TEST BORRADO, QUIZÁS LE INTERESE:
Piloto Privado DR
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Piloto Privado DR Descripción: Piloto Privado Autor:
Fecha de Creación: 28/08/2019 Categoría: Ciencia Número Preguntas: 84 |
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The basic purpose of adjusting the fuel¬/air mixture at altitude is to. decrease the amount of fuel in the mixture in order to compensate for increased air density. decrease the fuel flow in order to compensate for decreased air density. increase the amount of fuel in the mixture to compensate for the decrease in
Pressure and density of the air. Which condition is most favorable for the development of carburetor icing? any temperature below freezing and a relative humidity of less than 50 percent. Temperature between 32 and 50 F and low humidity. Temperature between 20 and 70 F and high humidity. 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 . Loss of RPM. Engine roughness A drop in oil temperature and cylinder head temperature. If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter? The elevation of the nearest airport corrected to mean sea level. The elevation of the departure area. Pressure altitude corrected for nonstandard temperature. Which V speed represents maneuvering speed? Va VLo Vne. Prior to takeoff, the altimeter should be set to which altitude or altimeter setting? The current local altimeter setting, if available, or the departure airport elevation. The corrected density altitude of the departure airport. The corrected pressure altitude for the departure airport. How do variations in temperature affect the altimeter? Pressure levels are raised on warm days, and the indicated altitude is lower than true altitude. Higher temperature expands the pressure levels and the indicated altitude is higher than true altitude. Lower temperatures lower the pressure levels and the indicated altitude is lower than true altitude. What is true altitude? The vertical distance of the aircraft above sea level. The vertical distance of the aircraft above the surface. The height above the standard datum plane. What is absolute altitude? The altitude read directly from the altimeter. The vertical distance of the aircraft above the surface. The height above the standard datum plane. What is density altitude? The height above the standard datum plane. The pressure altitude corrected for nonstandard temperature. The altitude read directly from the altitude. What is pressure altitude? The indicated altitude corrected for position and installation errors The altitude indicated when the barometric pressure scale is set to 29.92. The indicated altitude corrected for nonstandard temperature and pressure. Under what condition is indicated altitude the same as true altitude? If the altimeter has no mechanical error. When at sea level under standard conditions. When at 18,000 feet MSL with the altimeter set at 29.92. A turn coordinator provides an indication of the. Movement of the aircraft about the yaw and roll axes. Angle of bank up to but not exceeding 30. Altitude of the aircraft with references to the longitudinal axis. What are the standard temperature and pressure values for sea level? 15 C and 29.92 inches Hg. 59 C and 1013.2 milibars. 59 F and 1013.2 milibars. If a pilot changes the altimeter setting from 30.11 to 29.96, what is the approximate change in indication? Altimeter will indicate .15 inches Hg higher. Altimeter will indicate 150 feet higher. Altimeter will indicate 150 feet lower. Under which condition will pressure altitude be equal to true altitude? When the atmospheric pressure is 29.92 inches Hg. When standard atmospheric condition exist. When indicated altitude is equal to the pressure altitude. Under what condition is pressure altitude and density altitude the same value? At sea level, when the temperature is 0 F. When the altimeter has no installation error. At standard temperature. If a flight is made from an area of low pressure into an area of high pressure without the altimeter setting being adjusted, the altimeter will indicate. The actual altitude above sea level. Higher than the actual altitude above sea level. Lower than the actual altitude above sea level. If a flight is made from an area of high pressure into an area of low pressure without the altimeter setting being adjusted, the altimeter will indicate. Lower than the actual altitude above sea level. Higher than the actual altitude above sea level. The actual altitude above sea level. Under what condition will true altitude be lower than indicated altitude? In colder than standard air temperature. In warmers than standard air temperature. When density altitude is higher than indicated altitude. Which condition would cause the altimeter to indicate a lower altitude than true altitude? Air temperature lower than standard. Atmospheric pressure lower than standard. Air temperature warmer than standard. . The angular difference between true north and magnetic north is. Magnetic deviation Magnetic variation Compass acceleration error. What is ground effect? The result of the interference of the surface of the earth with the airflow patterns about an airplane. The result of an alteration in airflow patterns, increasing induced drag about the wings of an airplane. The result of the disruption of the airflow patterns about the wings of an airplane to the point where the wings will no longer support the airplane in flight. An airplane said to be inherently stable will. Be difficult to stall Require less effort to control not spin. What determines the longitudinal stability of an airplane? The location of the CG with respect to the center of lift. The effectiveness of the horizontal stabilizer, rudder, and rudder trim tab. The relationship of thrust and lift to weight and drag. Loading an airplane to the most aft CG will cause the airplane to be. less stable at all speeds. less stable at slow speed, but more stable at high speeds. less stable at high speeds, but more stable at low speeds. An airplane has been loaded in such manner that the CG is located aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be. A longer takeoff run. difficulty in recovering from a stalled condition. stalling at higher than normal airspeed. Which basic flight maneuver increase the load factor on an airplane as compared to straight and level flight? Climbs Turns stalls. What forces makes an airplane turn? The horizontal component of lift the vertical component of lift Centrifugal force. During an approach to stall, an increased load factor will cause the airplane to. Stall at a higher airspeed. Have a tendency to spin. be more difficult to control. Select the four flight fundamentals involved in maneuvering an aircraft? Aircraft power, pitch, bank, and trim. Starting, taxiing, takeoff, and landing. Straight and level flight, turn climbs, and descents. Which aircraft has the right of way over all other air traffic? Balloon An aircraft in distress An aircraft on final approach to land. Except when necessary for takeoff or landing, what is the minimum safe altitude for a pilot to operate an aircraft anywhere? An altitude allowing, if a power unit fails, an emergency landing, without undue hazard to persons or property on the surface. An altitude of 500 feet to any person, vessel, vehicle, or structure. An altitude of 500 feet above the highest obstacle within a horizontal radius of 1000 feet. What is the minimum safe altitude for a pilot to operate an aircraft over than a congested area? An altitude allowing, if a power unit fails, an emergency landing without undue hazard to persons or property on the surface. An altitude of 500 feet AGL, except over open water or a sparsely populated area, which required 500 feet from any person, vessel, vehicle, or structure. An altitude of 500 feet above the highest obstacle within a horizontal radius of 1000 feet. While operating in a class D airspace, each pilot of an aircraft approaching to land on a runway served by a visual approach slope indicator (VASI) shall. Maintain a 3° glide until approximately ½ mile to the runway before going below the VASI. Maintain an altitude at or above the glide slope until a lower altitude is necessary for safe landing. Stay high until the runway can be reached in a power off landing. The number 9 and 27 on a runway indicate that the runway is oriented approximately. 009° and 027° true 090° and 270° true 090° and 270° magnetic. ( Refer to figure 50) Select the proper traffic pattern and runway for landing. Left-hand traffic and runway 18. Right-hand traffic and runway 18. Left-hand traffic and runway 22. Who should not participate in the land and hold short operations (LAHSO) progam? Recreational pilots only Military pilots Student pilots. ( Refer to figure 21) ( Area 2) The flag symbol at lakes Drummond represents a Compulsory reporting point for the Norfolk class C airspace. Compulsory reporting point for Hampton roads airports. visual checkpoint used to identify position for initial call up to Norfolk approach control. ( Refer to figure 24 )(Area 3) What is the height of the lighted obstacle approximately 6 nautical miles southwest of savannah international? 1,534 feet MSL 1,549 feet AGL 1,549 feet MSL. What minimum pilot certification is required for operation within class B airspace? Recreational pilot certificate Private pilot certificate or student pilot certificate with appropriate logbook endorsements. Private pilot certificate with an instrument rating. An ATC radar facility issues the following advisory to a pilot flying on a heading of 360°:¨ traffic 10 o’clock, 2 mile, southbound…¨ where should the pilot look for this traffic? Northwest Northeast Southwest. An ATC radar facility issues the following advisory to a pilot flying north in a calm wind:¨ traffic 9 o’clock, 2 mile , southbound…¨ where should the pilot look for this traffic? South North West. Unless otherwise authorized, if flying a transponder equipped aircraft, a pilot should squawk which VFR code? 1200 7600 7700. ( Refer to figure 53) Which type radar service is provided to VFR aircraft at Lincoln Municipal? Sequencing to the primary class C airport and standard separation. Sequencing to the primary class C airport and conflict resolution so that radar targets do not touch, or 1000 feet vertical separation. Sequencing to the primary class C airport, traffic advisories, conflict resolution, and safety alerts. If the control tower uses a light signal to direct a pilot to give way to other aircraft and continue circling, the light will be. Flashing red. Steady red. alternating red and green. A flashing white light from the control tower to a taxiing aircraft is an indication of Taxi at a faster speed. Taxi only on taxiways and not cross runways. return to the starting point on the airports. (Refer to figure 21)(Area 3) What is the recommended communications procedure for a landing at Currituck county airport? Transmit intention on 122.9 MHZ when 10 miles out and give positions reports in the traffic patterns. Contact Elizabeth city FSS for airports advisory service. Contact New Bem FSS for area traffic information. Prior to entering an airports advisory area, a pilot should Monitor ATIS for weather and traffic advisories. Contact approach control for vectors to be traffic patterns. Contact the local FSS for airport and traffic advisories. When must the battery in emergency locator transmitter (ELT) be replaced (or recharged if the battery is rechargeable)? After one-half the battery’s useful life. During each annual and 100-hour inspection. Every 24 calendar months. Every physical process of weather is accompanied by, or is the result of, a Movement of air Pressure differential Heat exchange. What is meant by the term ¨dewpoint¨? The temperature at which condensation and evaporation are equal. The temperature at which dew will always form. The temperature to which air must be cooled to become saturated. The amount of water vapor which air can hold depends on the. Dewpoint Air temperature Stability of the air. What is a characteristic of stable air? Stratiform clouds Unlimited visibility Cumulus clouds. Clouds are divided into four families according to their Outward shape Height range Composition. What are characteristic of unstable air? Turbulence and good surface visibility. Turbulence and poor surface visibility. Nimbostratus clouds and good surface visibility. What condition are necessary for the formation of thunderstorm? High humidity, lifting force, and unstable condition. High humidity, high temperature, and cumulus clouds. Lifting force, moist air, and extensive cloud cover. Upon encountering severe turbulence, which flight condition should the pilot attempt to maintain? Constant altitude and airspeed Constant angle of attack. Level flight altitude. Wingtip vortices created by large aircraft tend to Sink below the aircraft generating turbulence. Rise into the traffic pattern. Rise into the takeoff or landing path of a crossing runway. (Refer to figure 12) What are the wind condition at Wink, Texas (KINK)? Calm 110° at 12 knots, peak gusts 18 knots. 111° at 2 knots, peak gusts 18 knots. (Refer to figure 15) During the time period from 0600z to 0800z, what visibility is forecast for KOKC? Greater than 6 statue miles Not forecasted Possibly 6 statue miles. (Refer to figure 17) What wind is forecast for STL at 12,000 feet? 230° true at 56 knots 230° true at 39 knots 230° magnetic at 56 knots. (Refer to figure 36) What is the expected fuel consumption for a 1,000 nautical mile flight under the following conditions? Pressure altitude… 8,000 ft, temperature… 22°C, manifolds p… 20.8 inches, wind… calm. 60.2 gallons 70.1 gallons 73.2 gallons. If an emergency situation requires a downwind landing, pilots should expect a faster… Airspeed at touchdown, a longer ground roll, and better control throughout the landing roll. Groundspeed at touchdown, a longer ground roll, and the likelihood of overshooting the desired touchdown point. Groundspeed at touchdown, a shorter ground roll, and the likelihood of understanding the desired touchdown point. An aircraft is loaded 110 pounds over maximum certificated gross weight. If fuel (gasoline) is drained to bring the aircraft weight within limits, how much fuel should be drained? 15.7 gallons 16.2 gallons 18.4 gallons. weight aim weight Empty weight 1,495.0 101.4 151,593.0 Pilot and pass 380.0 64.0 Fuel (30g) 96.0 The CG is located how far aft of datum? CG 92.44 CG 94.01 CG 119.8. (Refer to figures 33 and 34). Determine if the airplane weight and balance is within limits. Front seats occupants….415 lbs Rear seat occupants…...110 lbs Fuel, aux, tanks…...........44 gal Baggage…......................32 lb 19 pounds overweight, CG within limits 19 pounds overweight, CG out of limits forward Weight within limits, CG out of limits. ( Refer to figure 35.) Calculate the moment of the airplane and determine which category is applicable. Weight Mom/1000 Empty weight 1,350 51.5 Pilot and Pass 310 Rear pass 96 Fuel, 38gal Oil, 8qt -0.2 79.2 utility category 80.8 utility category 81.2 utility category. (Refer to figure 35) What is the maximum amount of fuel that may be aboard the airplane on takeoff if loaded as follows? Weight Mom/1000 Empty weight 1,350 51.5 Pilot and front passenger 340 Rear passenger 310 Baggage 45 -0.2 Oil,qt8 24 gallons 32 gallons 40 gallons. ( Refer to figure 35) Determine the aircraft loaded moment and the aircraft category. Weight Mom/1000 Empty weight 1,350 51.5 Pilot and front passenger 340 Rear passenger 310 Baggage 45 -0.2 Oil,qt8 78.2, Normal category 79.2, Normal category 80.4, utility category. ( Refer to figure 33 and 34) What effect does a 35-gallon fuel burn ( main tank) have on the weight and balance if the airplane weighed 2,890 pounds and MOM/100 WAS 2,452 at takeoff? Weight is reduced by 210 pounds and the CG is aft of limits. Weight is reduced by 210 pounds and the CG is unaffected. Weight is reduced to 2,680 pounds and the CG moves forward. ( Refer to figure 8) What is the effect of a temperature increase from 35 to 50°F on the density altitude if the pressure altitude remains at 3,000 feet MSL? 1,000 foot increase 1,100 foot decrease 1,300 foot increase. ( Refer to figure 22) What is the estimated time enroute from Mercer County Regional Airport (Area 3) to Minot International (Area 1)? The wind is from 330° at 25 knots and the true airspeed is 100 knots. Add 3-1/2 minutes for departures and climbout. 44 minutes 48 minutes 52 minutes. (Refer to figure 23) Determine the estimated time enroute for a flight from Priest River Airport (Area 1) to Shoshone County Airport (Area 3). The wind is from 030° at 12 knots. The true airspeed is 95 knots. Add 2 minutes for climbout. 27 minutes 29 minutes 31 minutes. (Refer to figure 26) What is the estimated time enrooted for a flight from Denton Muni (Area 1) to Addison (Area 2)? The wind is from 200° at 20 knots, the true airspeed is 110 knots, and the magnetic variation is 7° east. 13 minutes 16 minutes 19 minutes. (Refer to figure 63) In flying the rectangular course, when would the aircraft be turned less than 90°? Corners 1 and 4 Corners 1 and 2 Corners 2 and 4. How far will an aircraft travel in 2-1/2 minutes with a groundspeed of 98 knots? 2.45NM 3.35NM 4.08NM. How far will an aircraft travel in 7.5 minutes with a groundspeed of 114 knots? 14.25NM 15.00NM 14.50NM. (Refer to figure 22) Determine the magnetic heading for a flight from Mercer County Regional Airport (Area 3) to Minot International ( Area 1). The wind is from 330° at 25 knots, the true airspeed is 100 knots, and the magnetic variation is 10° east. 002° 012° 352°. (Refer to figure 21) Determine the magnetic course from First Flight Airport (Area 5) to Hampton Roads Airports (Area 2). 141° 321° 331°. (Refer to figure 23) Determine the magnetic heading for a flight from Sandpoint Airport (Area 1) to St.Maries Airport (Area 4). The wind is from 215° at 25 knots, and the true airspeed is 125 knots. 169° 349° 187°. (Refer to figure 23) Determine the magnetic heading for a Flight from St. Maries Airport (Area 4) to priest River Airport (Area 1). The wind is from 340° at 10 knots and the true airspeed is 90 knots. 345° 320° 327°. (Refer to figure 31)(Illustration 1). The relative bearing TO the station is 045° 180° 315°. (Refer to figure 31)(illustration 8) If the magnetic bearing TO the station is 135°, the magnetic heading is 135° 270° 360°. |
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