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Embry-Riddle Aeronautical University: AS 221 Instrument Rating Ground School - Gleim | Gleim IP tests, Exams 1-4 | Answered 100% latest 2026/2027 | A+ Solutions.

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AS 221 Instrument Rating Ground School - Gleim Test 1 ( IP02:5.1-5.5;5.14-5.15, IP03:1.1-1.3, IP04:1.4-1.9, IP05:7ALL, IP06:SU2 all) Gleim IP 02: 5.1 -5.7 ; 5.14 -5.15 Gleim IP 03: 1.1 -1.3 (Test 1) When an altimeter is changed from 30.11" Hg to 29.96" Hg, in which direction will the indicated altitude change and by what value?  A.Altimeter will indicate 150 feet lower.  B.Altimeter will indicate 15 feet lower.  C.Altimeter will indicate 150 feet higher. Below 18,000 feet pressure altitude may be obtained by  A.setting the altimeter to 29.92 inches Hg.  B.requesting the current pressure altitude for the area.  C.setting the altimeter to the local altimeter setting. During a constant-rate climb in IMC above the freezing level, you notice that both the airspeed and altitude are increasing. This indicates the  A.gyroscopic instruments have failed.  B.aircraft is in an unusual attitude.  C.pitot static system has malfunctioned. If you are departing from an airport where you cannot obtain an altimeter setting, you should set your altimeter  A.on 29.92 inches Hg.  B.on the current airport barometric pressure, if known.  C.to the airport elevation. On what headings will the magnetic compass read most accurately during a level 360° turn, with a bank of approximately 15°?  A.135° through 225°.  B.180° and 0°.  C.90° and 270°. If the pitot tube ram air pressure hole and drain hole become obstructed, the airspeed indicator will operate  A.like a very sluggish airspeed indicator lagging all the changes by minutes.  B.normally due to the static port pressure changes.  C.like an altimeter as the aircraft climbs and descends. If you are not able to obtain the current altimeter setting prior to takeoff, you should set this instrument to  A.field elevation.  B.29.92 inches Hg.  C.pressure altitude. The local altimeter setting should be used by all pilots in a particular area, primarily to provide for  A.better vertical separation of aircraft.  B.the cancellation of altimeter error due to nonstandard temperatures aloft.  C.more accurate terrain clearance in mountainous areas. If both the ram air input and the drain hole of the pitot system are blocked, what reaction should you observe on the airspeed indicator when power is applied and a climb is initiated out of severe icing conditions?  A.The airspeed would drop to, and remain at, zero.  B.The indicated airspeed would show a continuous deceleration while climbing.  C.No change until an actual climb rate is established, then indicated airspeed will increase. If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following should the pilot expect?  A.The vertical speed to momentarily show a descent.  B.The vertical speed to show a climb.  C.The altimeter to read higher than normal. You are preflighting for an IFR flight and set in the current altimeter setting, it should be not more than  A.±100 feet from your referenced level.  B.±150 feet from your referenced level.  C.±75 feet from your referenced level. On the taxi check, the magnetic compass should  A.exhibit the same number of degrees of dip as the latitude.  B.swing opposite to the direction of turn when turning from north.  C.swing freely and indicate known headings. How should you preflight check the altimeter prior to an IFR flight?  A.Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude should correspond to the change in setting.  B.Set the altimeter to the current altimeter setting. The indication should be within 75 feet of theactual elevation for acceptable accuracy.  C.Set the altimeter to the current temperature. With current temperature and the altimeter indication, determine the calibrated altitude to compare with the field elevation. When initiating a left turn in the Northern Hemisphere from a heading of 270°. The magnetic compass will  A.lag behind the actual rate of turn.  B.initially indicate a turn in the opposite direction.  C.initially indicate the actual rate of turn. If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following variations in instrument indications should the pilot expect?  A.The altimeter will read lower than normal, airspeed lower than normal, and the VSI will momentarily show a descent.  B.The altimeter will read higher than normal, airspeed greater than normal, and the VSI will momentarily show a climb.  C.The altimeter will read lower than normal, airspeed greater than normal, and the VSI will momentarily show a climb and then a descent. What CAS must be used to maintain the filed TAS of 158 kt. at the flight planned altitude of 8,000 ft.? (Temperature 0°C.)  A.140 KCAS.  B.153 KCAS.  C.147 KCAS. What is the procedure for setting the altimeter when assigned an IFR altitude of 18,000 feet or higher on a direct flight off airways?  A.Set the altimeter to 29.92" Hg before takeoff.  B.Set the altimeter to the current altimeter setting until reaching the assigned altitude, then set to 29.92" Hg.  C.Set the altimeter to the current reported setting for climb-out and 29.92" Hg upon reaching 18,000 feet. At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42" Hg. The pressure altitude would be approximately  A.6,500 feet.  B.7,500 feet.  C.6,000 feet. What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a westerly heading in the Northern Hemisphere?  A.The compass will remain on a westerly heading for a short time, then gradually catch up to the actual heading of the aircraft.  B.The compass will initially show a turn in the opposite direction, then turn to a northerly indication but lagging behind the actual heading of the aircraft.  C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. Which altitude is indicated when the altimeter is set to 29.92" Hg?  A.Density.  B.Pressure.  C.Standard. While flying at an altitude of 8,000 ft., what CAS must be used to maintain a TAS of 155 kt. if the outside air temperature is –5°C?  A.142 KCAS.  B.134 KCAS.  C.139 KCAS. During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be affected?  A.The airspeed indicator, altimeter, and Vertical Speed Indicator.  B.The airspeed indicator only.  C.The airspeed indicator and the altimeter. Under what condition is pressure altitude and density altitude the same value?  A.At standard temperature.  B.When indicated, and pressure altitudes are the same value on the altimeter.  C.When the altimeter setting is 29.92" Hg. Under which condition will pressure altitude be equal to true altitude?  A.When the atmospheric pressure is 29.92" Hg.  B.When standard atmospheric conditions exist.  C.When indicated altitude is equal to the pressure altitude. The pressure altitude at a given location is indicated on the altimeter after the altimeter is set to  A.29.92" Hg.  B.the current altimeter setting.  C.the field elevation.If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following should the pilot expect?  A.The altimeter and airspeed indicator to become inoperative.  B.The gyroscopic instruments to become inoperative.  C.The vertical speed to momentarily show a climb. Pressure altitude is the altitude read on your altimeter when the instrument is adjusted to indicate height above  A.ground level.  B.sea level.  C.the standard datum plane. Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight attitude?  A.Increase pitch attitude, reduce power, and level wings.  B.Correct the bank attitude, raise the nose to a level attitude, and reduce power.  C.Reduce power, correct the bank attitude, and raise the nose to a level attitude. What would be the indication on the VSI during entry into a 500 FPM actual descent from level flight if the static ports were iced over?  A.The VSI pointer would remain at zero regardless of the actual rate of descent.  B.The indication would be in reverse of the actual rate of descent (500 FPM climb).  C.The initial indication would be a climb, then descent at a rate in excess of 500 FPM. If you need to use an alternate static source during level flight, you can expect to see  A.a higher indication on the altimeter.  B.a momentary descent on the VSI.  C.a lower indicated airspeed. How can you obtain the pressure altitude on flights below 18,000 feet?  A.Set your altimeter to the field elevation and read the pressure altitude from the Kollsman window.  B.Contact an ATC facility FSS and request the current pressure altitude for the area.  C.Set your altimeter to 29.92" Hg and read the pressure altitude on the instrument face. En route at FL 290, the altimeter is set correctly, but not reset to the local altimeter setting of 30.57" Hg during descent. If the field elevation is 650 feet and the altimeter is functioning properly, what is the approximate indication upon landing?  A.1,300 feet.  B.Sea level.  C.715 feet. Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92" Hg?  A.When density altitude is higher than indicated altitude.  B.In warmer than standard air temperature.  C.In colder than standard air temperature. Which condition would cause the altimeter to indicate a lower altitude than actually flown (true altitude)?  A.Air temperature lower than standard.  B.Air temperature warmer than standard.  C.Atmospheric pressure lower than standard. What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a northerly heading in the Northern Hemisphere?  A.The compass will indicate a turn to the right, but at a faster rate than is actually occurring.  B.The compass will initially indicate a turn to the left.  C.The compass will remain on north for a short time, then gradually catch up to the magnetic heading of the aircraft. What causes the northerly turning error in a magnetic compass?  A.Coriolis force at the mid-latitudes.  B.The magnetic dip characteristic.  C.Centrifugal force acting on the compass card. What CAS must be used to maintain 180 kt. TAS at the flight planned altitude of 8,000 ft. if the outside air temperature is +8°C?  A.157 KCAS.  B.163 KCAS.  C.154 KCAS. What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a west heading in the Northern Hemisphere?  A.The compass will initially indicate a turn to the right.  B.The compass will remain on west for a short time, then gradually catch up to the magnetic heading of the aircraft.  C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates  A.pressure altitude at field elevation. B.pressure altitude at sea level.  C.true altitude at field elevation. What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a north heading in the Northern Hemisphere?  A.The compass will remain on north for a short time, then gradually catch up to the magnetic heading of the aircraft.  B.The compass will indicate a turn to the left, but at a faster rate than is actually occurring.  C.The compass will initially indicate a turn to the right. While you are flying at FL 250, you hear ATC give an altimeter setting of 28.92" Hg in your area. At what pressure altitude are you flying?  A.26,000 feet.  B.24,000 feet.  C.25,000 feet. Which of the following defines the type of altitude used when maintaining FL 210?  A.Indicated.  B.Calibrated.  C.Pressure. If both the ram air input and drain hole of the pitot system become blocked, the indicated airspeed will  A.increase during a climb.  B.remain constant regardless of altitude change.  C.decrease during a climb. En route at FL 290, your altimeter is set correctly, but you fail to reset it to the local altimeter setting of 30.26 in. Hg during descent. If the field elevation is 134 feet and your altimeter is functioning properly, what will it indicate after landing?  A.100 feet MSL.  B.474 feet MSL.  C.206 feet below MSL. What should be the indication on the magnetic compass when you roll into a standard rate turn to the left from a south heading in the Northern Hemisphere?  A.The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft.  B.The compass will initially indicate a turn to the right.  C.The compass will indicate a turn to the left, but at a faster rate than is actually occurring. What should be the indication on the magnetic compass as you roll into a standard-rate turn to the left from an east heading in the Northern Hemisphere?  A.The compass will initially indicate a turn to the right.  B.The compass will remain on east for a short time, then gradually catch up to the magnetic heading of the aircraft.  C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth. You check the flight instruments while taxiing and find the vertical speed indicator (VSI) indicates a descent of 100 feet per minute. In this case, you  A.may not proceed under IFR until the instrument is corrected by an authorized instrument repairman.  B.may take off under IFR and use 100 feet descent as the zero indication.  C.may take off and proceed under IFR but only in VFR weather conditions. How can you determine the pressure altitude on an airport without a tower or FSS?  A.Set the altimeter to 29.92" Hg and read the altitude indicated.  B.Use your computer and correct the field elevation for temperature.  C.Set the altimeter to the current altimeter setting of a station within 100 miles and correct this indicated altitude with local temperature. What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere?  A.The compass will remain on south for a short time, then gradually catch up to the magnetic heading of the aircraft.  B.The compass will initially indicate a turn to the left.  C.The compass will indicate a turn to the right, but at a faster rate than is actually occurring. How does a pilot normally obtain the current altimeter setting during an IFR flight in Class E airspace below 18,000 feet?  A.The pilot should contact ARTCC at least every 100 NM and request the altimeter setting.  B.FSS’s along the route broadcast the weather information at 15 minutes past the hour.  C.ATC periodically advises the pilot of the proper altimeter setting. If a standard-rate turn is maintained, how much time would be required to turn to the right from a heading of 090° to a heading of 270°?  A.1 minute.  B.3 minutes.  C.2 minutes.What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from an easterly heading in the Northern Hemisphere?  A.The compass will initially indicate a turn to the left.  B.The compass will indicate the approximate correct magnetic heading if the roll into the turn is smooth.  C.The compass will remain on east for a short time, then gradually catch up to the magnetic heading of the aircraft. If the outside air temperature increases during a flight at constant power and at a constant indicated altitude, the true airspeed will  A.increase and true altitude will increase.  B.increase and true altitude will decrease.  C.decrease and true altitude will increase. Gleim IP 04: 1.4 -1.9 (Test 1) Prior to starting an engine, you should check the turn-and-slip indicator to determine if the  A.needle indication properly corresponds to the angle of the wings or rotors with the horizon.  B.needle is approximately centered and the tube is full of fluid.  C.ball will move freely from one end of the tube to the other when the aircraft is rocked. To maintain a standard-rate turn as the airspeed decreases, the bank angle of the airplane will need to  A.remain constant.  B.decrease.  C.increase. What indications should you observe on the turn-and-slip indicator during taxi?  A.The ball deflects opposite the turn, but the needle remains centered.  B.The needle deflects in the direction of the turn, but the ball remains centered.  C.The ball moves freely opposite the turn, and the needle deflects in the direction of the turn. Primary flight displays  A.include instruments like the attitude indicator.  B.primarily present terrain avoidance.  C.provide traffic information. You are flying an aircraft equipped with an electronic flight display and the air data computer fails. What instrument is affected?  A.Airspeed indicator.  B.Attitude indicator.  C.ADS-B in capability. What pre-takeoff check should be made of the attitude indicator in preparation for an IFR flight?  A.The miniature airplane should erect and become stable within 5 minutes.  B.The horizon bar does not vibrate during warmup.  C.The horizon bar should erect and become stable within 5 minutes. What indication should be observed on a turn coordinator during a right turn while taxiing?  A.The miniature aircraft will show a turn to the left and the ball remains centered.  B.Both the miniature aircraft and the ball will remain centered.  C.The miniature aircraft will show a turn to the right and the ball moves to the left. In a Technologically Advanced Aircraft, the pilot sees the flight instruments on what?  A.MFD.  B.PFD.  C.AHRS. Which practical test should be made on the electric gyro instruments prior to starting an engine?  A.Check that the electrical connections are secure on the back of the instruments.  B.Check that the attitude of the miniature aircraft is wings level before turning on electrical power.  C.Turn on the electrical power and listen for any unusual or irregular mechanical noise. If a 180° steep turn is made to the right and the aircraft is rolled out to straight-and-level flight by visual references, the attitude indicator  A.should immediately show straight-and-level flight.  B.show a slight skid and climb to the right.  C.may show a slight climb and turn. During normal coordinated turns, what error due to precession should you observe when rolling out to straight-and-level flight from a 180° steep turn to the right?  A.A straight-and-level coordinated flight indication.  B.The miniature aircraft would show a slight descent and wings-level attitude.  C.The miniature aircraft would show a slight turn indication to the left. Which display combines instruments such as an altimeter, attitude indicator, and vertical speed indicator onto one given screen?  A.Multi-function display.  B.Primary flight display.  C.Glass cockpit display.During normal flight with a vacuum driven attitude indicator, control pressures normally should not move the horizon bar more than  A.One-half bar width, with not more than an additional one bar width for normal flight deviations.  B.One bar width, with not more than an additional one bar width for normal flight deviations.  C.One-half bar width, with not more than an additional one-half bar width for normal flight deviations. When an aircraft is accelerated, some attitude indicators will precess and incorrectly indicate a  A.right turn.  B.climb.  C.descent. Which is true of glass panel displays?  A.They require less frequent training.  B.They give less reliable information to the pilot than traditional instruments.  C.They enhance situational awareness. The primary flight display (PFD) receives attitude and heading data from the  A.vacuum system.  B.AHRS.  C.pitot-static system. In a left turn, correct control coordination is indicated by  A.The ball of the turn coordinator to the right of center.  B.The ball of the turn coordinator to the left of center.  C.The ball of the turn coordinator in the center. What indication should be observed on a turn coordinator during a left turn while taxiing?  A.The miniature aircraft will show a turn to the left and the ball moves to the right.  B.The miniature aircraft will show a turn to the left and the ball remains centered.  C.Both the miniature aircraft and the ball will remain centered. When a pilot believes advanced avionics enable operations closer to personal or environmental limits,  A.risk is increased.  B.greater utilization of the aircraft is achieved.  C.risk is decreased. During coordinated turns, which force moves the pendulous vanes of a vacuum-driven attitude indicator resulting in precession of the gyro toward the inside of the turn?  A.Deceleration.  B.Acceleration.  C.Centrifugal. To maintain a standard rate turn as the airspeed increases, the bank angle of the aircraft will need to  A.increase.  B.decrease.  C.remain constant. Errors in both pitch and bank indication on an attitude indicator are usually at a maximum as the aircraft rolls out of a  A.180° turn.  B.270° turn.  C.360° turn. What does the miniature aircraft of the turn coordinator display?  A.Initially rate of bank and then directly rate of turn.  B.Indirectly bank angle and indirectly rate of turn.  C.Directly bank angle and then directly rate of turn. Which condition during taxi is an indication that an attitude indicator is unreliable?  A.The horizon bar does not align itself with the miniature airplane after warmup.  B.The horizon bar tilts more than 5° while making taxi turns.  C.The horizon bar vibrates during warmup. What does the miniature aircraft of the turn coordinator directly display?  A.Angle of bank and rate of turn.  B.Rate of roll and rate of turn.  C.Angle of bank. The displacement of a turn coordinator during a coordinated turn will  A.increase as angle of bank increases.  B.remain constant for a given bank regardless of airspeed.  C.indicate the angle of bank. During normal operation of a vacuum-driven attitude indicator, what attitude indication should you see when rolling out from a 180° skidding turn to straight-and-level coordinated flight?  A.A straight-and-level coordinated flight indication.  B.The miniature aircraft shows a turn in the direction opposite the skid.  C.A nose-high indication relative to level flight. The advancement of avionics in light general aviation airplanes has enhanced situational awareness for properly trained pilots. However, there is concern that this technology could lead to A.resignation.  B.fatigue.  C.complacency. What pre-takeoff check should be made of a vacuum-driven heading indicator in preparation for an IFR flight?  A.After 5 minutes, check that the heading indicator card aligns itself with the magnetic heading of the aircraft.  B.After 5 minutes, set the indicator to the magnetic heading of the aircraft and check for proper alignment after taxi turns.  C.Determine that the heading indicator does not precess more than 2° in 5 minutes of ground operation. What indication is presented by the miniature aircraft of the turn coordinator?  A.Indirect indication of the bank attitude.  B.Quality of the turn.  C.Direct indication of the bank attitude and the quality of the turn. What indications are displayed by the miniature aircraft of a turn coordinator?  A.Indirect indication of bank angle and pitch attitude.  B.Rate of roll and rate of turn.  C.Direct indication of bank angle and pitch attitude. Risk is increased when flightcrew members  A.allocate time to verify expected performance of automated systems.  B.question the performance of each other’s duties.  C.fail to monitor automated navigation systems. The lighter workloads associated with glass panel flight deck instrumentation  A.may lead to complacency by the flightcrew.  B.are instrumental in decreasing flightcrew fatigue.  C.have proven to increase safety in operations. The “No Entry” sign identifies  A.an area that does not continue beyond intersection.  B.the exit boundary for the runway protected area.  C.paved area where aircraft entry is prohibited. When an aircraft is decelerated, some attitude indicators will precess and incorrectly indicate a  A.descent.  B.climb.  C.left turn. Automation in aircraft has proven to  A.show that automation is basically flawless.  B.prevent accidents.  C.present new hazards in its limitations. One characteristic that a properly functioning gyro depends upon for operation is the  A.deflecting force developed from the angular velocity of the spinning wheel.  B.ability to resist precession 90° to any applied force.  C.resistance to deflection of the spinning wheel or disc. An aircraft which is equipped with an Electronic Flight Display (EFD) can  A.compensate for a pilot’s lack of skill or knowledge.  B.offer new capabilities and simplify the basic flying task.  C.improve flight awareness by allowing the pilot to simply watch for alerts. Exam 1 – All Units The vertical extent of the Class A airspace extends from  A.18,000 feet to and including FL 450.  B.18,000 feet to and including FL 600.  C.12,500 feet to and including FL 600. Abrupt head movement during a prolonged constant rate turn in IMC or simulated instrument conditions can cause  A.elevator illusion.  B.false horizon.  C.pilot disorientation. Abrupt head movement during a prolonged constant rate turn in IMC or simulated instrument conditions can cause  A.elevator illusion.  B.Coriolis illusion.  C.inversion illusion. What is the flight attitude? One instrument has malfunctioned. (Figure 150)  A.Descending turn to the right.  B.Climbing turn to the right.  C.Climbing turn to the left. Displacement of the standard rate turn index during a coordinated turn will A.increase as rate of turn increases.  B.indicate the angle of bank.  C.remain constant for a given bank regardless of airspeed. What effect does haze have on the ability to see traffic or terrain features during flight?  A.Haze causes the eyes to focus at infinity, making terrain features harder to see.  B.Haze creates the illusion of being a greater distance than actual from the runway, and causes pilots to fly a lower approach.  C.The eyes tend to overwork in haze and do not detect relative movement easily. If a half-standard-rate turn is maintained, how much time would be required to turn clockwise from a heading of 090° to a heading of 180°?  A.1 minute.  B.30 seconds.  C.1 minute 30 seconds. Enhanced taxiway centerline markings are enhanced for a maximum of how many feet prior to the runway holding position markings?  A.150  B.100  C.50 As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using  A.two bar widths on the attitude indicator.  B.less than a half bar width on the attitude indicator.  C.less than a full bar width on the attitude indicator. If an airplane is in an unusual flight attitude and the attitude indicator has exceeded its limits, which instruments should be relied on to determine pitch attitude before starting recovery?  A.VSI and airspeed to detect approaching VSI or VMO.  B.Airspeed and altimeter.  C.Turn indicator and VSI. What minimum aircraft equipment is required for operation within Class C airspace?  A.Two-way communications, a Mode C transponder, and ADS-B Out equipment.  B.Transponder, ADS-B Out equipment, and DME.  C.Two-way communications. What night operations, if any, are authorized between the approach end of the runway and the threshold lights? (Figure 138)  A.Taxi and takeoff operations are permitted, providing the takeoff operations are toward the visible green threshold lights.  B.Only taxi operations are permitted in the area short of the threshold lights.  C.No aircraft operations are permitted short of the threshold lights. Having appropriate instrument lighting will  A.make a proper instrument scan difficult.  B.enable better recognition of outside references.  C.result in unnecessary eye strain. If severe turbulence is encountered during your IFR flight, the airplane should be slowed to the design maneuvering speed because the  A.maneuverability of the airplane will be increased.  B.amount of excess load that can be imposed on the wing will be decreased.  C.airplane will stall at a lower angle of attack, giving an increased margin of safety. To level off from a descent maintaining the descending airspeed, the pilot should lead the desired altitude by approximately  A.60 feet.  B.50 feet.  C.20 feet. When is an IFR clearance required during VFR weather conditions?  A.When operating in the Class E airspace.  B.When operating in airspace above 14,500 feet.  C.When operating in a Class A airspace. If a standard-rate turn is maintained, how long would it take to turn 180°?  A.3 minutes.  B.2 minutes.  C.1 minute. During a skidding turn to the right, what is the relationship between the component of lift, centrifugal force, and load factor?  A.Centrifugal force is greater than horizontal lift and the load factor is increased.  B.Centrifugal force is less than horizontal lift and the load factor is increased.  C.Centrifugal force and horizontal lift are equal and the load factor is decreased. MOAs are established to  A.separate certain military activities from IFR traffic.  B.prohibit all civil aircraft because of hazardous or secret activities. C.restrict civil aircraft during periods of high-density training activities. The sensory system responsible for most of the illusions leading to spatial disorientation is the  A.visual system.  B.vestibular system.  C.postural system. Which statement is correct regarding the use of flight deck lighting for night flight?  A.Coloration shown on maps is least affected by the use of direct red lighting.  B.The use of regular white light, such as a flashlight, will impair night adaptation.  C.Reducing the lighting intensity to a minimum level will eliminate blind spots. Why is fatigue hazardous to flight safety?  A.The pilot is lazy and rushes to get done quickly.  B.The pilot hurries to get done in order to rest.  C.Fatigue may not be apparent to a pilot until serious errors are made (an impaired pilot is a dangerous pilot). Which runway marking indicates a displaced threshold on an instrument runway?  A.Centerline dashes starting at the threshold.  B.Red chevron marks in the nonlanding portion of the runway.  C.Arrows leading to the threshold mark. While recovering from an unusual flight attitude without the aid of the attitude indicator, approximate level pitch attitude is reached when the  A.airspeed arrives at cruising speed, the altimeter reverses its trend, and the vertical speed stops its movement.  B.airspeed and altimeter stop their movement and the VSI reverses its trend.  C.altimeter and vertical speed reverse their trend and the airspeed stops its movement. To enter a constant-airspeed descent from level-cruising flight, and maintain cruising airspeed, the pilot should  A.first adjust the pitch attitude to a descent using the attitude indicator as a reference, then adjust the power to maintain the cruising airspeed.  B.first reduce power, then adjust the pitch using the attitude indicator as a reference to establish a specific rate on the VSI.  C.simultaneously reduce power and adjust the pitch using the attitude indicator as a reference to maintain the cruising airspeed. If you experience tunnel vision and cyanosis, you may have symptoms of  A.hypoxia.  B.hyperventilation.  C.carbon monoxide poisoning. When lined up for takeoff on runway 18, the compass and heading indicator should display a heading of about (Figure 251)  A.175°  B.185°  C.180° When lined up for takeoff on RWY 27, the compass and heading indicator should display a heading of about (Figure 251)  A.265°  B.275°  C.270° What is the slope of RWY 9? (Figure 251)  A.0.4% down.  B.0.3% down.  C.0.4% up. What is the actual heading of runway 36 at Oshkosh/Wittman Regional (OSH) airport? (Figure 251)  A.003.6°  B.0.3%  C.360° When lined up for takeoff on runway 4, the compass and heading indicator should read a heading of about (Figure 251)  A.055°  B.050°  C.040° Under what conditions might a pilot expect the possibility of hydroplaning?  A.When departing a grooved runway with less than a thousandth of an inch of water.  B.When the adiabatic lapse rate is high, and steam is rising from the landing surface.  C.When landing on a wet runway that is covered in rubber from previous landings. Which instruments should be used to make a pitch correction when you have deviated from your assigned altitude?  A.Attitude indicator, altimeter, and VSI.  B.Altimeter and VSI. C.Manifold pressure gauge and VSI. With winds reported as from 330° at 4 knots, you are given instructions to taxi to runway 4 for departure and to expect takeoff after an airliner departs from runway 29. What effect would you expect from that airliner’s vortices? (Figure 158)  A.The upwind vortex would tend to remain over the runway.  B.The downwind vortex will rapidly dissipate.  C.The winds will push the vortices southeast of your takeoff path. The primary reason the pitch attitude must be increased, to maintain a constant altitude during a coordinated turn, is because the  A.use of pedals has increased the drag.  B.vertical component of lift has decreased as the result of the bank.  C.thrust is acting in a different direction, causing a reduction in airspeed and loss of lift. When airspeed is decreased in a turn, what must be done to maintain level flight?  A.Increase the angle of bank and/or decrease the angle of attack.  B.Decrease the angle of bank and/or increase the angle of attack.  C.Increase the angle of attack. If a half-standard-rate turn is maintained, how long would it take to turn 135°?  A.1 minute 30 seconds.  B.1 minute.  C.1 minute 20 seconds. When is a pilot on an IFR flight plan responsible for avoiding other aircraft?  A.At all times when not in radar contact with ATC.  B.Only when advised by ATC.  The best way to counter the effects of spatial disorientation is toC.When weather conditions permit, regardless of whether operating under IFR or VFR. The best way to counter the effects of spatial disorientation is to  A.breathe deeply and exhale slowly to increase your oxygen content.  B.trust your flight instruments and disregard your sensory perceptions.  C.disregard your flight instruments and rely on your senses. To preserve night vision, the most appropriate flight deck lighting is  A.the use of regular white light, such as a flashlight, will not impair night adaptation.  B.increase the interior intensity to slightly above the outside level.  C.reducing the interior lighting intensity to a minimum level. How can an instrument pilot best overcome spatial disorientation?  A.Rely on kinesthetic sense.  B.Read and interpret the flight instruments, and act accordingly.  C.Use a very rapid cross-check. The middle and far bars of a 3-bar VASI will  A.both appear white to the pilot when on the upper glidepath.  B.constitute a 2-bar VASI for using the upper glidepath.  C.constitute a 2-bar VASI for using the lower glidepath. How can an instrument pilot best overcome spatial disorientation?  A.Properly interpret the flight instruments and act accordingly.  B.Use a very rapid cross-check.  C.Avoid banking in excess of 30°. In addition to a VOR receiver and two-way communications capability, which additional equipment is required for IFR operation in Class B airspace?  A.An operable coded transponder having Mode C capability and ADS-B Out equipment.  B.DME, an operable coded transponder having Mode C capability, and ADS-B Out equipment.  C.Standby communications receiver, DME, and coded transponder. Which is not a type of hypoxia?  A.Hypoxic.  B.Histotoxic.  C.Hypertoxic. Carbon monoxide poisoning, common in flying as a result of an exhaust leak, is considered what type of hypoxia?  A.Anemic.  B.Hypoxic.  C.Histotoxic. What force causes an airplane to turn?  A.Rudder pressure or force around the vertical axis.  B.Horizontal lift component.  C.Vertical lift component. What is the correct sequence in which to use the three skills used in instrument flying?  A.Instrument interpretation, cross-check, and aircraft control.  B.Aircraft control, cross-check, and instrument interpretation.  C.Cross-check, instrument interpretation, and aircraft control.Your transponder is inoperative. What are the requirements for flying in Class D airspace?  A.Pilot must immediately request priority handling to proceed to destination.  B.Continue the flight as planned.  C.The entry into Class D is prohibited. When turning onto a taxiway from another taxiway, the “taxiway directional sign” indicates  A.designation and direction of taxiway leading out of an intersection.  B.direction to the take-off runway.  C.designation and direction of exit taxiway from runway. What is the first fundamental skill in attitude instrument flying?  A.Aircraft control.  B.Instrument interpretation.  C.Instrument cross-check. When airspeed is increased in a turn, what must be done to maintain a constant altitude?  A.Decrease the angle of bank.  B.Decrease the angle of attack.  C.Increase the angle of bank and/or decrease the angle of attack. Which sign indicates you’re holding short of the ILS critical area? (Figure 254)  A.Bottom yellow.  B.Middle yellow.  C.Top red. Which of the signs in the figure is a mandatory instruction sign? (Figure 254)  A.Bottom yellow.  B.Top red.  C.Middle yellow. While clearing an active runway, you are clear of the ILS critical area when you pass which sign? (Figure 254)  A.Top red.  B.Middle yellow.  C.Bottom yellow. Altitude-induced hypoxia is caused by what atmospheric condition?  A.Insufficient partial pressure of the inhaled oxygen.  B.Significantly less oxygen molecules at high altitude.  C.Incorrect balance of oxygen and carbon dioxide. Within aircraft movement areas, “destination signs” identify the  A.entrance to the runway from a taxiway.  B.runway on which an aircraft is located.  C.direction to the takeoff runway. While making prolonged constant-rate turns under IFR conditions, an abrupt head movement can create the illusion of rotation on an entirely different axis. This is known as  A.the leans.  B.autokinesis.  C.Coriolis illusion. What is the minimum in-flight visibility and distance from clouds required for a VFR-on-Top flight at 9,500 feet MSL (above 1,200 feet AGL) during daylight hours?  A.3 miles; above 1,000 feet; horizontal 2,000 feet; below 500 feet.  B.2,000 feet; above 1,000 feet; horizontal 2,000 feet; below 500 feet.  C.5 miles; above 1,000 feet; horizontal 2,000 feet; below 500 feet. A runway exit sign  A.points toward a named taxiway that leads off the runway.  B.shows the direction to exit from a named taxiway onto a runway.  C.designates an intersection of two or more runways. Class G airspace is that airspace where  A.ATC controls only IFR flights.  B.the minimum visibility for VFR flight is 3 miles.  C.ATC does not control air traffic. A corrective action to overcome symptoms of hyperventilation is to  A.lower altitude immediately.  B.slow the breathing rate.  C.take quick, deep breaths. What is the flight attitude? One system which transmits information to the instruments has malfunctioned. (Figure 148)  A.Climbing turn to right.  B.Level turn to left.  C.Climbing turn to left. What is the correct sequence for recovery from the unusual attitude indicated? (Figure 145)  A.Level the wings, raise the nose of the aircraft to level flight attitude, and obtain desired airspeed.  B.Reduce power, increase back elevator pressure, and level the wings. C.Reduce power, level the wings, bring pitch attitude to level flight. Which technique should a pilot use to scan for traffic to the right and left during straight-and-level flight?  A.Systematically focus on different segments of the sky for short intervals.  B.Continuous sweeping of the windshield from right to left.  C.Concentrate on relative movement detected in the peripheral vision area. What is the best method of speed reduction if hydroplaning is experienced on landing?  A.Go around.  B.Step hard on the brakes.  C.Hold nose up. What is the best method of speed reduction if hydroplaning is experienced on landing?  A.Apply aerodynamic braking to the fullest advantage.  B.Apply full main wheel braking only.  C.Apply nosewheel and main wheel braking alternately and abruptly. The primary purpose of runway end identifier lights, installed at many airfields, is to provide  A.rapid identification of the approach end of the runway during reduced visibility.  B.rapid identification of the primary runway during reduced visibility.  C.a warning of the final 3,000 feet of runway remaining as viewed from the takeoff or approach position. For maintaining level flight at constant thrust, which instrument would be the least appropriate for determining the need for a pitch change?  A.VSI.  B.Altimeter.  C.Attitude indicator. Anemic (hypemic) hypoxia has the same symptoms as hypoxic hypoxia, but it is most often a result of  A.use of alcohol or drugs before flight.  B.poor blood circulation.  C.a leaking exhaust manifold. Wake turbulence is near maximum behind a jet transport just after takeoff because  A.of the high angle of attack and high gross weight.  B.the gear and flap configuration increases the turbulence to maximum.  C.the engines are at maximum thrust output at slow airspeed. What effect, if any, will landing at a higher-than-recommended touchdown speed have on hydroplaning?  A.Reduces hydroplaning potential if heavy braking is applied.  B.Increases hydroplaning potential regardless of braking.  C.No effect on hydroplaning, but increases landing roll. Which types of airspace are depicted on the En Route Low Altitude Chart?  A.Class A, special use airspace, Class D, and Class E.  B.Special use airspace, Class E, Class D, Class A, Class B, and Class C.  C.Limits of controlled airspace, military training routes, and special use airspace. Which illustration indicates a skidding turn? (Figure 144)  A.3  B.2  C.1 Which illustration indicates a slipping turn? (Figure 144)  A.2  B.3  C.1 What information is shown on turn coordinator #3? (Figure 144)  A.A standard rate, skidding turn to the left.  B.A half standard rate, coordinated turn to the left.  C.A standard rate, slipping turn to the right. What changes in control displacement should be made so that “2” would result in a coordinated standard-rate turn? (Figure 144)  A.Increase left rudder and increase rate of turn.  B.Decrease left rudder and decrease angle of bank.  C.Increase left rudder and decrease rate of turn. What changes in control displacement should be made so that “1” would result in a coordinated standard rate turn? (Figure 144)  A.Decrease right rudder and increase angle of bank.  B.Increase right rudder and decrease rate of turn.  C.Increase right rudder and increase rate of turn. Identify the system that has failed and determine a corrective action to return the airplane to straight-andlevel flight. (Figure 146)  A.Static/pitot system is blocked; lower the nose and level the wings to level-flight attitude by use of attitude indicator.  B.Vacuum system has failed; reduce power, roll left to level wings, and pitchup to reduce airspeed. C.Electrical system has failed; reduce power, roll left to level wings, and raise the nose to reduce airspeed. Which is the correct sequence for recovery from the unusual attitude indicated? (Figure 147)  A.Add power, lower nose, level wings, return to original attitude and heading.  B.Level wings, add power, lower nose, descend to original attitude, and heading.  C.Stop turn by raising right wing and add power at the same time, lower the nose, and return to original attitude and heading. The sensations which lead to spatial disorientation during instrument flight conditions  A.occur, in most instances, during the initial period of transition from visual to instrument flight.  B.are frequently encountered by beginning instrument pilots, but never by pilots with moderate instrument experience.  C.must be suppressed and complete reliance placed on the indications of the flight instruments. The purpose of an enhanced taxiway centerline is to  A.highlight an approaching runway holding position marking.  B.identify the location of taxiing aircraft during low visibility operations.  C.supplement location signs in confirming the designation of the taxiway. If a standard-rate turn is maintained, how much time would be required to turn to the left from a heading of 090° to a heading of 300°?  A.30 seconds.  B.40 seconds.  C.50 seconds. While cruising at 190 knots, you wish to establish a climb at 160 knots. When entering the climb (full panel), it would be proper to make the initial pitch change by increasing back elevator pressure until the  A.airspeed indication reaches 160 knots.  B.attitude indicator shows the approximate pitch attitude appropriate for the 160-knot climb.  C.attitude indicator, airspeed, and vertical speed indicate a climb. When on the proper glidepath of a 2-bar VASI, the pilot will see the near bar as  A.white and the far bar as white.  B.white and the far bar as red.  C.red and the far bar as white. The “runway hold position” sign denotes  A.an area protected for an aircraft approaching a runway.  B.an entrance to a taxiway from runway.  C.an entrance to a runway from a taxiway. The illusion associated with landing on a narrower than usual runway may result in the pilot flying a  A.slower approach with the risk of reducing airspeed below VSO or landing hard.  B.lower approach with the risk of striking objects along the approach path or landing short.  C.higher approach with the risk of leveling out high and landing hard or overshooting the runway. If an approach is being made to a runway that has an operating 3-bar VASI and all the VASI lights appear red as the airplane reaches the MDA, the pilot should  A.start a climb to reach the proper glidepath.  B.continue at the same rate of descent if the runway is in sight.  C.level off momentarily to intercept the proper approach path. To level off at an airspeed higher than the descent speed, the addition of power should be made, assuming a 500 FPM rate of descent, at approximately  A.100 to 150 feet above the desired altitude.  B.50 to 100 feet above the desired altitude.  C.150 to 200 feet above the desired altitude. Approximately what percent of the indicated vertical speed should be used to determine the number of feet to lead the level-off from a climb to a specific altitude?  A.25 percent.  B.10 percent.  C.20 percent. What is the minimum flight visibility and distance from clouds for flight at 10,500 feet with a VFR-on-Top clearance during daylight hours? (Class E airspace.)  A.5 SM, 1,000 feet above, 500 feet below, and 1 mile horizontal.  B.5 SM, 1,000 feet above, 1,000 feet below, and 1 mile horizontal.  C.3 SM, 1,000 feet above, 500 feet below, and 2,000 feet horizontal. Which instrument provides the most pertinent information for pitch control in straight-and-level flight?  A.Attitude indicator.  B.Altimeter.  C.Airspeed indicator. When landing behind a large jet aircraft, at which point on the runway should you plan to land?  A.If any crosswind, land on the windward side of the runway and prior to the jet’s touchdown point.  B.At least 1,000 feet beyond the jet’s touchdown point.  C.Beyond the jet’s touchdown point.What visual illusion creates the same effect as a narrower-than-usual runway?  A.An upsloping runway.  B.A downsloping runway.  C.A wider-than-usual runway. If a half-standard-rate turn is maintained, how long would it take to turn 360°?  A.2 minutes.  B.4 minutes.  C.1 minute. Which system is most likely responsible for a pilot suffering spatial disorientation?  A.Vestibular system.  B.Cardiopulmonary system.  C.Autokinesis system. An abrupt change from climb to straight-and-level flight can create the illusion of  A.tumbling backwards.  B.a descent with the wings level.  C.a noseup attitude. What in-flight visibility and distance from clouds is required for a flight at 8,500 feet MSL (above 1,200 feet AGL) in Class G airspace in VFR conditions during daylight hours?  A.3 miles; above 1,000 feet; horizontal 2,000 feet; below 500 feet.  B.5 miles; above 1,000 feet; horizontal 1 mile; below 1,000 feet.  C.1 mile; above 1,000 feet; horizontal 2,000 feet; below 500 feet. What is the minimum in-flight visibility and distance from clouds required for an airplane operating less than 1,200 feet AGL during daylight hours in Class G airspace?  A.1 mile; above 500 feet; horizontally 1,000 feet; below 500 feet.  B.3 miles; above 1,000 feet; horizontally 2,000 feet; below 500 feet.  C.1 mile; above clear of clouds; horizontally clear of clouds; below clear of clouds. If you fly into severe turbulence, which flight condition should you attempt to maintain?  A.Level flight attitude.  B.Constant altitude and constant airspeed.  C.Constant airspeed (VA). Which instrument indicates the quality of a turn?  A.Attitude indicator.  B.Ball of the turn coordinator.  C.Heading indicator or magnetic compass. What is the distance (C) from the beginning of the touchdown zone marker to the beginning of the fixed distance marker? (Figure 137)  A.250 feet.  B.500 feet.  C.1,000 feet. What is the distance (B) from the beginning of the runway to the touchdown zone marker? (Figure 137)  A.500 feet.  B.750 feet.  C.250 feet. What is the distance (A) from the beginning of the runway to the fixed distance marker?  A.1,500 feet.  B.500 feet.  C.1,000 feet. Conditions that determine pitch attitude required to maintain level flight are  A.airspeed, air density, wing design, and angle of attack.  B.relative wind, pressure altitude, and vertical lift component.  C.flightpath, wind velocity, and angle of attack. Which of the following indications would a pilot see while approaching to land on a runway served by a 2-bar VASI?  A.If on the glidepath, both near bars and far bars will appear white.  B.If departing to the high side of the glidepath, the far bars will change from red to white.  C.If on the glidepath, the near bars will appear red, and the far bars will appear white. Which procedure is recommended to prevent or overcome spatial disorientation?  A.Rely on the kinesthetic sense.  B.Reduce head and eye movements to the extent possible.  C.Rely on the indications of the flight instruments. Which of the following is a correct response to counteract the feelings of hypoxia in flight?  A.Increase cabin air flow.  B.Promptly descend to a lower altitude.  C.Avoid sudden inhalations. The rate of turn at any airspeed is dependent upon A.centrifugal force.  B.the horizontal lift component.  C.the vertical lift component. When is an IFR flight plan required?  A.When less than VFR conditions exist in either Class E or Class G airspace and in Class A airspace.  B.In all Class E airspace when conditions are below VFR, in Class A airspace, and in defense zone airspace.  C.In Class E airspace when IMC exists or in Class A airspace. Which of the following is required equipment for operating an aircraft within Class B airspace?  A.A 4096 code transponder with automatic pressure altitude reporting equipment.  B.A 4096 code transponder.  C.A VOR receiver with DME. What responsibility does the pilot in command of an IFR flight assume upon entering VFR conditions?  A.Obtaining an amended clearance authorizing VFR flight.  B.Seeing and avoiding other aircraft.  C.Reporting VFR conditions to ARTCC. Mandatory airport instruction signs are designated by having (Figure 94)  A.yellow lettering with a black background.  B.white lettering with a red background.  C.black lettering with a yellow background. What colors are runway holding position signs? (Figure 94)  A.Yellow with a black background.  B.Red with a white background.  C.White with a red background. What sign is designated by illustration 7? (Figure 94)  A.Direction sign.  B.Mandatory instruction sign.  C.Location sign. Hold line markings at the intersection of taxiways and runways consist of four lines that extend across the width of the taxiway. These lines are (Figure 94)  A.yellow, and the dashed lines are nearest the runway.  B.yellow, and the solid lines are nearest the runway.  C.white, and the dashed lines are nearest the runway. Flight deck lighting for night flight should include  A.using direct red lighting.  B.reducing lighting intensity to a minimum level.  C.using a white light such as a flashlight. Which is a common symptom of hyperventilation?  A.Visual acuity.  B.Decreased breathing rate.  C.Tingling sensations. A rapid acceleration during takeoff can create the illusion of  A.spinning in the opposite direction.  B.diving into the ground.  C.being in a noseup attitude. What are the vertical limits of a transition area that is designated in conjunction with an airport having a prescribed IAP?  A.1,200 feet AGL to the base of the overlying controlled airspace.  B.700 feet AGL or more to the base of the overlying controlled airspace.  C.Surface to 700 feet AGL. A flight is to be conducted in VFR-on-Top conditions at 12,500 feet MSL (above 1,200 feet AGL). What is the in-flight visibility and distance from clouds required for operation in Class E airspace during daylight hours?  A.3 miles; above 1,000 feet; horizontal 2,000 feet; below 1,000 feet.  B.5 miles; above 1,000 feet; horizontal 2,000 feet; below 500 feet.  C.5 miles; above 1,000 feet; horizontal 1 mile; below 1,000 feet. Which illustration would a pilot observe if the aircraft is less than 2.5°? (Figure 136)  A.12  B.11  C.10 Which illustration would a pilot observe if the aircraft is far below the glidepath? (Figure 136)  A.11  B.12  C.10 As you emerge from the clouds during an instrument approach and make visual contact with the runway environment, you see PAPI lights corresponding to those depicted in illustration 12. You are (Figure 136) A.on the glidepath.  B.above the glidepath.  C.below the glidepath.  Which illustration depicts a “slightly low” (2.8°) indication? (Figure 136)  A.9  B.10  C.11 An “on glidepath” indication is (Figure 136)  A.10  B.8  C.11 Which illustration would a pilot observe if the aircraft is below both glidepaths? (Figure 135)  A.4  B.6  C.5 Which illustration would a pilot observe when on the lower glidepath? (Figure 135)  A.4  B.6  C.5 Which illustration would a pilot observe if the aircraft is above both glidepaths? (Figure 135)  A.7  B.5  C.6 Without visual aid, a pilot often interprets centrifugal force as a sensation of  A.rising or falling.  B.turning.  C.motion reversal. What is expected of you as pilot on an IFR flight plan if you are descending or climbing in VFR conditions?  A.Execute gentle banks, left and right, at a frequency which permits continuous visual scanning of the airspace about you.  B.If on an airway, climb or descend to the right of the centerline.  C.Advise ATC you are in visual conditions and will remain a short distance to the right of the centerline while climbing. Due to visual illusion, when landing on a narrower-than-usual runway, the aircraft will appear to be Risk is increased when flightcrew members  A.higher than actual, leading to a higher-than-normal approach.  B.higher than actual, leading to a lower-than-normal approach.  C.lower than actual, leading to a higher-than-normal approach. What action should be taken if hyperventilation is suspected?  A.Consciously force yourself to take deep breaths and breathe at a faster rate than normal.  B.Breathe at a slower rate by taking very deep breaths.  C.Consciously breathe at a slower rate than normal. As a rule of thumb, altitude corrections of less than 100 feet should be corrected by using a  A.full bar width on the attitude indicator.  B.half bar width on the attitude indicator.  C.two bar width on the attitude indicator. What is the minimum in-flight visibility and distance from clouds required in VFR conditions above clouds at 13,500 feet MSL (above 1,200 feet AGL) in Class G airspace during daylight hours?  A.5 miles; above 1,000 feet; horizontal 1 mile; below 1,000 feet.  B.3 miles; above 1,000 feet; horizontal 1 mile; below 1,000 feet.  C.5 miles; above 1,000 feet; horizontal 2,000 feet; below 500 feet. Operation in which airspace requires filing an IFR flight plan?  A.Positive control area, Continental Control Area, and all other airspace, if the visibility is less than 1 mile.  B.Class E airspace with IMC and Class A airspace.  C.Any airspace when the visibility is less than 1 mile. Your heading indicator has failed. To turn left from a heading of 090° to a heading of 360°, using a standard rate turn, how many seconds will it take?  A.30 seconds.  B.50 seconds.  C.40 seconds. Which illustration indicates a coordinated turn? (Figure 144)  A.3  B.1  C.2 The primary reason the angle of attack must be increased, to maintain a constant altitude during acoordinated turn, is because the  A.use of ailerons has increased the drag.  B.vertical component of lift has decreased as the result of the bank.  C.thrust is acting in a different direction, causing a reduction in airspeed and loss of lift. When are you required to have an instrument rating for flight in VMC?  A.Flight into an ADIZ.  B.Flight through an MOA.  C.Flight into Class A airspace. You are most likely to experience somatogravic illusion during  A.a rapid descent.  B.rapid acceleration on takeoff.  C.deceleration upon landing. Rate of turn can be increased and radius of turn decreased by  A.decreasing airspeed and shallowing the bank.  B.decreasing airspeed and increasing the bank.  C.increasing airspeed and increasing the bank. Why is hypoxia particularly dangerous during flights with one pilot?  A.The pilot may not be able to control the aircraft even if using oxygen.  B.Symptoms of hypoxia may be difficult to recognize before the pilot’s reactions are affected.  C.Night vision may be so impaired that the pilot cannot see other aircraft. The “ILS critical area boundary” sign identifies the  A.Exit boundary for the runway protected area.  B.Area where an aircraft is prohibited from entering.  C.Edge of the ILS critical area. During recoveries from unusual attitudes, level flight is attained the instant  A.the horizon bar on the attitude indicator is exactly overlapped with the miniature airplane.  B.the altimeter and airspeed needles stop prior to reversing their direction of movement.  C.a zero rate of climb is indicated on the VSI. What is the third fundamental skill in attitude instrument flying?  A.Instrument cross-check.  B.Power control.  C.Aircraft control. When exiting the runway, what is the purpose of the runway exit sign?  A.Indicates direction to take-off runway.  B.Indicates designation and direction of taxiway leading out of an intersection.  C.Indicates designation and direction of exit taxiway from runway. What is the purpose of the runway exit sign?  A.Defines direction and designation of runway when exiting a taxiway.  B.Defines a mandatory exit point from the runway during Land and Hold Short Operations (LAHSO).  C.Defines direction and designation of exit taxiway from runway. Hyperventilation occurs when  A.there is a lack of oxygen in the bloodstream.  B.an insufficient amount of air is breathed into the lungs.  C.an excessive amount of air is breathed into the lungs. To level off from a descent to a specific altitude, the pilot should lead the level-off by approximately  A.50 percent of the vertical speed.  B.30 percent of the vertical speed.  C.10 percent of the vertical speed. What is the relationship between centrifugal force and the horizontal lift component in a coordinated turn?  A.Horizontal lift and centrifugal force are equal.  B.Centrifugal force exceeds horizontal lift.  C.Horizontal lift exceeds centrifugal force. Under which conditions is hydroplaning most likely to occur?  A.When rudder is used for directional control instead of allowing the nosewheel to contact the surface early in the landing roll on a wet runway.  B.During a landing on any wet runway when brake application is delayed until a wedge of water begins to build ahead of the tires.  C.During conditions of standing water, slush, high speed, and smooth runway texture. Which airspace is defined as a transition area when designated in conjunction with an airport which has a prescribed IAP?  A.That Class D airspace extending from the surface and terminating at the base of the continental control area.  B.The Class E airspace extending upward from 700 feet or more above the surface and terminating at the base of the overlying controlled airspace.  C.The Class C airspace extending from the surface to 700 or 1,200 feet AGL, where designated. What wind condition prolongs the hazards of wake turbulence on a landing runway for the longest period of time? A.Direct tailwind.  B.Light quartering tailwind.  C.Direct headwind. “Runway hold position” markings on the taxiway  A.identifies area where aircraft are prohibited.  B.allows an aircraft permission onto the runway.  C.identifies where aircraft hold short of the runway. Which type of runway lighting consists of a pair of synchronized flashing lights, one on each side of the runway threshold?  A.MALSR.  B.HIRL.  C.REIL. You are cleared to land on RWY 16L at Eugene Mahlon Sweet Field. As you break out of the clouds, you are lined up with the white lights down the center of the runway, which lets you know that you (Figure 162)  A.are on course and lined up correctly.  B.should recheck the winds prior to landing.  C.are off course. What effect would a light crosswind of approximately 5 knots have on vortex behavior?  A.The downwind vortex would tend to remain over the runway.  B.The light crosswind would rapidly dissipate vortex strength.  C.The upwind vortex would tend to remain over the runway. Test

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AS 221 Instrument Rating Ground School - Gleim
Test 1 ( IP02:5.1-5.5;5.14-5.15, IP03:1.1-1.3, IP04:1.4-1.9, IP05:7ALL, IP06:SU2 all)
Gleim IP 02: 5.1 -5.7 ; 5.14 -5.15


Gleim IP 03: 1.1 -1.3 (Test 1)
When an altimeter is changed from 30.11" Hg to 29.96" Hg, in which direction will the indicated altitude
change and by what value?
 A.Altimeter will indicate 150 feet lower.
 B.Altimeter will indicate 15 feet lower.
 C.Altimeter will indicate 150 feet higher.
Below 18,000 feet pressure altitude may be obtained by
 A.setting the altimeter to 29.92 inches Hg.
 B.requesting the current pressure altitude for the area.
 C.setting the altimeter to the local altimeter setting.
During a constant-rate climb in IMC above the freezing level, you notice that both the airspeed and altitude
are increasing. This indicates the
 A.gyroscopic instruments have failed.
 B.aircraft is in an unusual attitude.
 C.pitot static system has malfunctioned.
If you are departing from an airport where you cannot obtain an altimeter setting, you should set your
altimeter
 A.on 29.92 inches Hg.
 B.on the current airport barometric pressure, if known.
 C.to the airport elevation.
On what headings will the magnetic compass read most accurately during a level 360° turn, with a bank of
approximately 15°?
 A.135° through 225°.
 B.180° and 0°.
 C.90° and 270°.
If the pitot tube ram air pressure hole and drain hole become obstructed, the airspeed indicator will operate
 A.like a very sluggish airspeed indicator lagging all the changes by minutes.
 B.normally due to the static port pressure changes.
 C.like an altimeter as the aircraft climbs and descends.
If you are not able to obtain the current altimeter setting prior to takeoff, you should set this instrument to
 A.field elevation.
 B.29.92 inches Hg.
 C.pressure altitude.
The local altimeter setting should be used by all pilots in a particular area, primarily to provide for
 A.better vertical separation of aircraft.
 B.the cancellation of altimeter error due to nonstandard temperatures aloft.
 C.more accurate terrain clearance in mountainous areas.
If both the ram air input and the drain hole of the pitot system are blocked, what reaction should you observe
on the airspeed indicator when power is applied and a climb is initiated out of severe icing conditions?
 A.The airspeed would drop to, and remain at, zero.
 B.The indicated airspeed would show a continuous deceleration while climbing.
 C.No change until an actual climb rate is established, then indicated airspeed will increase.
If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the
airplane, which of the following should the pilot expect?
 A.The vertical speed to momentarily show a descent.
 B.The vertical speed to show a climb.
 C.The altimeter to read higher than normal.
You are preflighting for an IFR flight and set in the current altimeter setting, it should be not more than
 A.±100 feet from your referenced level.
 B.±150 feet from your referenced level.
 C.±75 feet from your referenced level.
On the taxi check, the magnetic compass should
 A.exhibit the same number of degrees of dip as the latitude.
 B.swing opposite to the direction of turn when turning from north.
 C.swing freely and indicate known headings.
How should you preflight check the altimeter prior to an IFR flight?
 A.Set the altimeter first with 29.92" Hg and then the current altimeter setting. The change in altitude
should correspond to the change in setting.
 B.Set the altimeter to the current altimeter setting. The indication should be within 75 feet of the

, actual elevation for acceptable accuracy.
 C.Set the altimeter to the current temperature. With current temperature and the altimeter
indication, determine the calibrated altitude to compare with the field elevation.
When initiating a left turn in the Northern Hemisphere from a heading of 270°. The magnetic compass will
 A.lag behind the actual rate of turn.
 B.initially indicate a turn in the opposite direction.
 C.initially indicate the actual rate of turn.
If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the
airplane, which of the following variations in instrument indications should the pilot expect?
 A.The altimeter will read lower than normal, airspeed lower than normal, and the VSI will
momentarily show a descent.
 B.The altimeter will read higher than normal, airspeed greater than normal, and the VSI will
momentarily show a climb.
 C.The altimeter will read lower than normal, airspeed greater than normal, and the VSI will
momentarily show a climb and then a descent.
What CAS must be used to maintain the filed TAS of 158 kt. at the flight planned altitude of 8,000 ft.?
(Temperature 0°C.)
 A.140 KCAS.
 B.153 KCAS.
 C.147 KCAS.
What is the procedure for setting the altimeter when assigned an IFR altitude of 18,000 feet or higher on a
direct flight off airways?
 A.Set the altimeter to 29.92" Hg before takeoff.
 B.Set the altimeter to the current altimeter setting until reaching the assigned altitude, then set to
29.92" Hg.
 C.Set the altimeter to the current reported setting for climb-out and 29.92" Hg upon reaching
18,000 feet.
At an altitude of 6,500 feet MSL, the current altimeter setting is 30.42" Hg. The pressure altitude would be
approximately
 A.6,500 feet.
 B.7,500 feet.
 C.6,000 feet.
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from
a westerly heading in the Northern Hemisphere?
 A.The compass will remain on a westerly heading for a short time, then gradually catch up to the
actual heading of the aircraft.
 B.The compass will initially show a turn in the opposite direction, then turn to a northerly indication
but lagging behind the actual heading of the aircraft.
 C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is
smooth.


Which altitude is indicated when the altimeter is set to 29.92" Hg?
 A.Density.
 B.Pressure.
 C.Standard.
While flying at an altitude of 8,000 ft., what CAS must be used to maintain a TAS of 155 kt. if the outside air
temperature is –5°C?
 A.142 KCAS.
 B.134 KCAS.
 C.139 KCAS.
During flight, if the pitot tube becomes clogged with ice, which of the following instruments would be
affected?
 A.The airspeed indicator, altimeter, and Vertical Speed Indicator.
 B.The airspeed indicator only.
 C.The airspeed indicator and the altimeter.
Under what condition is pressure altitude and density altitude the same value?
 A.At standard temperature.
 B.When indicated, and pressure altitudes are the same value on the altimeter.
 C.When the altimeter setting is 29.92" Hg.
Under which condition will pressure altitude be equal to true altitude?
 A.When the atmospheric pressure is 29.92" Hg.
 B.When standard atmospheric conditions exist.
 C.When indicated altitude is equal to the pressure altitude.
The pressure altitude at a given location is indicated on the altimeter after the altimeter is set to
 A.29.92" Hg.
 B.the current altimeter setting.
 C.the field elevation.

,If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the
airplane, which of the following should the pilot expect?
 A.The altimeter and airspeed indicator to become inoperative.
 B.The gyroscopic instruments to become inoperative.
 C.The vertical speed to momentarily show a climb.
Pressure altitude is the altitude read on your altimeter when the instrument is adjusted to indicate height
above
 A.ground level.
 B.sea level.
 C.the standard datum plane.
Which is the correct sequence for recovery from a spiraling, nose-low, increasing airspeed, unusual flight
attitude?
 A.Increase pitch attitude, reduce power, and level wings.
 B.Correct the bank attitude, raise the nose to a level attitude, and reduce power.
 C.Reduce power, correct the bank attitude, and raise the nose to a level attitude.
What would be the indication on the VSI during entry into a 500 FPM actual descent from level flight if the
static ports were iced over?
 A.The VSI pointer would remain at zero regardless of the actual rate of descent.
 B.The indication would be in reverse of the actual rate of descent (500 FPM climb).
 C.The initial indication would be a climb, then descent at a rate in excess of 500 FPM.
If you need to use an alternate static source during level flight, you can expect to see
 A.a higher indication on the altimeter.
 B.a momentary descent on the VSI.
 C.a lower indicated airspeed.
How can you obtain the pressure altitude on flights below 18,000 feet?
 A.Set your altimeter to the field elevation and read the pressure altitude from the Kollsman window.
 B.Contact an ATC facility FSS and request the current pressure altitude for the area.
 C.Set your altimeter to 29.92" Hg and read the pressure altitude on the instrument face.
En route at FL 290, the altimeter is set correctly, but not reset to the local altimeter setting of 30.57" Hg
during descent. If the field elevation is 650 feet and the altimeter is functioning properly, what is the
approximate indication upon landing?
 A.1,300 feet.
 B.Sea level.
 C.715 feet.
Under what condition will true altitude be lower than indicated altitude with an altimeter setting of 29.92"
Hg?
 A.When density altitude is higher than indicated altitude.
 B.In warmer than standard air temperature.
 C.In colder than standard air temperature.
Which condition would cause the altimeter to indicate a lower altitude than actually flown (true altitude)?
 A.Air temperature lower than standard.
 B.Air temperature warmer than standard.
 C.Atmospheric pressure lower than standard.
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from
a northerly heading in the Northern Hemisphere?
 A.The compass will indicate a turn to the right, but at a faster rate than is actually occurring.
 B.The compass will initially indicate a turn to the left.
 C.The compass will remain on north for a short time, then gradually catch up to the magnetic
heading of the aircraft.
What causes the northerly turning error in a magnetic compass?
 A.Coriolis force at the mid-latitudes.
 B.The magnetic dip characteristic.
 C.Centrifugal force acting on the compass card.
What CAS must be used to maintain 180 kt. TAS at the flight planned altitude of 8,000 ft. if the outside air
temperature is +8°C?
 A.157 KCAS.
 B.163 KCAS.
 C.154 KCAS.
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a
west heading in the Northern Hemisphere?
 A.The compass will initially indicate a turn to the right.
 B.The compass will remain on west for a short time, then gradually catch up to the magnetic heading
of the aircraft.
 C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is
smooth.
Altimeter setting is the value to which the scale of the pressure altimeter is set so the altimeter indicates
 A.pressure altitude at field elevation.

,  B.pressure altitude at sea level.
 C.true altitude at field elevation.
What should be the indication on the magnetic compass as you roll into a standard rate turn to the left from a
north heading in the Northern Hemisphere?
 A.The compass will remain on north for a short time, then gradually catch up to the magnetic
heading of the aircraft.
 B.The compass will indicate a turn to the left, but at a faster rate than is actually occurring.
 C.The compass will initially indicate a turn to the right.
While you are flying at FL 250, you hear ATC give an altimeter setting of 28.92" Hg in your area. At what
pressure altitude are you flying?
 A.26,000 feet.
 B.24,000 feet.
 C.25,000 feet.
Which of the following defines the type of altitude used when maintaining FL 210?
 A.Indicated.
 B.Calibrated.
 C.Pressure.
If both the ram air input and drain hole of the pitot system become blocked, the indicated airspeed will
 A.increase during a climb.
 B.remain constant regardless of altitude change.
 C.decrease during a climb.
En route at FL 290, your altimeter is set correctly, but you fail to reset it to the local altimeter setting of 30.26
in. Hg during descent. If the field elevation is 134 feet and your altimeter is functioning properly, what will it
indicate after landing?
 A.100 feet MSL.
 B.474 feet MSL.
 C.206 feet below MSL.
What should be the indication on the magnetic compass when you roll into a standard rate turn to the left
from a south heading in the Northern Hemisphere?
 A.The compass will remain on south for a short time, then gradually catch up to the magnetic
heading of the aircraft.
 B.The compass will initially indicate a turn to the right.
 C.The compass will indicate a turn to the left, but at a faster rate than is actually occurring.
What should be the indication on the magnetic compass as you roll into a standard-rate turn to the left from
an east heading in the Northern Hemisphere?
 A.The compass will initially indicate a turn to the right.
 B.The compass will remain on east for a short time, then gradually catch up to the magnetic heading
of the aircraft.
 C.The compass will indicate the approximate correct magnetic heading if the roll into the turn is
smooth.
You check the flight instruments while taxiing and find the vertical speed indicator (VSI) indicates a descent of
100 feet per minute. In this case, you
 A.may not proceed under IFR until the instrument is corrected by an authorized instrument
repairman.
 B.may take off under IFR and use 100 feet descent as the zero indication.
 C.may take off and proceed under IFR but only in VFR weather conditions.
How can you determine the pressure altitude on an airport without a tower or FSS?
 A.Set the altimeter to 29.92" Hg and read the altitude indicated.
 B.Use your computer and correct the field elevation for temperature.
 C.Set the altimeter to the current altimeter setting of a station within 100 miles and correct this
indicated altitude with local temperature.
What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from
a south heading in the Northern Hemisphere?
 A.The compass will remain on south for a short time, then gradually catch up to the magnetic
heading of the aircraft.
 B.The compass will initially indicate a turn to the left.
 C.The compass will indicate a turn to the right, but at a faster rate than is actually occurring.
How does a pilot normally obtain the current altimeter setting during an IFR flight in Class E airspace below
18,000 feet?
 A.The pilot should contact ARTCC at least every 100 NM and request the altimeter setting.
 B.FSS’s along the route broadcast the weather information at 15 minutes past the hour.
 C.ATC periodically advises the pilot of the proper altimeter setting.
If a standard-rate turn is maintained, how much time would be required to turn to the right from a heading of
090° to a heading of 270°?
 A.1 minute.
 B.3 minutes.
 C.2 minutes.

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