories, and single-engine/multiengine land and sea are airplane class ratings (61.5(b)(2)).

Source: 14 CFR 61.5(b)(1)ACS PA.I.A.K1

3

Pre-takeoff briefing of passengers about the use of seat belts for a flight is the responsibility of

  1. Aall passengers.
  2. Bthe pilot in command.
  3. Cthe right seat pilot.
Show answer and explanation

Correct answer: B. the pilot in command.

14 CFR 91.107(a) prohibits taking off unless the pilot in command ensures that each person on board has been briefed on how to fasten and unfasten the safety belt and shoulder harness, and has been told to fasten it for surface movement, takeoff and landing. The duty belongs to the PIC, not to the passengers themselves or to whoever occupies the right seat.

Source: 14 CFR 91.107(a)ACS PA.II.B.K1

4

A 100-hour inspection was due at 3302.5 hours. The 100-hour inspection was actually done at 3309.5 hours. When is the next 100-hour inspection due?

  1. A3312.5 hours.
  2. B3395.5 hours.
  3. C3402.5 hours.
Show answer and explanation

Correct answer: C. 3402.5 hours.

14 CFR 91.409(b) allows the 100-hour limit to be exceeded by up to 10 hours only to reach a place where the inspection can be done, and the excess time must be included in computing the next 100 hours. The next inspection is therefore still based on the original due time: 3302.5 + 100 = 3402.5 hours, not 3309.5 + 100 = 3409.5. 3312.5 is just the 10-hour ferry allowance, and 3395.5 subtracts the overrun twice.

Source: 14 CFR 91.409(b)ACS PA.I.B.K1b

5

Your cousin wants you to take him flying. You must have made at least three takeoffs and three landings in your aircraft within the preceding

  1. A90 days.
  2. B60 days.
  3. C30 days.
Show answer and explanation

Correct answer: A. 90 days.

Under 14 CFR 61.57(a), to act as pilot in command of an aircraft carrying passengers you must have made at least three takeoffs and three landings within the preceding 90 days, as sole manipulator of the controls, in an aircraft of the same category, class and type (if a type rating is required). 30 and 60 days are not periods used in this regulation.

Source: 14 CFR 61.57(a)ACS PA.I.A.K1

6

When must the battery in an emergency locator transmitter (ELT) be replaced (or recharged if the battery is rechargeable)?

  1. AAfter one-half the battery's useful life.
  2. BDuring each annual and 100-hour inspection.
  3. CEvery 24 calendar months.
Show answer and explanation

Correct answer: A. After one-half the battery's useful life.

14 CFR 91.207(c) requires ELT batteries to be replaced (or recharged, if rechargeable) when the transmitter has been in use for more than 1 cumulative hour or when 50 percent of the battery's useful life has expired. There is no fixed 24-month or every-inspection replacement rule; 91.207(d) requires an annual ELT inspection, not a new battery.

Source: 14 CFR 91.207(c)

7

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

  1. AThe pilot in command.
  2. BThe certificated mechanic who performed the annual inspection.
  3. CThe owner or operator.
Show answer and explanation

Correct answer: A. The pilot in command.

14 CFR 91.7(b) makes the pilot in command responsible for determining whether the aircraft is in condition for safe flight, and 91.3 gives the PIC final authority for its operation. The owner or operator is responsible for maintaining airworthiness (91.403), and the mechanic signs for the work he or she performed, but neither decides whether this flight is safe.

Source: 14 CFR 91.7(b)

8

With respect to the certification of aircraft, which is a category of aircraft?

  1. ANormal, utility, acrobatic.
  2. BAirplane, rotorcraft, glider.
  3. CLandplane, seaplane.
Show answer and explanation

Correct answer: A. Normal, utility, acrobatic.

14 CFR 1.1 says that for the certification of aircraft, category means a grouping by intended use or operating limitations, such as transport, normal, utility, acrobatic, limited, restricted and provisional. Airplane, rotorcraft and glider are categories for airman certification, and landplane/seaplane describe a class.

Source: 14 CFR 1.1

9

With respect to the certification of airmen, which is a class of aircraft?

  1. AAirplane, rotorcraft, glider, lighter-than-air.
  2. BSingle-engine land and sea, multiengine land and sea.
  3. CLighter-than-air, airship, hot air balloon, gas balloon.
Show answer and explanation

Correct answer: B. Single-engine land and sea, multiengine land and sea.

For airman certification, 14 CFR 1.1 defines class as a grouping of aircraft with similar operating characteristics, such as single-engine, multiengine, land, water, gyroplane, helicopter, airship and free balloon; 61.5 lists single-engine land and sea and multiengine land and sea for airplanes. Airplane, rotorcraft, glider and lighter-than-air are categories.

Source: 14 CFR 1.1

10

Preventive maintenance has been performed on an aircraft. What paperwork is required?

  1. AA full, detailed description of the work done must be entered in the airframe logbook.
  2. BThe date the work was completed, and the name of the person who did the work must be entered in the airframe and engine logbook.
  3. CThe signature, certificate number, and kind of certificate held by the person approving the work and a description of the work must be entered in the aircraft maintenance records.
Show answer and explanation

Correct answer: C. The signature, certificate number, and kind of certificate held by the person approving the work and a description of the work must be entered in the aircraft maintenance records.

14 CFR 43.9(a) requires a maintenance record entry for preventive maintenance containing a description of the work, the date of completion, the name of the person who performed it and, if the work is approved for return to service, the signature, certificate number and kind of certificate of the person approving it. The other options leave out the required approval information.

Source: 14 CFR 43.9(a)

11

How soon after the conviction for driving while intoxicated by alcohol or drugs shall it be reported to the FAA, Civil Aviation Security Division?

  1. ANo later than 60 days after the motor vehicle action.
  2. BNo later than 30 working days after the motor vehicle action.
  3. CRequired to be reported upon renewal of medical certificate.
Show answer and explanation

Correct answer: A. No later than 60 days after the motor vehicle action.

14 CFR 61.15(e) requires a written report of each motor vehicle action (such as a DWI conviction or license suspension) to the FAA's Civil Aviation Security Division no later than 60 days after the motor vehicle action. It is a separate report from the medical application, and the deadline is 60 calendar days, not 30 working days.

Source: 14 CFR 61.15(e)

12

Each person who holds a pilot certificate or a medical certificate shall present it for inspection upon the request of the Administrator, the National Transportation Safety Board, or any

  1. Aauthorized representative of the Department of Transportation.
  2. Bperson in a position of authority.
  3. Cfederal, state, or local law enforcement officer.
Show answer and explanation

Correct answer: C. federal, state, or local law enforcement officer.

14 CFR 61.3(l) requires a person holding a pilot or medical certificate to present it for inspection on request of the Administrator, an authorized representative of the NTSB or TSA, or any Federal, State or local law enforcement officer. A generic 'person in a position of authority' is not in the rule.

Source: 14 CFR 61.3(l)

13

What document(s) must be in your personal possession or readily accessible in the aircraft while operating as pilot in command of an aircraft?

  1. ACertificates showing accomplishment of a checkout in the aircraft and a current biennial flight review.
  2. BA pilot certificate with an endorsement showing accomplishment of an annual flight review and a pilot logbook showing recency of experience.
  3. CAn appropriate pilot certificate and an appropriate current medical certificate if required.
Show answer and explanation

Correct answer: C. An appropriate pilot certificate and an appropriate current medical certificate if required.

Under 14 CFR 61.3(a) and (c), a pilot acting as PIC must have in physical possession or readily accessible in the aircraft an appropriate pilot certificate and, when required, a current medical certificate (along with photo identification). Logbooks showing checkouts, flight reviews or recency need not be carried.

Source: 14 CFR 61.3(a)

14

What exception, if any, permits a private pilot to act as pilot in command of an aircraft carrying passengers who pay for the flight?

  1. AIf the passengers pay all the operating expenses.
  2. BIf a donation is made to a charitable organization for the flight.
  3. CThere is no exception.
Show answer and explanation

Correct answer: B. If a donation is made to a charitable organization for the flight.

14 CFR 61.113(d) lets a private pilot act as PIC of a charitable, nonprofit or community event flight in which passengers make a donation to the sponsoring organization, provided the conditions of 91.146 are met. Passengers paying all the operating expenses is not allowed; a private pilot may share expenses only on a pro rata basis (61.113(c)).

Source: 14 CFR 61.113(d)

Weather theory questions

10 of the 61 the FAA published on this topic for this test.

15

Why is frost considered hazardous to flight?

  1. AFrost changes the basic aerodynamic shape of the airfoils, thereby increasing lift.
  2. BFrost slows the airflow over the airfoils, thereby increasing control effectiveness.
  3. CFrost spoils the smooth flow of air over the wings, thereby decreasing lifting capability.
Show answer and explanation

Correct answer: C. Frost spoils the smooth flow of air over the wings, thereby decreasing lifting capability.

Frost roughens the wing surface and disrupts the smooth airflow over it, causing early airflow separation; as PHAK Ch. 12 explains, this reduces the wing's lifting capability and increases drag and stall speed, possibly preventing the airplane from becoming airborne. Frost never increases lift, and it does not improve control effectiveness.

Source: PHAK (FAA-H-8083-25)ACS PA.I.C.K3k

16

The mature stage of a thunderstorm begins with

  1. Aformation of the anvil top.
  2. Bthe start of precipitation.
  3. Ccontinuous downdrafts.
Show answer and explanation

Correct answer: B. the start of precipitation.

A thunderstorm cell goes through cumulus, mature and dissipating stages. According to PHAK Ch. 12, precipitation beginning to fall from the cloud base signals that a downdraft has developed and the cell has entered the mature stage. The anvil top forms later as the storm reaches maturity, and continuous downdrafts throughout the cell characterize the dissipating stage.

Source: PHAK (FAA-H-8083-25)ACS PA.I.C.K3h

17

The wind at 5,000 feet AGL is southwesterly while the surface wind is southerly. This difference in direction is primarily due to

  1. Astronger pressure gradient at higher altitudes.
  2. Bfriction between the wind and the surface.
  3. Cstronger Coriolis force at the surface.
Show answer and explanation

Correct answer: B. friction between the wind and the surface.

Above the friction layer, wind blows nearly parallel to the isobars as pressure gradient and Coriolis force balance. Within roughly the lowest 2,000 feet, friction with the surface slows the wind, which weakens the Coriolis force. The wind then turns toward lower pressure, which is why a southwesterly wind aloft becomes more southerly at the surface (PHAK Ch. 12). Coriolis force is weaker, not stronger, at the surface, and the pressure gradient is not what causes the directional change.

Source: PHAK (FAA-H-8083-25)ACS PA.I.C.K3b

18

When there is a temperature inversion, you would expect to experience

  1. Aclouds with extensive vertical development above an inversion aloft.
  2. Bgood visibility in the lower levels of the atmosphere and poor visibility above an inversion aloft.
  3. Can increase in temperature as altitude increases.
Show answer and explanation

Correct answer: C. an increase in temperature as altitude increases.

A temperature inversion is by definition a layer in which temperature increases as altitude increases (PHAK Ch. 12). The warm layer on top acts as a lid on stable air, trapping haze, smoke and fog, so visibility is typically poor below the inversion and better above it, the reverse of the other visibility statement. Inversions go with stable air, not with clouds of extensive vertical development.

Source: PHAK (FAA-H-8083-25)ACS PA.I.C.K3c

19

When warm, moist, stable air flows upslope, it

  1. Aproduces stratus type clouds.
  2. Bcauses showers and thunderstorms.
  3. Cdevelops convective turbulence.
Show answer and explanation

Correct answer: A. produces stratus type clouds.

When moist, stable air is forced up sloping terrain, it cools until it condenses. Because stable air resists vertical motion, the result is a layered, stratus-type cloud or upslope fog (PHAK Ch. 12). Showers, thunderstorms and convective turbulence come from lifting unstable air, not stable air.

Source: PHAK (FAA-H-8083-25)ACS PA.I.C.K3f

20

How will frost on the wings of an airplane affect takeoff performance?

  1. AFrost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability.
  2. BFrost will change the camber of the wing, increasing its lifting capability.
  3. CFrost will cause the airplane to become airborne with a higher angle of attack, decreasing the stall speed.
Show answer and explanation

Correct answer: A. Frost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability.

Even a thin layer of frost roughens the wing surface and disrupts the smooth airflow, which causes early airflow separation, less lift and more drag; PHAK and AC 91-74B warn it can prevent the airplane from becoming airborne at normal takeoff speed. Frost does not usefully change camber, and it raises rather than lowers the stall speed.

Source: PHAK (FAA-H-8083-25) · AC 91-74B

21

The suffix 'nimbus,' used in naming clouds, means

  1. Aa cloud with extensive vertical development.
  2. Ba rain cloud.
  3. Ca middle cloud containing ice pellets.
Show answer and explanation

Correct answer: B. a rain cloud.

PHAK Chapter 12 explains that the prefix nimbo- or suffix -nimbus in a cloud name means a rain cloud, as in nimbostratus and cumulonimbus. Extensive vertical development is indicated by cumulus, and 'alto' marks middle clouds.

Source: PHAK Chapter 12

22

Clouds are divided into four families according to their

  1. Aoutward shape.
  2. Bheight range.
  3. Ccomposition.
Show answer and explanation

Correct answer: B. height range.

Clouds are grouped into four families by the height range in which they form: low, middle and high clouds, plus clouds with extensive vertical development (PHAK Chapter 12). Shape (cumulus, stratus) and composition (water or ice) describe clouds within those families but are not the basis of the four-family division.

Source: PHAK Chapter 12

23

What cloud types would indicate convective turbulence?

  1. ACirrus clouds.
  2. BNimbostratus clouds.
  3. CTowering cumulus clouds.
Show answer and explanation

Correct answer: C. Towering cumulus clouds.

Towering cumulus clouds are built by strong rising air currents, so they indicate convective turbulence (PHAK Chapter 12). Cirrus are high ice-crystal clouds, and nimbostratus are stratiform rain clouds associated with stable air and little turbulence.

Source: PHAK Chapter 12

24

What clouds have the greatest turbulence?

  1. ATowering cumulus.
  2. BCumulonimbus.
  3. CNimbostratus.
Show answer and explanation

Correct answer: B. Cumulonimbus.

Cumulonimbus clouds (thunderstorms) contain the strongest updrafts and downdrafts and are the most turbulent clouds, as PHAK Chapter 12 and AIM 7-1-26 describe. Towering cumulus are turbulent but less so, and nimbostratus are stable, stratiform rain clouds.

Source: PHAK Chapter 12 · AIM 7-1-26

Quiz yourself: 10 more PAR questions

Questions that are not on this page, one at a time, with the explanation after each answer.

Question 1 of 10 · ChartsScore 0

A blue segmented circle on a Sectional Chart depicts which class airspace?

Airspace questions

5 of the 38 the FAA published on this topic for this test.

25

(Refer to FAA-CT-8080-2H, Figure 26, area 2.) The day VFR visibility and cloud clearance requirements to operate over the town of Cooperstown, after departing and climbing out of the Cooperstown Airport at or below 700 feet AGL are

FAA Figure 26Sectional chart excerpt (Cooperstown, ND)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. A1 mile and clear of clouds.
  2. B1 mile and 1,000 feet above, 500 feet below, and 2,000 feet horizontally from clouds.
  3. C3 miles and clear of clouds.
Show answer and explanation

Correct answer: A. 1 mile and clear of clouds.

On Figure 26, Cooperstown Airport (S32) sits inside a magenta shaded vignette, meaning Class E airspace begins at 700 feet AGL, so the airspace at or below 700 feet AGL is Class G. For Class G at 1,200 feet AGL or less during the day, 14 CFR 91.155(a) requires 1 statute mile flight visibility and clear of clouds. The 3-mile and 1,000/500/2,000 cloud-clearance values are Class E (or Class G above 1,200 feet AGL) requirements.

Source: 14 CFR 91.155(a)ACS PA.I.E.K1

26

(Refer to FAA-CT-8080-2H, Figure 20, area 1.) The NALF Fentress (NFE) Airport is in what type of airspace?

FAA Figure 20Sectional chart excerpt (Norfolk, VA)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. AClass C.
  2. BClass E.
  3. CClass G.
Show answer and explanation

Correct answer: B. Class E.

On Figure 20, Fentress NALF (NFE), south of Norfolk near Great Bridge, is enclosed by a magenta dashed line, which the Aeronautical Chart User's Guide defines as a Class E surface area. The solid magenta rings of the Norfolk Class C airspace pass north of the field, so NFE is not in Class C. Because controlled airspace extends to the surface there, it is not Class G either.

Source: Chart User's GuideACS PA.I.E.K2

27

(Refer to FAA-CT-8080-2H, Figure 78.) What are the basic VFR weather minima required to takeoff from the Onawa, IA (K36) airport during the day?

FAA Figure 78Sectional chart excerpt (Onawa, IA)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. A3 statute miles visibility, 500 feet below the clouds, 1,000 feet above the clouds, and 2,000 feet horizontally from the clouds.
  2. B0 statute miles, clear of clouds.
  3. C1 statute mile, clear of clouds.
Show answer and explanation

Correct answer: C. 1 statute mile, clear of clouds.

On Figure 78, Onawa (K36, elevation 1,047 ft, CTAF 123.0) has no dashed magenta Class E surface area or Class D boundary around it, so the airspace at the surface where the takeoff occurs is Class G. For day operations in Class G at 1,200 feet or less above the surface, 14 CFR 91.155(a) requires 1 statute mile visibility and clear of clouds. The 3-mile, 500/1,000/2,000 values apply in controlled airspace such as a Class E surface area. The regulations have no '0 miles' VFR minimum for airplanes.

Source: 14 CFR 91.155(a)ACS PA.I.E.K1

28

During operations outside controlled airspace at altitudes of more than 1,200 feet AGL, but less than 10,000 feet MSL, the minimum flight visibility for day VFR flight is

  1. A1 mile.
  2. B3 miles.
  3. C5 miles.
Show answer and explanation

Correct answer: A. 1 mile.

Outside controlled airspace is Class G. The 14 CFR 91.155(a) table gives, for Class G more than 1,200 feet above the surface but below 10,000 feet MSL, a day flight visibility of 1 statute mile (with 500 below, 1,000 above and 2,000 feet horizontal from clouds). 3 miles is the night value there (and the Class C, D and E value below 10,000 MSL), and 5 miles applies at or above 10,000 feet MSL.

Source: 14 CFR 91.155(a)ACS PA.I.E.K1

29

During operations outside controlled airspace at altitudes of more than 1,200 feet AGL, but less than 10,000 feet MSL, the minimum distance below clouds requirement for VFR flight at night is

  1. A500 feet.
  2. B1,000 feet.
  3. C1,500 feet.
Show answer and explanation

Correct answer: A. 500 feet.

In Class G airspace more than 1,200 feet above the surface but below 10,000 feet MSL, 14 CFR 91.155(a) requires at night 3 statute miles visibility and cloud clearance of 500 feet below, 1,000 feet above and 2,000 feet horizontal. 1,000 feet is the required distance above clouds, and 1,500 feet is not a value in the table.

Source: 14 CFR 91.155(a)ACS PA.I.E.K1

Weather reports and forecasts questions

5 of the 33 the FAA published on this topic for this test.

30

When speaking to a flight service weather briefer, you should state

  1. Athe pilot in command's full name and address.
  2. Ba summary of your qualifications.
  3. Cwhether the flight is VFR or IFR.
Show answer and explanation

Correct answer: C. whether the flight is VFR or IFR.

AIM 5-1-1 says that when requesting a preflight briefing you identify yourself as a pilot and provide the type of flight planned (VFR or IFR), the aircraft number or pilot's name, aircraft type, departure airport, route, destination, altitude, ETD and ETE, so the briefer can tailor the briefing. A home address and a summary of your qualifications are not part of that background information.

Source: AIM 5-1-1ACS PA.I.C.K1

31

You plan to phone a weather briefing facility for preflight weather information. You should

  1. Aprovide the number of occupants on board.
  2. Bidentify yourself as a pilot.
  3. Cbegin with your route of flight.
Show answer and explanation

Correct answer: B. identify yourself as a pilot.

AIM 5-1-1 says that when you request a preflight briefing you should identify yourself as a pilot and then give background information: VFR or IFR, aircraft number or pilot's name, aircraft type, departure airport, route, destination, altitude(s), ETD and ETE. The number of occupants is not part of the briefing request. The route of flight is provided, but not as the opening item before you identify yourself as a pilot.

Source: AIM 5-1-1ACS PA.I.C.K1

32

(Refer to FAA-CT-8080-2H, Figure 17.) What wind is forecast for STL at 12,000 feet?

FAA Figure 17Winds and temperatures aloft forecast (FB)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. A230° true at 56 knots.
  2. B230° true at 39 knots.
  3. C230° magnetic at 56 knots.
Show answer and explanation

Correct answer: B. 230° true at 39 knots.

In Figure 17 the STL entry under 12,000 feet is 2339-04: 23 = 230 degrees, 39 = 39 knots, and -04 = minus 4 degrees Celsius. Winds and temperatures aloft forecasts give direction relative to true north, so the forecast is 230 degrees true at 39 knots. 56 knots is the 18,000-foot value (2356-16), and the direction is not magnetic.

ACS PA.I.C.K2

33

What information is contained in a CONVECTIVE SIGMET?

  1. ATornadoes, embedded thunderstorms, and hail 3/4 inch or greater in diameter.
  2. BSevere icing, severe turbulence, or widespread dust storms lowering visibility to less than 3 miles.
  3. CSurface winds greater than 40 knots or thunderstorms equal to or greater than video integrator processor (VIP) level 4.
Show answer and explanation

Correct answer: A. Tornadoes, embedded thunderstorms, and hail 3/4 inch or greater in diameter.

AIM 7-1-6 lists the criteria for a Convective SIGMET: severe thunderstorms (surface winds of 50 knots or more, hail of 3/4 inch or more, or tornadoes), embedded thunderstorms, lines of thunderstorms, and areas of strong thunderstorms covering a large area. Severe icing, severe turbulence and dust storms are non-convective SIGMET items, and the wind threshold is 50, not 40, knots.

Source: AIM 7-1-6

34

Which in-flight advisory would contain information on severe icing not associated with thunderstorms?

  1. AConvective SIGMET.
  2. BSIGMET.
  3. CAIRMET.
Show answer and explanation

Correct answer: B. SIGMET.

AIM 7-1-6 says a (non-convective) SIGMET is issued for severe icing not associated with thunderstorms, severe or extreme turbulence or CAT, dust and sandstorms reducing visibility below 3 miles, and volcanic ash. Convective SIGMETs cover thunderstorms, and AIRMETs cover moderate icing and turbulence.

Source: AIM 7-1-6

Aircraft systems questions

4 of the 28 the FAA published on this topic for this test.

35

What is one purpose of wing flaps?

  1. ATo enable the pilot to make steeper approaches to a landing without increasing the airspeed.
  2. BTo relieve the pilot of maintaining continuous pressure on the controls.
  3. CTo decrease wing area to vary the lift.
Show answer and explanation

Correct answer: A. To enable the pilot to make steeper approaches to a landing without increasing the airspeed.

Flaps are secondary flight controls that increase both lift and drag, so the airplane can fly a steeper descent angle toward the runway without picking up speed (PHAK Ch. 6; AFH Ch. 9). Relieving the pilot of continuous control pressure is the job of trim tabs, not flaps. Flaps also do not decrease wing area; extending them increases camber (and on some designs wing area) to change lift.

Source: PHAK (FAA-H-8083-25)ACS PA.I.G.K1b

36

With regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be

  1. Amore susceptible to icing.
  2. Bequally susceptible to icing.
  3. Cless susceptible to icing.
Show answer and explanation

Correct answer: A. more susceptible to icing.

In a float-type carburetor, fuel vaporization and the pressure drop in the venturi can cool the air below freezing, so ice can form even at moderate outside air temperatures. A fuel injection system has no venturi and injects fuel at or near the intake ports, so PHAK Ch. 7 describes it as less susceptible to icing than a carburetor system. Therefore carburetors are more, not equally or less, susceptible to icing.

Source: PHAK (FAA-H-8083-25)ACS PA.IX.C.K1b

37

If an aircraft is equipped with a fixed-pitch propeller and a float-type carburetor, the first indication of carburetor ice would most likely be

  1. Aa drop in oil temperature and cylinder head temperature.
  2. Bengine roughness.
  3. Closs of RPM.
Show answer and explanation

Correct answer: C. loss of RPM.

PHAK Ch. 7 states that in an airplane with a fixed-pitch propeller the first indication of carburetor ice is a loss of RPM, because ice restricts the fuel/air flow and reduces power; engine roughness typically follows later. A drop in oil and cylinder head temperature is not the recognized first sign. With a constant-speed propeller the first sign would instead be a drop in manifold pressure.

Source: PHAK (FAA-H-8083-25)ACS PA.IX.C.K1b

38

When activated, an emergency locator transmitter (ELT) transmits on

  1. A118.0 and 118.8 MHz.
  2. B121.5 and 243.0 MHz.
  3. C123.0 and 119.0 MHz.
Show answer and explanation

Correct answer: B. 121.5 and 243.0 MHz.

AIM 6-2-4 says ELTs transmit on 121.5 MHz and 243.0 MHz (and newer ones also on 406 MHz, which satellites monitor, while keeping a 121.5 homing signal). 118.0/118.8 and 123.0/119.0 MHz are ordinary communication frequencies, not emergency beacon frequencies.

Source: AIM 6-2-4

Airport operations questions

3 of the 23 the FAA published on this topic for this test.

39

(Refer to FAA-CT-8080-2H, Figure 48.) The portion of the runway identified by the letter A may be used for

FAA Figure 48Airport diagramFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. Alanding.
  2. Btaxiing and takeoff.
  3. Ctaxiing and landing.
Show answer and explanation

Correct answer: B. taxiing and takeoff.

Area A on Figure 48 is the paved runway section before Runway 12's threshold, marked with white arrows along the centerline and arrowheads ahead of the threshold bar. That is a displaced threshold. Per AIM 2-3-3 and PHAK Ch. 14, the pavement behind a displaced threshold is available for taxiing and for takeoffs in either direction. An aircraft landing on Runway 12 may not touch down there; only the rollout of an aircraft landing in the opposite direction may use it. So it is correctly described as usable for taxiing and takeoff, not for landing.

Source: AIM 2-3-3 · PHAK (FAA-H-8083-25)ACS PA.II.D.K3

40

(Refer to FAA-CT-8080-2H, Figure 47.) While on final approach to a runway equipped with a standard 2-bar VASI, the lights appear as shown by illustration D. This means that the aircraft is

FAA Figure 47VASI illustrationsFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. Aabove the glide path.
  2. Bbelow the glide path.
  3. Con the glide path.
Show answer and explanation

Correct answer: B. below the glide path.

Each VASI light unit shows white in the upper part of its beam and red in the lower part (AIM 2-1-2). On a 2-bar VASI, seeing red on both the near and far bars (illustration D in Figure 47: all six lights red) means the aircraft is below the glide path. Red over white is on the glide path, and white over white is above it.

Source: AIM 2-1-2ACS PA.III.B.K2

41

This sign confirms your position on

Sample test figureRunway holding position sign (22)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. Arunway 22.
  2. Brouting to runway 22.
  3. Ctaxiway 22.
Show answer and explanation

Correct answer: A. runway 22.

The sign shows yellow '22' on a black background with a yellow border, the format of a runway location sign. AIM 2-3-9 says its inscription is the designation of the runway on which the aircraft is located, so it confirms you are on Runway 22. A sign routing you toward a runway would be a direction or destination sign (black on yellow, with an arrow). Taxiways are identified by letters, not numbers.

Source: AIM 2-3-9ACS PA.II.D.K3

Flight instruments questions

3 of the 21 the FAA published on this topic for this test.

42

What does the red line on an airspeed indicator represent?

  1. AManeuvering speed.
  2. BTurbulent or rough-air speed.
  3. CNever-exceed speed.
Show answer and explanation

Correct answer: C. Never-exceed speed.

The red radial line on an airspeed indicator marks VNE, the never-exceed speed; operating above it can cause structural damage or failure (PHAK Ch. 8). Maneuvering speed (VA) is not marked on the airspeed indicator, and the caution range for smooth air only is the yellow arc, whose lower end is VNO, the maximum structural cruising speed.

Source: PHAK (FAA-H-8083-25)ACS PA.I.F.R2

43

Deviation error of the magnetic compass is caused by

  1. Aa northerly turning error.
  2. Bcertain metals and electrical systems within the aircraft.
  3. Cthe difference in location of true north and magnetic north.
Show answer and explanation

Correct answer: B. certain metals and electrical systems within the aircraft.

Deviation is compass error caused by magnetic fields from metal parts and electrical equipment inside the aircraft, and it is recorded on the compass correction card (PHAK Ch. 8). The angular difference between true north and magnetic north is variation, a different error. Northerly turning error is a dip-related error that shows up in turns.

Source: PHAK (FAA-H-8083-25)ACS PA.VI.A.K2

44

(Refer to figure 7.) The proper adjustment to make on the attitude indicator during level flight is to align the

FAA Figure 7Attitude indicatorFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. Ahorizon bar to the level-flight indication.
  2. Bhorizon bar to the miniature airplane.
  3. Cminiature airplane to the horizon bar.
Show answer and explanation

Correct answer: C. miniature airplane to the horizon bar.

PHAK Chapter 8 explains that the pilot adjusts the attitude indicator in level flight by moving the miniature airplane (C in Figure 7) with the adjustment knob so it is aligned with the horizon bar (B). The horizon bar is driven by the gyro and cannot be adjusted by the pilot.

Source: PHAK Chapter 8

Radio communications questions

3 of the 20 the FAA published on this topic for this test.

45

(Refer to FAA-CT-8080-2H, Figure 52.) What is the recommended communications procedure for landing at Lincoln Municipal during the hours when the tower is not in operation?

FAA Figure 52Chart Supplement excerpt (Lincoln, NE)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. AMonitor airport traffic and announce your position and intentions on 118.5 MHz.
  2. BContact UNICOM on 122.95 MHz for traffic advisories.
  3. CMonitor ATIS for airport conditions, then announce your position on 122.95 MHz.
Show answer and explanation

Correct answer: A. Monitor airport traffic and announce your position and intentions on 118.5 MHz.

The Lincoln Chart Supplement entry lists CTAF 118.5, the same frequency as the tower, which operates only 1130-0600Z. When the tower is closed, AIM 4-1-9 calls for pilots to monitor the CTAF and self-announce position and intentions on it, so reports go out on 118.5 MHz. The UNICOM frequency 122.95 is for airport services and advisories, not the CTAF at this airport.

Source: AIM 4-1-9ACS PA.III.A.K2

46

(Refer to FAA-CT-8080-2H, Figure 52.) When approaching Lincoln Municipal from the west at noon for the purpose of landing, initial communications should be with

FAA Figure 52Chart Supplement excerpt (Lincoln, NE)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. ALincoln Approach Control on 124.0 MHz.
  2. BMinneapolis Center on 128.75 MHz.
  3. CLincoln Tower on 118.5 MHz.
Show answer and explanation

Correct answer: A. Lincoln Approach Control on 124.0 MHz.

At noon local time (1700-1800Z), Lincoln's Class C airspace is in effect (service 1130-0600Z). The Chart Supplement says to contact Approach Control. 14 CFR 91.130(c)(1) requires two-way radio communication with the ATC facility providing air traffic services before entering Class C. An aircraft west of the field lies in the 180-359 degree sector, whose approach frequency is 124.0 MHz. The tower is contacted later, when approach hands you off. Minneapolis Center is not the facility that serves this Class C airspace.

Source: 14 CFR 91.130(c)(1)ACS PA.I.D.K1

47

Unless otherwise authorized, if flying a transponder equipped aircraft, a pilot should squawk which VFR code?

  1. A1200
  2. B7600
  3. C7700
Show answer and explanation

Correct answer: A. 1200

AIM 4-1-20 states that, unless otherwise instructed by an ATC facility, VFR pilots set the transponder to Mode 3/A code 1200 regardless of altitude, with altitude reporting enabled. Code 7600 signals a two-way radio communications failure and 7700 signals an emergency, so neither is the normal VFR code.

Source: AIM 4-1-20ACS PA.III.A.K4

Aerodynamics questions

2 of the 17 the FAA published on this topic for this test.

48

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

  1. Achord line of the wing and the relative wind.
  2. Bairplane's longitudinal axis and that of the air striking the airfoil.
  3. Cairplane's center line and the relative wind.
Show answer and explanation

Correct answer: A. chord line of the wing and the relative wind.

Angle of attack is the acute angle between the chord line of the wing and the direction of the relative wind (PHAK Ch. 5). It is measured from the airfoil's chord, not from the airplane's longitudinal axis or centerline. The angle between the longitudinal axis and the horizon is the pitch attitude, and the angle between the chord and the longitudinal axis is the angle of incidence.

Source: PHAK (FAA-H-8083-25)ACS PA.I.F.K3

49

Which statement relates to Bernoulli's principle?

  1. AFor every action there is an equal and opposite reaction.
  2. BAn additional upward force is generated as the lower surface of the airfoil deflects air downward.
  3. CAir traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface.
Show answer and explanation

Correct answer: C. Air traveling faster over the curved upper surface of an airfoil causes lower pressure on the top surface.

Bernoulli's principle says that as the velocity of a moving fluid increases, its pressure decreases (PHAK Ch. 4). Air flowing faster over the curved upper surface of the wing therefore has lower pressure than the air below, and that pressure difference produces lift. The action/reaction statement is Newton's third law, and the downward deflection of air by the lower surface is also a Newtonian explanation of lift, not Bernoulli's principle.

Source: PHAK (FAA-H-8083-25)ACS PA.I.F.K3

Flight operations questions

2 of the 16 the FAA published on this topic for this test.

50

The Aeronautical Information Manual (AIM) specifically encourages pilots to turn on their landing lights when operating below 10,000 feet, day or night, and especially when operating

  1. Ain Class B airspace.
  2. Bin conditions of reduced visibility.
  3. Cwithin 15 miles of a towered airport.
Show answer and explanation

Correct answer: B. in conditions of reduced visibility.

Under the FAA's voluntary 'Operation Lights On' program, AIM 4-3-24 encourages pilots to turn on landing lights below 10,000 feet, day or night. It singles out operations within 10 miles of any airport, in conditions of reduced visibility, and in areas where flocks of birds may be expected. The AIM does not single out Class B airspace, and its distance is 10 miles of any airport, not 15 miles of a towered airport.

Source: AIM 4-3-24ACS PA.III.B.R1

51

(Refer to figure 9, area A.) How should the flight controls be held while taxiing a tricycle-gear equipped airplane into a left quartering headwind?

FAA Figure 9Control position for taxiFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. ALeft aileron up, elevator neutral.
  2. BLeft aileron down, elevator neutral.
  3. CLeft aileron up, elevator down.
Show answer and explanation

Correct answer: A. Left aileron up, elevator neutral.

Area A in Figure 9 is a wind from ahead and to the left, a left quartering headwind. The Airplane Flying Handbook says that in a tricycle-gear airplane you turn the control wheel into the wind, which raises the aileron on the upwind (left) side so the wind cannot lift that wing, and hold the elevator neutral. Lowering the left aileron would let the wind get under the wing, and down elevator is used for tailwinds.

Source: Airplane Flying Handbook

More topics

Aeromedical factors, Performance, Navigation, Weight and balance, Night operations, Charts, Emergency operations, Decision making and risk, Helicopter operations. 9 of the 49 the FAA published on these topics for this test.

52

A pilot experiencing the effects of hyperventilation should be able to restore the proper carbon dioxide level in the body by

  1. Aslowing the breathing rate, breathing into a paper bag, or talking aloud.
  2. Bbreathing spontaneously and deeply or gaining mental control of the situation.
  3. Cincreasing the breathing rate in order to increase lung ventilation.
Show answer and explanation

Correct answer: A. slowing the breathing rate, breathing into a paper bag, or talking aloud.

Hyperventilation is an excessive loss of carbon dioxide caused by breathing too fast or too deeply. PHAK Ch. 17 lists the cure as slowing the breathing rate, breathing into a paper bag, or talking aloud, and AIM 8-1-3 likewise says symptoms subside once breathing is brought back under control and that breathing into a paper bag speeds the rebuilding of CO2. Breathing more deeply or faster would make the CO2 deficit worse.

Source: PHAK (FAA-H-8083-25) · AIM 8-1-3ACS PA.I.H.K1b

53

(Refer to FAA-CT-8080-2H, Figure 38.) Determine the approximate landing ground roll distance. Pressure altitude: 5,000 ft Headwind: Calm Temperature: 101°F

FAA Figure 38Airplane landing distance tableFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. A445 feet.
  2. B545 feet.
  3. C495 feet.
Show answer and explanation

Correct answer: B. 545 feet.

The 5,000-foot column of Figure 38 is based on 41 degrees F, which is the standard temperature at that altitude, and shows a 495-foot ground roll. Note 2 adds 10% for each 60 degrees F above standard. The given 101 degrees F is 60 degrees F above standard, so 495 x 1.10 = 544.5, about 545 feet. The calm wind means no headwind reduction. 445 feet is the sea-level value, and 495 feet leaves out the temperature correction.

ACS PA.I.F.K1

54

When the course deviation indicator (CDI) needle is centered using a VOR test signal (VOT), the omnibearing selector (OBS) and the TO/FROM indicator should read

  1. A180° FROM, only if the pilot is due north of the VOT.
  2. B0° TO or 180° FROM, regardless of the pilot's position from the VOT.
  3. C0° FROM or 180° TO, regardless of the pilot's position from the VOT.
Show answer and explanation

Correct answer: C. 0° FROM or 180° TO, regardless of the pilot's position from the VOT.

A VOT transmits a test signal that radiates the same 360 radial in all directions, so the result does not depend on where the aircraft is. AIM 1-1-4 states that with the CDI centered, the OBS should read 0 degrees with a FROM indication or 180 degrees with a TO indication (an RMI shows 180). The reversed pairing (0 TO / 180 FROM) and any position-dependent reading are incorrect.

Source: AIM 1-1-4ACS PA.VI.B.K1

55

(Refer to FAA-CT-8080-2H, Figures 32 and 33.) Which action can adjust the airplane's weight to maximum gross weight and the CG within limits for takeoff? Front seat occupants: 425 lb Rear seat occupants: 300 lb Fuel, main tanks: 44 gal

FAA Figures 32 and 33Airplane weight and balance tablesFAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. ADrain 12 gallons of fuel.
  2. BDrain 9 gallons of fuel.
  3. CTransfer 12 gallons of fuel from the main tanks to the auxiliary tanks.
Show answer and explanation

Correct answer: B. Drain 9 gallons of fuel.

From Figure 32: empty 2,015 lb (moment/100 1,554); front seats 425 lb x 85 in = 361.3; rear seats 300 lb x 121 in = 363.0; 44 gal main fuel 264 lb (198). Total 3,004 lb, 54 lb over the 2,950 lb maximum. At 6 lb per gallon, draining 9 gallons removes exactly 54 lb: 35 gal = 210 lb, moment 158, giving 2,950 lb and moment/100 2,436.3, inside the Figure 33 limits of 2,422 to 2,499 at 2,950 lb (CG about 82.6 in). Draining 12 gallons would leave the airplane below, not at, maximum gross weight, and transferring fuel to the auxiliary tanks does not reduce weight at all (still 3,004 lb).

ACS PA.I.F.K2f

56

The definition of nighttime is

  1. Asunset to sunrise.
  2. B1 hour after sunset to 1 hour before sunrise.
  3. Cthe time between the end of evening civil twilight and the beginning of morning civil twilight.
Show answer and explanation

Correct answer: C. the time between the end of evening civil twilight and the beginning of morning civil twilight.

14 CFR 1.1 defines night as the time between the end of evening civil twilight and the beginning of morning civil twilight, as published in the Air Almanac and converted to local time. Sunset to sunrise is the period for position lights (91.209), and 1 hour after sunset to 1 hour before sunrise is the passenger-carrying recency period (61.57(b)).

Source: 14 CFR 1.1

57

(Refer to FAA-CT-8080-2H, Figure 25, area 5.) The navigation facility at Dallas-Ft. Worth International (DFW) is a

FAA Figure 25Sectional chart excerpt (Dallas-Fort Worth, TX)FAA-CT-8080-2H · Sport, Recreational, Private & Remote Pilot supplement
  1. AVOR.
  2. BVORTAC.
  3. CVOR/DME.
Show answer and explanation

Correct answer: C. VOR/DME.

Next to area 5 on Figure 25, the navaid symbol at Dallas/Ft. Worth International is a hexagon with a center dot enclosed in a square, which the Aeronautical Chart User's Guide identifies as a VOR/DME. A plain VOR is a hexagon without the square, and a VORTAC is a hexagon with three small rectangles attached to alternate sides.

Source: Chart User's GuideACS PA.I.E.K2

58

While on a VFR cross country and not in contact with ATC, what frequency would you use in the event of an emergency?

  1. A121.5 MHz.
  2. B122.5 MHz.
  3. C128.725 MHz.
Show answer and explanation

Correct answer: A. 121.5 MHz.

121.5 MHz is the international VHF emergency frequency. It is monitored by ATC facilities, many FSSs and military facilities, so a pilot who is not already talking to ATC should use it to declare a distress or urgency situation (AIM 6-3-1). 122.5 MHz is a flight service frequency and 128.725 MHz is not an emergency frequency, so neither is guaranteed to reach an emergency service.

Source: AIM 6-3-1ACS PA.III.A.K1

59

A pilot and two passengers landed on a 2,100 foot east-west gravel strip with an elevation of 1,800 feet. The temperature is warmer than expected and after computing the density altitude it is determined the takeoff distance over a 50 foot obstacle is 1,980 feet. The airplane is 75 pounds under gross weight. What would be the best choice?

  1. ATaking off into the headwind will give the extra climb-out time needed.
  2. BTry a takeoff without the passengers to make sure the climb is adequate.
  3. CWait until the temperature decreases, and recalculate the takeoff performance.
Show answer and explanation

Correct answer: C. Wait until the temperature decreases, and recalculate the takeoff performance.

The computed 1,980 feet to clear a 50-foot obstacle leaves only 120 feet of the 2,100-foot strip, with no margin for a gravel surface, pilot technique or an aging engine. Density altitude is the problem, and it improves as the temperature drops (PHAK Ch. 11). Sound ADM (PHAK Ch. 2; Risk Management Handbook) is to wait for cooler air and recompute performance. Counting on a headwind that may not be there, or 'testing' a marginal takeoff even with a lighter load, accepts an unmitigated risk instead of removing it.

Source: PHAK (FAA-H-8083-25) · Risk Management HandbookACS PA.I.H.K4

60

Ground resonance is most likely to develop when

  1. Aon the ground and harmonic vibrations develop between the main and tail rotors.
  2. Ba series of shocks causes the rotor system to become unbalanced.
  3. Cthere is a combination of a decrease in the angle of attack on the advancing blade and an increase in the angle of attack on the retreating blade.
Show answer and explanation

Correct answer: B. a series of shocks causes the rotor system to become unbalanced.

The Helicopter Flying Handbook explains that ground resonance occurs on the ground when a series of shocks (for example a hard landing on one skid or gear) unbalances the rotor system and the oscillation builds through the landing gear. It is not a main/tail rotor harmonic, and the change in angle of attack between advancing and retreating blades describes dissymmetry of lift.

Source: Helicopter Flying Handbook

How to use these questions to pass the PAR

  1. 1Cover the explanation, answer, then open it. If you got it right for the wrong reason, count it as wrong.
  2. 2Group your misses by topic. Two misses in the same heading (say, airspace) tell you more than your total score.
  3. 3Do the chart and weight-and-balance questions with the real figure open at full size, the way you will on test day.
  4. 4When you score 80% or better on fresh questions twice in a row, book the test: the FAA needs 70%, and the margin covers test-day nerves.
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Private Pilot test questions: FAQ

How many questions are on the FAA Private Pilot written test?

60 scored questions plus 5 unscored validation questions, with 2 hours to finish. Each question has three answer choices and you need 70% (42 of 60) to pass. Sources: FAA Airman Knowledge Testing Matrix and the PSI PAR bulletin.

Are these the real FAA Private Pilot test questions?

They are real FAA questions, published by the FAA itself: its August 2021 PAR sample test and its 2008 Private Pilot question bank. The questions on the live test are confidential and different, but they test the same knowledge, so the explanations matter more than memorizing answers.

What score do I need to pass the PAR?

70%. In 2025, 89.56% of 44,657 PAR attempts passed, with an average score of 81.64% (FAA CY2025 Airman Knowledge Test Volume Report).

Do I need an endorsement to take the Private Pilot written?

Yes. You need an endorsement from an authorized instructor or a ground-school completion certificate (14 CFR 61.35). After a failure you need an instructor endorsement for additional training before retesting (14 CFR 61.49).

How long is a passed Private Pilot knowledge test valid?

24 calendar months: you must take the checkride within that window (14 CFR 61.39).

Renzo Madueño

Written and reviewed by Renzo Madueño

Former Airbus A320 First Officer (Avianca), FAA commercial pilot · Founder, Rotate Pilot

The questions are the FAA's own words. The FAA does not publish an answer key, so each answer here was worked out against the regulations and handbooks in force today, and every explanation names its source so you can check it yourself. Questions whose answer changed with newer rules were left out. Found something wrong? Tell us and we fix it.

Last reviewed . Rotate Pilot is independent and not affiliated with the FAA, PSI or any aviation authority.