Jeppesen Private Pilot Exam Chapter 2 Questions With 100% Correct Answers 2024, Exams of Advanced Education

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Jeppesen Private Pilot Exam Chapter 2

Questions With 100% Correct Answers

A. Identify the major components of the airplane that are depicted in the accompanying illustration. - Correct Answer-- Fuselage

• Wings
• powerplant
• empennage -landing gear A. What is the primary difference between monocoque and semi-monocoque aircraft construction? - Correct Answer-The monocoque design uses the skin to support almost all imposed loads while the semi-monocoque system uses a substructure attached to the airplane's skin to maintain the shape of the airframe and increase its strength A. True/False. The rudder is located on the horizontal stabilizer. - Correct Answer-The left aileron moves up and the right aileron moves down

A. What is the purpose of trim devices? - Correct Answer-False A. What is the purpose of trim devices? - Correct Answer-Trim devices aerodynamically help move a control surface, or maintain the surface in a desired position A. An airplane with a wheel mounted on the tail is equipped with what type of landing gear? - Correct Answer- Conventional landing gear A. In addition to providing power to turn the propeller, what other functions does the engine in a typical training airplane perform? - Correct Answer-Accessories mounted on, or connected to the engine generate electrical power, provide vacuum power for some of the flight instruments, and, in most single-engine airplanes, provide a source of heat for the pilot and passengers. A. Which of the following are required to be in the aircraft during all flight operations? - Correct Answer-FAA approved airplane flight manual

A. An aircraft's annual inspection was performed on June 13, this year. when is the next annual inspection due? - Correct Answer-June 30, next year A. A 100-hour inspection was due at 2202.5 hours on the tachometer. The 100-hour inspection was performed at 2209.5 hours. When is the next 100-hour inspection due? - Correct Answer-2302.5 hours A. You discover inoperative equipment on an airplane that you are planning to fly. What four requirements must you check to determine if the equipment must be operational for this flight? - Correct Answer--The VFR-day type certificate requirements prescribed in the airworthiness certification regulations

• FAR 91.205 for the specific kind of flight operation or by other flight rules for the specific kind of flight to be conducted
• The aircraft's equipment list or the kinds of operations equipment list
• an airworthiness directive B. Identify the four-stroke operating cycle step - Correct Answer-- power

• intake
• exhaust
• compression B. As an airplane climbs, doe you enrich or lean the mixture to maintain an optimum fuel/air ratio - Correct Answer-lean the mixture as the airplane climbs B. What is your first indication of carburetor ice in an airplane equipped with a fixed-pitch propeller? - Correct Answer-The first indication for carburetor icing in an airplane with a fixed- pitch propeller is a decrease in engine RPM. B. Explain why an engine equipped with a fuel injection system is less susceptible to induction icing than one equipped with a float-type carburetor - Correct Answer-A sharp temperature drop occurs in a float-type carburetor due to fuel vaporization and decreasing air pressure in the venturi. If water vapor in the air condenses when the carburetor temperature is at or below freezing, ice can form. Because fuel injection systems eliminate fuel vaporization in a venturi and introduce the fuel directly into the hot engine cylinders, they are relatively free from the formation of induction icing.

B. What is a magneto - Correct Answer-A magneto is a self- contained, engine-driven unit that supplies electrical current to the spark plugs. It uses a permanent magnet to generate an electrical current completely independent of the aircraft's electrical system B. The uncontrolled, explosive ignition of the fuel/air mixture within the cylinder's combustion chamber describes which type of abnormal combustion? what actions can you take while airborne to help correct for this problem? - Correct Answer-detonation. Because detonation can occur when the engine overheats, if you suspect detonation while in flight you should attempt to lower the cylinder temperature. Methods include reducing power, enriching the fuel mixture, and lowering the nose to increase airspeed and cooling airflow around the engine. B. give a statement regarding fuel systems - Correct Answer-A fuel-pump system is used in airplanes with fuel injection systems to provide sufficient pressure to the injector nozzles. B. True/False. If the fuel grade specified for your airplane is not available, you can use a higher grade of fuel. - Correct Answer-True

B. Describe at least two functions performed by the engine oil system - Correct Answer-The engine oil system performs many functions including lubrication the engine's moving parts, cooling the engine by reducing friction and removing some of the heat from the cylinders, providing a seal between the cylinder walls and pistons, and carrying away contaminants, which are removed as the oil passes through a filter. B. If a constant=speed propeller is set to a high RPM, will the blade pitch be high or low? - Correct Answer-Low B. True/ False. To prevent internal engine damage in airplane equipped with a constant-speed propeller, you should avoid low RPM settings with a high manifold pressure setting. - Correct Answer-True B. Immediately after engine start you notice that the ammeter shows a discharge. Is this normal? Why or why not? - Correct Answer-No. the ammeter should initially show a charge because the battery power used to start the engine is being replace. C. What is the atmospheric pressure and temperature at sea level in a standard atmosphere? - Correct Answer-Standard

atmospheric pressure and temperature at sea level equals 29.92 in Hg and 15C, respectively. C. Pitot pressure is used by which flight instrument? - Correct Answer-the airspeed indicator is the only instrument which uses pitot pressure C. Referring to the airspeed indicator below, identify the V- speeds associated with the colored arcs - Correct Answer-The V-speeds are -Vso -Vs -Vfe -Vno -Vne C. Which important airspeed limitation changes with aircraft weight and is not depicted on the airspeed indicator? - Correct Answer-Maneuvering speed (Va) C. what is pressure altitude - Correct Answer-The vertical distance above the standard datum plane

C. what is density altitude - Correct Answer-Pressure altitude corrected for non-standard temperature C. what is true altitude - Correct Answer-The actual height of an object above mean sea level C. what is absolute altitude - Correct Answer-The height of the airplane above the earth's surface C. you fly from an area of high pressure to an area of low pressure but do not reset your altimeter. If you maintain a consistent indicated altitude, will you be at your desired altitude? why? - Correct Answer-No. If you fly from an area of high pressure to an area of low pressure without resetting your altimeter, the altimeter will sense the decrease in pressure as an increase in altitude. The altitude indicated on the altimeter will be higher than the true altitude of the airplane. C. What will the effect be on the airspeed indicator if the static system becomes clogged, but the pitot system remains unobstructed? why? - Correct Answer-At altitudes above the point where the static ports become clogged, the airspeed

indicator will indicate slower than actual because the trapped static pressure is higher than normal for the altitude. At altitudes lower than the point where the static ports became clogged, the airspeed will indicate faster than actual since the trapped static pressure is lower than normal for that altitude. C. What type of movement is shown by the attitude indicator, but not by the turn coordinator? - Correct Answer-pitch C. True/False. If you accelerate an airplane in the northern hemisphere on a heading of east, your compass will indicate a turn to the south. - Correct Answer-False C. Describe the function of the AHRS. - Correct Answer-To provide attitude, heading, rate of turn, and slip/skid information, integrated flight displays use an attitude and heading reference system. The AHRS uses inertial sensors such as electronic gyroscopes and accelerometers to determine the aircraft's attitude relative to the horizon. An electronic magnetometer provides magnetic heading data C. Select the true statement regarding the digital attitude indicator. - Correct Answer-In a slip, the trapezoid of the

slip/skid indicator located beneath the roll pointer moves to the inside of the turn C. What information is provided by the trend vector on the HSI? - Correct Answer-The end of the trend vector shows what the airplane's heading will be in six seconds if the turn continues at the same rate. Index marks 18 degrees either side of center on the turn-rate indicator provide a reference for standard-rate turns C. If the AHRS detects a problem with the integrity of the sensor information, what occurs? - Correct Answer-A red X is placed over the display of the affected instrument C. Select the true statement about the ADC. - Correct Answer- The pitot tube, static source, and outside air temperature probe provide information to the ADC C. What is true about the indications on the altimeter? - Correct Answer-in six seconds, the airplane will reach an altitude of 8,500 feet MSL if it continues to climb at the same rate

C. Describe how the integrated flight display system compensates for a PFD screen failure. - Correct Answer-the integrated flight display is configured so that the functions of the PFD can be transferred to the MFD screen, and vice versa. If the PFD screen turns black, the PFD display should automatically switch to the MFD in reversionary mode. In the event that the PFD does not appear on the MFD, most systems enable you to manually switch to reversionary mode C. True/False. An enhanced flight vision system can be displayed on a PFD - Correct Answer-False