Private Pilot Knowledge Test: Chapter 2
What regulation allows a private pilot to perform preventive maintenance? A - 14 CFR 43.7. B - 14 CFR 91.403. C - 14 CFR 61.113.
A - 14 CFR 43.7.
A 100-hour inspection was due at 3303 hours. The 100-hour inspection was actually done at 3300 hours. When is the next 100-hour inspection due? A - 3400 hours. B - 3403 hours. C - 3413 hours.
A - 3400 hours.
(Refer to Figure 4.) What is the full flap operating range for the airplane? A - 55 to 100 knots. B - 55 to 208 knots. C - 55 to 165 knots.
A - 55 to 100 knots.
(Refer to Figure 3.) Altimeter 3 indicates A - 9,500 feet. B - 10,950 feet. C - 15,940 feet.
A - 9,500 feet.
What should be the first action after starting an aircraft engine? A - Adjust for proper RPM and check for desired indications on the engine gauges. B - Place the magneto or ignition switch momentarily in the OFF position to check for proper grounding. C - Test each brake and the parking brake.
A - Adjust for proper RPM and check for desired indications on the engine gauges.
Which records or documents shall the owner or operator of an aircraft keep to show compliance with an applicable Airworthiness Directive? A - Aircraft maintenance records. B - Airworthiness certificate and pilot's operating handbook. C - Airworthiness and registration certificates.
A - Aircraft maintenance records.
What aircraft inspections are required for rental aircraft that are also used for flight instruction? A - Annual and 100-hour inspections. B - Biannual and 100-hour inspections. C - Annual and 50-hour inspections.
A - Annual and 100-hour inspections.
During the runup at a high elevation airport, you notice a slight engine roughness that is not affected by the magneto check but grows worse during the carburetor heat check. Under these circumstances, what would be the most logical initial action? A - Check the results obtained with a leaner setting of the mixture. B - Taxi back to the flight line for a maintenance check. C - Reduce manifold pressure to control detonation.
A - Check the results obtained with a leaner setting of the mixture.
What is one procedure to aid in cooling an engine that is overheating? A - Enrichen the fuel mixture. B - Increase the RPM. C - Reduce the airspeed.
A - Enrichen the fuel mixture.
How do variations in temperature affect the altimeter? A - Pressure levels are raised on warm days and the indicated altitude is lower than true altitude. B - Higher temperatures expand the pressure levels and the indicated altitude is higher than true altitude. C - Lower temperatures lower the pressure levels and the indicated altitude is lowered than true altitude.
A - Pressure levels are raised on warm days and the indicated altitude is lower than true altitude.
What action can a pilot take to aid in cooling an engine that is overheating during a climb? A - Reduce rate of climb and increase airspeed. B - Reduce climb speed and increase RPM. C - Increase climb speed and increase RPM.
A - Reduce rate of climb and increase airspeed.
While cruising at 9,500 feet MSL, the fuel/air mixture is properly adjusted. What will occur if a descent to 4,500 feet MSL is made without readjusting the mixture? A - The fuel/air mixture can become excessively lean. B - There can be more fuel in the cylinders than is needed for normal combustion, and the excess fuel will absorb heat and cool the engine. C - The excessively rich mixture creates higher cylinder head temperatures and can cause detonation.
A - The fuel/air mixture can become excessively lean.
What type fuel can be substituted for an aircraft if the recommended octane is not available? A - The next higher octane aviation gas. B - The next lower octane aviation gas. C - Unleaded automotive gas of the same octane rating.
A - The next higher octane aviation gas.
How is engine operation controlled on an engine equipped with a constant-speed propeller? A - The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM. B - The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates a constant blade angle. C - The throttle controls engine RPM as registered on the tachometer and the mixture control regulates the power output.
A - The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM.
What is true altitude? A - The vertical distance of the aircraft above the level. B - The vertical distance of the aircraft above the surface. C - The height above the standard datum plane.
A - The vertical distance of the aircraft above the level.
How should an aircraft preflight inspection be accomplished for the first flight of the day? A - Thorough and systematic means recommended by the manufacturer. B - Quick walk around with a check of gas and oil. C - Any sequence as determined by the pilot-in-command.
A - Thorough and systematic means recommended by the manufacturer.
Which would most likely cause the cylinder head temperature and engine oil temperature gauges to exceed their normal operating ranges? A - Using fuel that has a lower-than-specified fuel rating. B - Using fuel that has a higher-than-specified fuel rating. C - Operating with higher-than-normal oil pressure.
A - Using fuel that has a lower-than-specified fuel rating.
Which V-speed represents maneuvering speed? A - V(A). B - V(LO). C - V(NE).
A - V(A).
Which V-speed represents maximum flap extended speed? A - V(FE). B - V(LOF). C - V(FC).
A - V(FE).
Which V-speed represents maximum landing gear extended speed? A - V(LE). B - V(LO). C - V(FE).
A - V(LE).
Which preflight checks should you make on an airplane with full-authority digital engine control (FADEC)? A - Verify proper operation of both ECUs as well as their back-up power sources. B - Ensure that engine RPM drops sufficiently when the propeller control is pulled back. C - Ensure that the mixture control is adjusted for highest RPM with smooth engine operation.
A - Verify proper operation of both ECUs as well as their back-up power sources.
Generally speaking, the use of carburetor heat tends to A - decrease engine performance. B - increase engine performance. C - have no effect on engine performance.
A - decrease engine performance.
If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will most likely cause A - detonation. B - a mixture of fuel and air that is not uniform in all cylinders. C - lower cylinder head temperatures.
A - detonation.
The risk of carburetor ice is A - high when the ambient temperature is between 20°F and 70°F and the relative humidity is high. B - nonexistent at 95°F even when there is visible moisture. C - high at 0°F when the relative humidity is high.
A - high when the ambient temperature is between 20°F and 70°F and the relative humidity is high.
One purpose of the dual ignition system on an aircraft engine is to provide for A - improved engine performance. B - uniform heat distribution. C - balanced cylinder head pressure.
A - improved engine performance.
With regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be A - more susceptible to icing. B - equally susceptible to icing. C - less susceptible to icing.
A - more susceptible to icing.
The responsibility for ensuring that maintenance personnel make the appropriate entries in the aircraft maintenance records indicating the aircraft has been approved for return to service lies with the A - owner or operator. B - pilot in command. C - mechanic who performs the work.
A - owner or operator.
V(S0) is defined as the A - stalling speed or minimum steady flight speed in the landing configuration. B - stalling speed or minimum steady flight speed in a specified configuration. C - stalling speed or minimum takeoff safety speed.
A - stalling speed or minimum steady flight speed in the landing configuration.
Prior to takeoff, the altimeter should be set to A - the current local altimeter setting, if available, or the departure airport elevation. B - the corrected density altitude of the departure airport. C - the corrected pressure altitude of the departure airport.
A - the current local altimeter setting, if available, or the departure airport elevation.
Detonation may occur at high-power settings as A - the fuel mixture ignites instantaneously instead of burning progressively and evenly. B - an excessively rich fuel mixture causes an explosive gain in power. C - the fuel mixture is ignited too early bu hot carbon deposits in the cylinder.
A - the fuel mixture ignites instantaneously instead of burning progressively and evenly.
An abnormally high engine oil temperature indication may be caused by A - the oil level being too low. B - operating with a too high viscosity oil. C - operating with an excessively rich mixture.
A - the oil level being too low.
(Refer to Figure 3.) Which altimeter(s) indicate(s) more than 10,000 feet? A - 1, 2, and 3. B - 1 and 2 only. C - 1 only.
B - 1 and 2 only.
(Refer to Figure 4.) What is the maximum flap extended speed? A - 58 knots. B - 100 knots. C - 165 knots.
B - 100 knots.
An aircraft had a 100-hour inspection when the tachometer read 1259.6. When is the next 100-hour inspection due? A - 1349.6 hours. B - 1359.6 hours. C - 1369.6 hours.
B - 1359.6 hours.
(Refer to Figure 4.) What is the maximum structural cruising speed? A - 100 knots. B - 165 knots. C - 208 knots.
B - 165 knots.
Which preflight action is specifically required of the pilot prior to each flight? A - Check the aircraft logbooks for appropriate entries. B - Become familiar with all available information concerning the flight. C - Review wake turbulence avoidance procedures.
B - Become familiar with all available information concerning the flight.
What is an important airspeed limitation that is not color coded on airspeed indicators? A - Never-exceed speed. B - Maneuvering speed. C - Maximum structural cruising speed.
B - Maneuvering speed.
Who is responsible for ensuring that airworthiness directives (ADs) are complied with? A - Mechanic with inspection authorization (IA). B - Owner or operator. C - Repair station.
B - Owner or operator.
What is an advantage of a constant-speed propeller? A - Permits the pilot to select and maintain a desired cruising speed. B - Permits the pilot to select the blade angle for the most efficient performance. C - Provide a smoother operation with table RPM and eliminates vibrations.
B - Permits the pilot to select the blade angle for the most efficient performance.
Who may perform preventative maintenance on an aircraft and approve it for return to service? A - Student or Recreational pilot. B - Private or Commercial pilot. C - None of the above.
B - Private or Commercial pilot.
Which operation would be described as preventive maintenance? A - Repair of landing gear brace struts. B - Replenishing hydraulic fluid. C - Repair of portions of skin sheets by making additional seams.
B - Replenishing hydraulic fluid.
If the pitot tube and outside static vents become clogged, which instruments would be affected? A - The altimeter, airspeed indicator, and turn-and-slip indicator. B - The altimeter, airspeed indicator, and vertical speed indicator. C - altimeter, attitude indicator, and turn-and-slip indicator.
B - The altimeter, airspeed indicator, and vertical speed indicator.
What is pressure altitude? A - The indicated altitude corrected for position and installation error. B - The altitude indicated when the barometric pressure scale is set to 29.92. C - The indicated altitude corrected for nonstandard temperature and pressure.
B - The altitude indicated when the barometric pressure scale is set to 29.92.
If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter? A - The elevation of the nearest airport corrected to mean sea level. B - The elevation of the departure area. C - Pressure altitude corrected for nonstandard temperature.
B - The elevation of the departure area.
What change occurs in the fuel/air mixture when carburetor heat is applied? A - A decrease in RPM results from the lean mixture. B - The fuel/air mixture becomes richer. C - The fuel/air mixture becomes leaner.
B - The fuel/air mixture becomes richer.
Who is responsible for determining if an aircraft is in condition for safe flight? A - A certificated aircraft mechanic. B - The pilot in command. C - The owner or operator.
B - The pilot in command.
What is density altitude? A - The height above the standard datum plane. B - The pressure altitude corrected for nonstandard temperature. C - The altitude read directly from the altimeter.
B - The pressure altitude corrected for nonstandard temperature.
What is absolute altitude? A - The altitude read directly from the altimeter. B - The vertical distance of the aircraft above the surface. C - The height above the standard datum plane.
B - The vertical distance of the aircraft above the surface.
What should an owner or operator know about Airworthiness Directives (ADs)? A - They are for informational purposes only. B - They are mandatory. C - They are voluntary.
B - They are mandatory.
When are non-rechargeable batteries of an emergency locator transmitter (ELT) required to be replaced? A - Every 24 months. B - When 50 percent of their useful life expires. C - At the time of each 100-hour or annual inspection.
B - When 50 percent of their useful life expires.
Under what condition is indicated altitude the same as true altitude? A - If the altimeter has no mechanical error. B - When at sea level under standard conditions. C - When at 18,000 feet MSL with the altimeter set at 29.92.
B - When at sea level under standard conditions.
When must batteries in an emergency locator transmitter (ELT) be replaced or recharged, if rechargeable? A - After any inadvertent activation of the ELT. B - When the ELT has been in use for more than one cumulative hour. C - When the ELT can no longer be heard over the airplane's communication radio receiver.
B - When the ELT has been in use for more than one cumulative hour.
Completion of an annual inspection and the return of the aircraft to service should always be indicated by A - the relicensing date on the Registration Certificate. B - an appropriate notation in the aircraft maintenance records. C - an inspection sticker placed on the instrument panel that lists the annual inspection completion date.
B - an appropriate notation in the aircraft maintenance records.
A precaution for the operation of an engine equipped with a constant-speed propeller is to A - avoid high RPM settings with high manifold pressure. B - avoid high manifold pressure settings with low RPM. C - always use a rich mixture with high RPM settings.
B - avoid high manifold pressure settings with low RPM.
If it becomes necessary to hand-prop an airplane engine, it is extremely important that a competent pilot A - call "contact" before touching the propeller. B - be at the controls in the cockpit. C - be in the cockpit and call out all commands
B - be at the controls in the cockpit.
Excessively high engine temperatures will A - cause damage to heat-conducting hoses and warping of the cylinder cooling fins. B - cause loss of power, excessive oil consumption, and possible permanent internal engine damage. C - not appreciably affect an aircraft engine.
B - cause loss of power, excessive oil consumption, and possible permanent internal engine damage.
The basic purpose of adjusting the fuel/air mixture at altitude is to A - decrease the amount of fuel in the mixture in order to compensate for increased air density. B - decrease the fuel flow in order to compensate for decreased air density. C - increase the amount of fuel in the mixture to compensate for the decrease in pressure and density of the air.
B - decrease the fuel flow in order to compensate for decreased air density.
Applying carburetor heat will A - result in more air going through the carburetor. B - enrich the fuel/air mixture. C - not affect the fuel/air mixture.
B - enrich the fuel/air mixture.
You suspect that your engine (with a fixed-pitch propeller) is detonating during climbout after takeoff. Your initial corrective action would be to A - lean the mixture. B - lower the nose slightly to increase airspeed. C - apply carburetor heat.
B - lower the nose slightly to increase airspeed.
The responsibility for ensuring that an aircraft is maintained in an airworthy condition is primarily that of the A - pilot in command. B - owner or operator. C - mechanic who performs the work.
B - owner or operator.
The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as A - combustion. B - preignition. C - detonation.
B - preignition.
Float-type carburetors operate based on A - automatic metering of air at the venturi as the aircraft gain altitude. B - the difference in air pressure at the venturi throat and the air inlet. C - increase in air velocity in the throat of a venturi causing an increase in air pressure.
B - the difference in air pressure at the venturi throat and the air inlet.
(Refer to Figure 3.) Altimeter 1 indicates A - 500 feet. B - 1,500 feet. C - 10,500 feet.
C - 10,500 feet.
(Refer to Figure 3.) Altimeter 2 indicates A - 1,500 feet. B - 4,500 feet. C - 14,500 feet.
C - 14,500 feet.
(Refer to Figure 4.) What is the caution range of the airplane? A - 0 to 55 knots. B - 100 to 165 knots. C - 165 to 208 knots.
C - 165 to 208 knots.
(Refer to Figure 4.) The maximum speed at which the airplane can be operated in smooth air is A - 100 knots. B - 165 knots. C - 208 knots.
C - 208 knots.
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? A - 3312.5 hours. B - 3395.5 hours. C - 3402.5 hours.
C - 3402.5 hours.
If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs? A - 70-foot decrease in indicated altitude. B - 700-foot decrease in indicated altitude. C - 700-foot increase in indicated altitude.
C - 700-foot increase in indicated altitude.
The pitot system provides impact pressure for which instrument? A - Altimeter. B - Vertical-speed indicator. C - Airspeed indicator.
C - Airspeed indicator.
Which instrument(s) become inoperative if the static vents become clogged? A - Airspeed only. B - Altimeter only. C - Airspeed, altimeter, and vertical speed.
C - Airspeed, altimeter, and vertical speed.
Which instrument become inoperative if the pitot tube becomes clogged? A - Altimeter. B - Vertical speed. C - Airspeed.
C - Airspeed.
How long does the airworthiness certificate of an aircraft remain valid? A - As long as the aircraft has a current registration certificate. B - Indefinitely, unless the aircraft suffers major damage. C - As long as the aircraft is maintained and operated as required by the Federal Aviation Regulations.
C - As long as the aircraft is maintained and operated as required by the Federal Aviation Regulations.
Which of the following are required to be carried in the aircraft during flight? A - Pilot's information manual (PIM). B - Pilot's operating handbook (POH). C - FAA-approved Airplane Flight Manual (AFM).
C - FAA-approved Airplane Flight Manual (AFM).
Where can the operating limitations for an aircraft be found? A - On the airworthiness certificate. B - In the aircraft airframe and engine logbooks. C - In the current, FAA-approved flight manual, approved manual material, markings, and placards, or any combination thereof.
C - In the current, FAA-approved flight manual, approved manual material, markings, and placards, or any combination thereof.
An annual inspection was performed on an aircraft June 12, 2018. When is the next annual inspection due? A - June 1, 2019. B - June 13, 2019. C - June 30, 2019.
C - June 30, 2019.
(Refer to Figure 4.) Which color identifies the power-off stalling speed in a specified configuration? A - Upper limit of the green arc. B - Upper limit of the white arc. C - Lower limit of the green arc.
C - Lower limit of the green arc.
(Refer to Figure 4.) Which color identifies the power-off stalling speed with the wing flaps and landing gear in the landing configuration? A - Upper limit of the green arc. B - Upper limit of the white arc. C - Lower limit of the white arc.
C - Lower limit of the white arc.
What does the red line on an airspeed indicator represent? A - Maneuvering speed. B - Turbulence or rough-air speed. C - Never-exceed speed.
C - Never-exceed speed.
In addition to a valid airworthiness certificate, what documents or records must be aboard an aircraft during flight? A - Aircraft engine and airframe logbooks, and owner's manual. B - Radio operator's permit, and repair and alteration forms. C - Operating limitations and registration certificate.
C - Operating limitations and registration certificate.
Who is responsible for ensuring appropriate entries are made in maintenance records indicating the aircraft has been approved for return to service? A - Repair station. B - Certified mechanic. C - Owner or operator.
C - Owner or operator.
Maintenance records show the last transponder inspection was performed on September 1, 2014. The next inspection is due no later than A - September 30, 2015. B - September 1, 2016. C - September 30, 2016.
C - September 30, 2016.
Which condition is most favorable to the development of carburetor icing? A - Any temperature below freezing and a relative humidity of less than 50 percent. B - Temperature between 32°F and 50°F and low humidity. C - Temperature between 20°F and 70°F and high humidity.
C - Temperature between 20°F and 70°F and high humidity.
You discover inoperative equipment on an airplane that you are planning to fly. Under what conditions can you complete the flight under VFR? A - The equipment is not required by FAR 91.205. B - The pilot in command, who has at least a private pilot certificate, determines the airplane is in a safe condition for flight. C - The equipment is not required by FAR 91.205, an equipment list or KOEL, the VFR-day type certificate requirements, or an AD.
C - The equipment is not required by FAR 91.205, an equipment list or KOEL, the VFR-day type certificate requirements, or an AD.
During the preflight inspection who is responsible for determining the aircraft is safe for flight? A - The owner or operator. B - The certified mechanic who performed the annual inspection. C - The pilot in command.
C - The pilot in command.
(Refer to Figure 4.) Which marking identifies the never-exceed speed? A - Upper limit of the green arc. B - Upper limit of the white arc. C - The red radial line.
C - The red radial line.
Preventative maintenance has been performed on an aircraft. What paperwork is required? A - A full detailed description of the work done must be entered in the airframe logbook. B - The date the work was completed, and the name of the person who did the work must be entered in the airframe and engine logbook. 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.
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.
(Refer to Figure 4.) Which color identifies the normal flap operating range? A - The lower limit of the white arc to the upper limit of the green arc. B - The green arc. C - The white arc.
C - The white arc.
May a pilot operate an aircraft that is not in compliance with an airworthiness directive (AD)? A - Yes, under VFR conditions only. B - Yes, ADs are only voluntary. C - Yes, if allowed by the AD.
C - Yes, if allowed by the AD.
The presence of carburetor ice in an aircraft equipped with a fixed-pitch propeller can be verified by applying carburetor heat and noting A - an increase in RPM and then a gradual decrease in RPM. B - a decrease in RPM and then a constant RPM indication. C - a decrease in RPM and then a gradual increase in RPM.
C - a decrease in RPM and then a gradual increase in RPM.
To determine the expiration date of the last annual aircraft inspection, you should refer to the A - airworthiness certificate. B - registration certificate. C - aircraft maintenance records.
C - aircraft maintenance records.
Excessively high engine temperatures, either in the air or on the ground, will A - increase fuel consumption and may increase power due to the increased heat. B - result in damage to heat-conducting hoses and warping of cylinder cooling fans. C - cause loss of power, excessive oil consumption, and possible permanent internal engine damage.
C - cause loss of power, excessive oil consumption, and possible permanent internal engine damage.
To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the A - fuel strainer drain. B - lowest point in the fuel system. C - fuel strainer drain and the fuel tank sumps.
C - fuel strainer drain and the fuel tank sumps.
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 A - a drop in oil temperature and cylinder head temperature. B - engine roughness. C - loss of RPM.
C - loss of RPM.
V(NO) is defined ass the A - normal operating range. B - never-exceed speed. C - maximum structural cruising speed.
C - maximum structural cruising speed.
Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will A - force any existing water to the top of the tank away from the fuel lines to the engine. B - prevent expansion of the fuel by eliminating airspace in the tanks. C - prevent moisture condensation by eliminating airspace in the tanks.
C - prevent moisture condensation by eliminating airspace in the tanks.
As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will A - decrease as the true airspeed decreases. B - decrease as the true airspeed increases. C - remain the same regardless of altitude.
C - remain the same regardless of altitude.
For internal cooling, reciprocating aircraft engines are especially dependent on A - a properly functioning thermostat. B - air flowing over the exhaust manifold. C - the circulation of lubricating oil.
C - the circulation of lubricating oil.
Detonation occurs in a reciprocating aircraft engine when A - the spark plugs are fouled or shorted out or the wiring is defective. B - hot spots in the combustion chamber ignite the fuel/air mixture in advance of normal ignition. C - the unburned charge in the cylinders explodes instead of burning normally.
C - the unburned charge in the cylinders explodes instead of burning normally.
If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with A - the mixture set too rich. B - higher-than-normal oil pressure. C - too much power and with the mixture set too lean.
C - too much power and with the mixture set too lean.
Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates A - calibrated altitude at field elevation. B - absolute altitude at field elevation. C - true altitude at field elevation.
C - true altitude at field elevation.
