TEST BORRADO, QUIZÁS LE INTERESE:
Commercial Pilot - (CH. 9) Navigation NO FIG
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Título del Test:
Commercial Pilot - (CH. 9) Navigation NO FIG Descripción: Examen PC DGAC Autor:
Fecha de Creación: 07/03/2024 Categoría: Otros Número Preguntas: 60 |
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1.- The ADF is tuned to a nondirectional radiobeacon and the relative
bearing changes from 090° to 100° in 2.5 minutes of elapsed time. If
the true airspeed is 90 knots, th distance and time en route to that
radiobeacon would be 15 miles and 22.5 minutes. 22.5 miles and 15 minutes. 32 miles and 18 minutes. 2.- GIVEN: Wingtip bearing change ............................................. 10° Elapsed time between bearing change ..................... 4 min Rate of fuel consumption .................................. 11 gal/hr Calculate the fuel required to fly to the station. 4.4 gallons. 8.4 gallons. 12 gallons. 3.- GIVEN: Wingtip bearing change ............................................. 15° Elapsed time between bearing change ................... 7.5 min True airspeed ....................................................... 85 kts Rate of fuel consumption .................................. 9.6 gal/hr The time, distance, and fuel required to fly to the station is 30 minutes; 42.5 miles; 4.80 gallons. 32 minutes; 48 miles; 5.58 gallons. 48 minutes; 48 miles; 4.58 gallons. 4.- GIVEN: Wingtip bearing change ............................................. 15° Elapsed time between bearing change ..................... 6 min Rate of fuel consumption ................................. 8.6 gal/hr Calculate the approximate fuel required to fly to the station. 3.44 gallons. 6.88 gallons. 17.84 gallons. 5.- While maintaining a constant heading, a relative bearing of 15° doubles in 6 minutes. The time to the station being used is 3 minutes. 6 minutes. 12 minutes. 6.- If the relative bearing changes from 090° to 100° in 2.5 minutes of elapsed time, the time en route to that station would be 12 minutes 15 minutes. 18 minutes. 7.- GIVEN: Wingtip bearing change .............................................. 5° Elapsed time between bearing change ..................... 6 min Rate of fuel consumption .................................. 12 gal/hr The fuel required to fly to the station is 8.2 gallons. 14.4 gallons. 18.7 gallons. 8.- The ADF is tuned to a nondirectional radiobeacon and the relative bearing changes from 085° to 090° in 2 minutes of elapsed time. The time en route to that station would be 15 minutes. 18 minutes. 24 minutes. 10.- The ADF is tuned to a nondirectional radiobeacon and the relative bearing changes from 095° to 100° in 1.5 minutes of elapsed time. The time en route to that station would be 18 minutes. 24 minutes. 30 minutes. 11.- GIVEN: Wingtip bearing change ......................................... 5° Time elapsed between bearing change ............... 5 min True airspeed ............................................... 115 kts The distance to the station is 36 NM. 57.5 NM. 115 NM. 12.- With a TAS of 115 knots, the relative bearing on an ADF changes from 090° to 095° in 1.5 minutes of elapsed time. The distance to the station would be 12.5 NM. 24.5 NM. 34.5 NM. 13.- The ADF indicates a wingtip bearing change of 10° in 2 minutes of elapsed time, and the TAS is 160 knots. What is the distance to the station? 15 NM. 32 NM. 36 NM. 14.- The relative bearing on an ADF changes from 265° to 260° in two (2) minutes of elapsed time. If the groundspeed is 145 knots, the distance to that station would be: 26 NM. 37 NM. 58 NM. 16.- GIVEN: True course .................................................................. 345° True heading ................................................................ 355° True airspeed ............................................................. 85 kts Groundspeed .............................................................. 95 kts Determine the wind direction and speed. 095° and 19 knots. 113° and 19 knots. 238° and 18 knots. 17.- GIVEN: True course .................................................................. 105° True heading ................................................................ 085° True airspeed ............................................................. 95 kts Groundspeed .............................................................. 87 kts Determine the wind direction and speed. 020° and 32 knots. 030° and 38 knots. 200° and 32 knots. 18.- If fuel consumption is 14.7 gallons per hour and groundspeed is 157 knots, how much fuel is required for an airplane to travel 612 NM? 58 gallons. 60 gallons. 64 gallons. 19.- If an airplane is consuming 14.8 pounds of fuel per hour at a cruising altitude of 7,500 feet and the groundspeed is 167 knots, how much fuel is required to travel 560 NM? 50 gallons. 53 gallons. 57 gallons. 20.- If an airplane is consuming 9.5 gallons of fuel per hour at a cruising altitude of 6,000 feet and the groundspeed is 135 knots, how much fuel is required to travel 490 NM? 27 gallons. 30 gallons. 35 gallons. 21.- If an airplane is consuming 95 pounds of fuel per hour at a cruising altitude of 6,500 feet and the groundspeed is 173 knots, how much fuel is required to travel 450 NM? 248 pounds. 265 pounds. 284 pounds. 22.- If fuel consumption is 80 pounds per hour and groundspeed is 180 knots, how much fuel is required for an airplane to travel 460 NM? 205 pounds. 212 pounds. 460 pounds. 23.- An airplane descends to an airport under the following conditions: Cruising altitude .................................................................... 10,500 ft Airport elevation ..................................................................... 1,700 ft Descends to .................................................................... 1,000 ft AGL Rate of descent ................................................................. 600 ft/min Average true airspeed ............................................................ 135 kts True course .............................................................................. 263° Average wind velocity .................................................. 330° at 30 kts Variation .................................................................................. 7°E Deviation .................................................................................. +3° Average fuel consumption ............................................... 11.5 gal/hr Determine the approximate time, compass heading, distance, and fuel consumed during the descent. 9 minutes, 274°, 26 NM, 2.8 gallons. 13 minutes, 274°, 26 NM, 2.5 gallons. 13 minutes, 271°, 26 NM, 2.5 gallons. 24.- An airplane descends to an airport under the following conditions: Cruising altitude ..................................................................... 6,500 ft Airport elevation ....................................................................... 700 ft Descends to ...................................................................... 800 ft AGL Rate of descent ................................................................. 500 ft/min Average true airspeed ............................................................ 110 kts True course .............................................................................. 335° Average wind velocity .................................................. 060° at 15 kts Variation .................................................................................. 3°W Deviation .................................................................................. +2° Average fuel consumption ................................................. 8.5 gal/hr Determine the approximate time, compass heading, distance, and fuel consumed during the descent. 10 minutes, 348°, 18 NM, 1.4 gallons. 10 minutes, 355°, 17 NM, 2.4 gallons. 12 minutes, 346°, 18 NM, 1.6 gallons. 25.- GIVEN: Pressure altitude ...................................................... 7,000 ft True air temperature .................................................... +15°C From the conditions given, the approximate density altitude is 5,000 feet. 8,500 feet. 9,500 feet. 26.- GIVEN: Pressure altitude ...................................................... 6,000 ft True air temperature .................................................... +30°F From the conditions given, the approximate density altitude is 9,000 feet. 5,500 feet. 5,000 feet. 27.- GIVEN: Pressure altitude ...................................................... 5,000 ft True air temperature ................................................... +30°C From the conditions given, the approximate density altitude is 7,200 feet. 7,800 feet. 9,000 feet. 28.- GIVEN: Pressure altitude .................................................... 12,000 ft True air temperature .................................................... +50°F From the conditions given, the approximate density altitude is 11,900 feet. 14,130 feet. 18,150 feet. 29.- Which data must be recorded in the aircraft logbook or other record by a pilot making a VOR operational check for IFR operations? VOR name or identification, place of operational check, amount of bearing error, and date of check. Date of check, place of operational check, bearing error, and signature. VOR name or identification, amount of bearing error, date of check, and signature. 30.- When must an operational check on the aircraft VOR equipment be accomplished to operate under IFR? Within the preceding 30 days or 30 hours of flight time. 10 days or 10 hours of flight time. 30 days. 31.- What is the maximum bearing error (+ or -) allowed for an operational VOR equipment check when using an approved ground test signal? 4 degrees 8 degrees 12 degrees. 34.- While maintaining a constant heading, the ADF needle increases from a relative bearing of 45° to 090° in 5 minutes. The time to the station being used is 5 minutes. 10 minutes 15 minutes. 35.- The ADF is tuned to a nondirectional radiobeacon and the relative bearing changes from 270° to 265° in 2.5 minutes of elapsed time. The time en route to that beacon would be 9 minutes 18 minutes. 30 minutes. 36.- While cruising at 135 knots and on a constant heading, the ADF needle decreases from a relative bearing of 315° to 270° in 7 minutes. The approximate time and distance to the station being used is 7 minutes and 16 miles. 14 minutes. and 28 miles. 19 minutes and 38 miles. 37.- Inbound on the 190 radial, a pilot selects the 195 radial, turns 5° to the left, and notes the time. While maintaining a constant heading, the pilot notes the time for the CDI to center is 10 minutes. Based on this information, the ETE to the station is 10 minutes. 15 minutes. 20 minutes. 38.- When checking the course sensitivity of a VOR receiver, how many degrees should the OBS be rotated to move the CDI from the center to the last dot on either side? 5° to 10°. 10° to 12°. 18° to 20°. 39.- When the CDI needle is centered during an airborne VOR check, the omnibearing selector and the TO/FROM indicator should read within 4° of the selected radial. within 6° of the selected radial. 0° TO, only if you are due south of the VOR. 40.- When using VOT to make a VOR receiver check, the CDI should be centered and the OBS should indicate that the aircraft is on the 090 radial. 180 radial. 360 radial. 41.- How should the pilot make a VOR receiver check when the aircraft is located on the designated checkpoint on the airport surface? Set the OBS on 180° plus or minus 4°; the CDI should center with a FROM indication. Set the OBS on the designated radial. The CDI must center within plus or minus 4° of that radial with a FROM indication. With the aircraft headed directly toward the VOR and the OBS set to 000°, the CDI should center within plus or minus 4° of that radial with a TO indication. 42.- Inbound on the 315 radial, a pilot selects the 320 radial, turns 5° to the left, and notes the time. While maintaining a constant heading, the pilot notes the time for the CDI to center is 12 minutes. Based on this information, the ETE to the station is 10 minutes. 12 minutes. 24 minutes. 43.- Inbound on the 090 radial, a pilot rotates the OBS 010° to the left, turns 010° to the right, and notes the time. While maintaining a constant heading, the pilot determines that the elapsed time for the CDI to center is 8 minutes. Based on this information, the ETE to the station is 8 minutes. 16 minutes. 24 minutes. 44.- Inbound on the 040 radial, a pilot selects the 055 radial, turns 15° to the left, and notes the time. While maintaining a constant heading, the pilot notes the time for the CDI to center is 15 minutes. Based on this information, the ETE to the station is 8 minutes. 15 minutes. 30 minutes. 49.- While maintaining a magnetic heading of 270° and a true airspeed of 120 knots, the 360 radial of a VOR is crossed at 1237 and the 350 radial is crossed at 1244. The approximate time and distance to this station are 42 minutes and 84 NM. 42 minutes and 91 NM. 44 minutes and 96 NM. 55.- An aircraft 60 miles from a VOR station has a CDI indication of onefifth deflection, this represents a course centerline deviation of approximately 6 miles. 2 miles. 1 mile. 56.- While maintaining a constant heading, a relative bearing of 10° doubles in 5 minutes. If the true airspeed is 105 knots, the time and distance to the station being used is approximately 5 minutes and 8.7 miles. 10 minutes and 17 miles. 15 minutes and 31.2 miles. 58.- If an airplane is consuming 12.5 gallons of fuel per hour at a cruising altitude of 8,500 feet and the groundspeed is 145 knots, how much fuel is required to travel 435 NM? 27 gallons. 34 gallons. 38 gallons. 60.- You have flown 52 miles, are 6 miles off course, and have 118 miles yet to fly. To converge on your destination, the total correction angle would be 3°. 6°. 10°. 61.- GIVEN: Distance off course .................................................................. 9 mi Distance flown ....................................................................... 95 mi Distance to fly ...................................................................... 125 mi To converge at the destination, the total correction angle would be 4°. 6°. 10°. 62.- An airplane descends to an airport under the following conditions: Cruising altitude ....................................................................... 7,500 ft Airport elevation ....................................................................... 1,300 ft Descends to ......................................................................... 800 ft AGL Rate of descent .................................................................... 300 ft/min Average true airspeed ............................................................... 120 kts True course ................................................................................. 165° Average wind velocity ..................................................... 240° at 20 kts Variation .................................................................................. 4°E Deviation .................................................................................. -2° Average fuel consumption ................................................. 9.6 gal/hr Determine the approximate time, compass heading, distance, and fuel consumed during the descent. 16 minutes, 168°, 30 NM, 2.9 gallons. 18 minutes, 164°, 34 NM, 3.2 gallons 18 minutes, 168°, 34 NM, 2.9 gallons. 63.- GIVEN: Wind .................................................................. 175° at 20 kts Distance ...................................................................... 135 NM True course ...................................................................... 075° True airspeed ................................................................. 80 kts Fuel consumption ........................................................ 105 lb/hr Determine the time en route and fuel consumption. 1 hour 28 minutes and 73.2 pounds. 1 hour 38 minutes and 158 pounds. 1 hour 40 minutes and 175 pounds. 65.- True course measurements on a Sectional Aeronautical Chart should be made at a meridian near the midpoint of the course because the values of isogonic lines change from point to point. angles formed by isogonic lines and lines of latitude vary from point to point. angles formed by lines of longitude and the course line vary from point to point. 68.- To track inbound on the 215 radial of a VOR station, the recommended procedure is to set the OBS to 215° and make heading corrections toward the CDI needle. 215° and make heading corrections away from the CDI needle. 035° and make heading corrections toward the CDI needle. 69.- To track outbound on the 180 radial of a VOR station, the recommended procedure is to set the OBS to 360° and make heading corrections toward the CDI needle. 180° and make heading corrections away from the CDI needle. 180° and make heading corrections toward the CDI needle. 73.- Which situation would result in reverse sensing of a VOR receiver? Flying a heading that is reciprocal to the bearing selected on the OBS. Setting the OBS to a bearing that is 90° from the bearing on which the aircraft is located. Failing to change the OBS from the selected inbound course to the outbound course after passing the station. 74.- If the relative bearing to a nondirectional radiobeacon is 045° and the magnetic heading is 355°, the magnetic bearing TO that radiobeacon would be 040°. 065°. 220°. 75.- For night flying operations, the best night vision is achieved when the: pupils of the eyes have become dilated in approximately 10 minutes rods in the eyes have become adjusted to the darkness in approximately 30 minutes cones in the eyes have become adjusted to the darkness in aproximately 5 minutes. 76.- When operating VFR at night, what is the first indication of flying into restricted visibility conditions A gradual disappearence of lights on the ground Ground lights begin to take on an appearance of being surrounded by a halo or glow Cockpit lights begin to take on an appearance of a halo or glow around them. 77.- An airplane departs an airport under the following conditions: Airport elevation ..................................................................... 1,500 ft Cruising altitude ...................................................................... 9,500 ft Rate of climb ...................................................................... 500 ft/min Average true airspeed ............................................................. 160 kts True course ............................................................................... 145° Average wind velocity ................................................... 080° at 15 kts Variation .................................................................................. 5°E Deviation .................................................................................. -3° Average fuel consumption .................................................. 14 gal/hr Determine the approximate time, compass heading, distance, and fuel consumed during the climb. 14 minutes, 128°, 35 NM, 3.2 gallons. 16 minutes, 132°, 41 NM, 3.7 gallons. 16 minutes, 128°, 32 NM, 3.8 gallons. 78.- After experiencing a powerplant failure at night, one of the primary consdiderations should include: turning off all electrical switches to save battery power for landing Maneuvering to and landing on a lighted highway or road planning the emergency approach and landing to an unlighted portion of an area. 79.- When planning for an emergency landing at night on of the primary considerations should include landing without flaps to ensure a nose - high landing attitude at touchdown turning off all the electrical switches to save battery power for the landing selecting a landing area close to public access, if possible. 80.- The ADF is tuned to a radiobeacon. If the magnetic heading is 040° and the relative bearing is 290°, the magnetic bearing TO that radiobeacon would be 150°. 285°. 330°. 81.- An airplane departs an airport under the following conditions: Airport elevation ..................................................................... 1,000 ft Cruise altitude ...................................................................... 9,500 ft Rate of climb ...................................................................... 500 ft/min Average true airspeed ............................................................. 135 kts True course .............................................................................. 215° Average wind velocity .................................................. 290° at 20 kts Variation .................................................................................. 3°W Deviation .................................................................................. -2° Average fuel consumption .................................................. 13 gal/hr Determine the approximate time, compass heading, distance, and fuel consumed during the climb. 14 minutes, 234°, 26 NM, 3.9 gallons. 17 minutes, 224°, 36 NM, 3.7 gallons. 17 minutes, 242°, 31 NM, 3.5 gallons. |
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