FAA Private Pilot Test Guide Review

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A set of flashcards based on FAA Private Pilot Test Guide notes covering definitions, regulations, and procedures relevant to aviation and pilot certification.

Last updated 10:55 PM on 3/26/26
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277 Terms

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Nighttime

A period beginning one hour after sunset and one hour before sunrise.

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Certification Categories of Aircraft

Airplane, rotorcraft, powered lift, glider.

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FAA BasicMed Rule

Allows pilots to operate small aircraft using a driver license instead of a medical certificate.

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Complex Airplane

An airplane with retractable landing gear, flaps, and a controllable-pitch propeller or FADEC.

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ARROW

Airworthiness certificate, Registration, Radio station license, Operating limitations, Weight and balance.

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ELT Inspection Requirement

Must occur every 12 months.

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Operating Limitations

Can be found in the form of placards.

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Aircraft Registration Validity

7 years from the date of issuance.

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Emergency Locator Transmitter Operation Limit

May operate a maximum of 60 minutes before the battery needs recharging.

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Preflight Inspection for First Flight

Should be thorough and systematic as recommended by the manufacturer.

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Maintenance Records for Airworthy Directives

Aircraft maintenance records must show compliance.

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14 CFR 43.7

Regulation that allows private pilots to perform preventative maintenance.

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Minimum Equipment List (MEL)

Must be used if your airplane is equipped with one.

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Inoperative Equipment Conditions for VFR Flight

The equipment must not be required by FAR 91.205, an equipment list, or KOEL.

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Special Flight Permit Application

Must be submitted to the nearest FAA FSDO.

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Float Type Carburetors Operation Principle

Based on the difference in air pressure at the venturi throat and the air inlet.

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Carburetor Heat Application Effect

Makes the fuel/air mixture richer.

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Detonation during Climbout Initial Action

Lower the nose slightly to increase airspeed.

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Fuel-Injected Engine Starting Procedure

Using the electric auxiliary fuel pump to prime the engine can help purge vapor.

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Engine Overheating Cooling Action

Reduce rate of climb and increase airspeed.

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Constant Speed Propeller Advantage

Permits the pilot to select the blade angle for the most efficient performance.

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FADEC Preflight Checks

Verify proper operation of both ECUs and their backup power sources.

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Engine Starting Best Practices in Cold Weather

Pre-heating, using external power.

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Alternator Failure Management Action

Shed electrical load to preserve battery power.

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Situations Requiring Emergency Descent

Loss of cabin pressurization, engine fire, smoke on the flight deck.

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Emergency Descent Procedure

Establish a descending turn at 30-45 degrees.

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Flaps Non-Extension Effect on Landing

The glide path is less steep, and floating during the flare is likely.

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Pitot Tube and Static Vents Clogging Effect

Affects the altimeter, airspeed indicator, and vertical speed indicator.

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Vso Definition

Stalling speed or minimum steady flight speed in the landing configuration.

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Power-off Stalling Speed Color

Identified by the lower limit of the green arc.

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Normal Flap Operating Range Color

Identified by the white arc.

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OAT Warmth Impact on Density Altitude

Higher than pressure altitude.

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Flight through Pressure Areas Effect without Adjustment

Altimeter indicates higher than actual altitude.

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Altimeter Adjustment from 29.15 to 29.85 Impact

700 feet increase in indicated altitude.

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Density Altitude Increase Factor

Increase in ambient temperature.

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Magnetic Variation Definition

The angular difference between true north and magnetic north.

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Northern Hemisphere Magnetic Compass Behavior during Left Turn

Indicates a turn toward the east.

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Northern Hemisphere Compass Behavior during East/West Acceleration

Indicates a turn toward the north.

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Backup for PFD Instruments Failure

Display PFD instruments on the MFD screen.

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Standard-Rate Turn with Instruments Procedure

Monitor the trend vector on the HSI and adjust the angle of bank.

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Air Data Computer Instruments

Airspeed indicator, altimeter, VSI.

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Flaps Function during Landing Approach

Increase angle of descent without increasing airspeed.

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Wing Flaps Purpose

Enable steeper approaches without increasing airspeed.

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Inherently Stable Airplane Definition

Requires less effort to control.

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Tendency to Pitch Up and Stall Situation

Shifting the center of gravity toward the rear.

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Common Stall Indication

Flight controls become less responsive.

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Spin Recovery Difficulty Factor in Small Aircraft

CG too far rearward and rotation around the CG.

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Incipient Phase of a Spin Characteristic

Occurs within 4 to 6 seconds.

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Nose High Recovery Sequence

Add power, lower the nose, level wings.

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Engine Failure Approach Statement

A stabilized approach at best glide speed provides maximum gliding distance.

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Excess Load on Airplane Wing Dependence

Depends upon the speed of the airplane.

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Overbanking Tendency Cause in Turn

Additional lift on the raised wing.

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Rate and Radius of Turn Relationship

For a specific angle of bank and airspeed, the rate and radius of turn will not vary.

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Rate Increase and Radius Decrease Action

Maintain bank and decrease airspeed.

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Load Factor Increase during Stall

Causes the airplane to stall at a higher speed.

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Imminent Accelerated Stall Situation

Improperly performing a steep turn.

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Energy Management True Statement

An airplane that is low and slow on final approach is a total energy error.

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Flying on the Back Side of the Power Curve Impact

Any decrease in airspeed requires an increase in power to maintain flight.

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Preflight Action Requirement for Flights Away from Airport

Must include an alternate course of action.

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In-Flight Emergency Deviation Allowance

May deviate from FARs as necessary to meet the emergency.

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Cockpit Display of Traffic Information Purpose

Continuously scan for traffic and cross-check CDTI.

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Lighted Position Lights Display Requirement

From sunset to sunrise, except in Alaska.

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Aerobatic Flight Prohibition Area

Class E below 1,500 feet AGL.

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Approved Natural Material Parachute Packing Requirement

Packed by a certified parachute rigger within the preceding 60 days.

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Minimum Safe Altitude over Congested Area

1,000 feet above the highest obstacle within a horizontal radius of 2,000 feet.

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Safety Belts Requirement

Must be secured for passengers during takeoff, taxi, and landing.

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NTSB 830 Notification Requirement for Elevator Malfunction

Must notify the nearest NTSB office immediately.

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Accident Report Filing Requirement

Required within 10 days by the operator of an aircraft involved in an accident.

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Cabin Door Opening Management Action

Perform a normal traffic pattern and landing.

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Emergency Equipment Familiarity Requirement

Must know how to use specific equipment on board.

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Runway Numbers Indication

Indicate orientation approximately 090 and 270 magnetic.

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Recommended Entry Position to Traffic Pattern

45 degrees at the midpoint of the downwind leg at traffic pattern altitude.

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Wind Direction Landing Expectation

Land on runway 18 and expect a crosswind from the right.

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Segmented Circle Indication for Runway 36

Left hand for runway 36; right hand for runway 18.

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Landing on Runway 26 Wind Indication

With a right-quarting headwind.

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Traffic Pattern Procedure Indication by Wind Cone

Left hand traffic on runway 36.

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Position Declaration when Calling Tower for Takeoff

State your position, especially when departing from a runway intersection.

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Yellow Demarcation Bar Marking Indicator

Indicates a displaced threshold from the blast pad.

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Visual Clue for Taxiway Location Confirmation

Confirms the aircraft's location on taxiway B.

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Marking Confirmation from Cockpit

Confirms aircraft is on a runway, about to clear.

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Statement Validation about Runway 12

Takeoff may start at position A; landing begins at position B.

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Area A and Area E Difference on Airport Diagram

A used for taxi and takeoff; E only for overturn.

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Vehicle Lane Marking Identification

Indicated by the letter C on the diagram.

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Arrow Ends on North/South Runway Indication

Cannot be used for landing, but may be for taxiing and takeoff.

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Runway Incursion Prevention Suggestion

Use exterior taxi/landing lights in low visibility.

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Runway/Runway Hold Position Sign Purpose

Denotes intersecting runways.

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Outbound Destination Sign Identification

Identifies direction to takeoff runway.

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Landing Distance Available (ALD) Data Publication Location

Published in the special notices section of the chart supplements.

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Minimum Visibility for LAHSO Clearance

3 statute miles.

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Airport Rotating Beacon Daylight Operation Indication

That weather at the airport is below basic VFR minimums.

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Class D Visual Approach Slope Indicator Altitude Maintenance Requirement

Maintain altitude at or above glide slope until lower altitude necessary.

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High Intensity Runway Lights Setting Process

Click the microphone seven times then five times in five seconds.

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Currituck County Airport Latitude and Longitude

36 24N - 76 01W.

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Washburn Airport Approximate Location

24 21’30N latitude and 101 01’30 longitude.

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Putnam Airport Approximate Location

41 02’00” latitude and 83 59’00”W longitude.

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Garrison Airport CTAF/MULTICOM Frequency

122.9.

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Wyandot County Airport CTAF/MULTICOM Frequency

112.9.

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Coeur D’Alene Common Advisory Frequency (CTAF)

122.8.

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Toledo Approach Contact Frequency

126.1 MHz.

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Dallas Executive Tower Advisory Frequency when Tower Not in Operation

127.25 MHz.

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