PAR MIS.
(Refer to Figure 40.) What is the necessary distance required for takeoff to clear a 50-foot obstacle? OAT - Std, Pressure altitude - Sea level, Takeoff weight - 2,700 lb, Headwind component - Calm 2,100 feet. 1,800 feet. 1,400 feet.
1,400 feet.
(Refer to figure 37.) Determine the total distance required to land. OAT: 32 F Pressure altitude: 8,000 ft Weight: 2,600 lb Headwind component: 20 kts Obstacle: 50 ft 850 feet. 1,400 feet. 1,750 feet
1,400 feet.
Refer to Figure 40.) What is the approximate ground roll distance necessary for takeoff under the following conditions? OAT - 100°F, Pressure altitude - 4,000 ft, Takeoff weight - 2,700 lb, Headwind component - Calm 1,400 feet. 1,000 feet. 1,800 feet.
1,400 feet.
(Refer to Figure 82.) Based upon the altitude indicated by altimeter #3, which course direction is appropriate for this VFR cruising altitude? 0°-179° true. 080° magnetic. 180°-359° magnetic.
080° magnetic.
(Refer to figure 3.) Which altimeter(s) indicate(s) more than 10,000 feet? 1 only. 1 and 2 only. 1, 2, and 3.
1 and 2 only.
(Refer to figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude: 7,500 ft Headwind: 8 kts Temperature: 32 F Runway: Hard surface 1,004 feet. 1,205 feet. 1,506 feet.
1,004 feet.
(Refer to figure 40.) Determine the approximate ground roll distance required for takeoff. OAT: 38 C Pressure altitude: 2,000 ft Takeoff weight: 2,750 lb Headwind component: Calm 1,300 feet. 1,800 feet. 1,150 feet.
1,150 feet.
(Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97. 1,562 feet MSL. 1,341 feet MSL. 1,451 feet MSL
1,341 feet MSL.
The CG is located how far aft of datum? GIVEN: WEIGHT (LB) ARM (IN) MOMENT (LB-IN) Empty weight: 1,495.0 101.4 151,593.0 Pilot and passengers: 380.0 64.0 --- Fuel (30 gal usable no reserve): --- 96.0 --- CG 119.8. CG 92.44. CG 94.01.
CG 94.01.
Prior to takeoff, the altimeter should be set to which altitude or altimeter setting? The corrected density altitude of the departure airport. The corrected pressure altitude for the departure airport. The current local altimeter setting, if available, or the departure airport elevation.
The current local altimeter setting, if available, or the departure airport elevation.
If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter? Pressure altitude corrected for nonstandard temperature. The elevation of the departure area. The elevation of the nearest airport corrected to mean sea level.
The elevation of the departure area.
What is density altitude? The pressure altitude corrected for nonstandard temperature. The altitude read directly from the altimeter. The height above the standard datum plane.
The pressure altitude corrected for nonstandard temperature.
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
The vertical distance of the aircraft above the surface.
What minimum radio equipment is required for VFR operation within Class B airspace? Two-way radio communications equipment, a 4096-code transponder, an encoding altimeter, and ADS-B Out. Two-way radio communications equipment and a 4096-code transponder. Two-way radio communications equipment, a 4096-code transponder, an encoding altimeter, and a VOR or TACAN receiver.
Two-way radio communications equipment, a 4096-code transponder, an encoding altimeter, and ADS-B Out.
What minimum radio equipment is required for operation within Class C airspace? Two-way radio communications equipment, a 4096-code transponder, and DME. Two-way radio communications equipment and a 4096-code transponder. Two-way radio communications equipment, a 4096-code transponder, an encoding altimeter, and ADS-B Out.
Two-way radio communications equipment, a 4096-code transponder, an encoding altimeter, and ADS-B Out.
What causes variations in altimeter settings between weather reporting points? Variation of terrain elevation. Coriolis force. Unequal heating of the Earth's surface.
Unequal heating of the Earth's surface.
If a flight is made from an area of high pressure into an area of lower pressure without the altimeter setting being adjusted, the altimeter will indicate higher than the actual altitude above sea level.. lower than the actual altitude above sea level. the actual altitude above sea level.
higher than the actual altitude above sea level.
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 lower than the actual altitude above sea level. higher than the actual altitude above sea level. the actual altitude above sea level.
lower than the actual altitude above sea level.
(Refer to Figure 37.) What is your total distance to land using the data below? OAT - 90°F, Pressure altitude - 6,000 ft, Weight - 2,700 lb, Headwind component - 20 kts, Obstacle - 50 ft 1,550 feet.. 1,725 feet. 1,800 feet.
1,550 feet..
(Refer to figure 40.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT: Std Pressure altitude:: 4,000 ft Takeoff weight: 2,800 lb Headwind component: Calm 1,500 feet 2,000 feet. 1,750 feet.
1,750 feet.
(Refer to figure 37.) Determine the approximate total distance required to land over a 50-foot obstacle. OAT: 090 F Pressure altitude: 4,000 ft Weight: 2,800 lb Headwind component: 10 kts 1,950 feet. 1,525 feet. 1,775 feet.
1,775 feet.
(Refer to Figure 37.) What is your total distance to land using the data below? OAT - Std, Pressure altitude - 6,000 ft, Weight - 2,700 lb, Wind component - Calm, Obstacle - 50 ft. 1,450 feet. 1,900 feet. 1,750 feet.
1,900 feet.
At approximately what altitude above the surface would the pilot expect the base of cumuliform clouds if the surface air temperature is 82 °F and the dewpoint is 38 °F? 11,000 feet AGL. 10,000 feet AGL. 9,000 feet AGL
10,000 feet AGL.
Refer to figure 3.) Altimeter 1 indicates 500 feet. 10,500 feet. 1,500 feet.
10,500 feet.
(Refer to figure 34.) What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope? WEIGHT (LB) MOM/1000 Empty weight: 1,350 51.5 Pilot and front passenger: 250 --- Rear passengers: 400 --- Baggage: --- --- Fuel, 30 gal: --- --- Oil, 8 qt: --- -0.2 105 pounds. 120 pounds. 110 pounds.
105 pounds.
On a cross-country flight, point A is crossed at 1500 hours and the plan is to reach point B at 1530 hours. Use the following information to determine the airspeed required to reach point B on schedule. Distance between A and B: 70 NM Forecast wind: 310° at 15 kts Pressure altitude: 8,000 ft Ambient temperature: -10° C True course: 270° 126 knots. 152 knots. 137 knots.
137 knots.
(Refer to figure 3) Altimeter 2 indicates 4,500 feet. 1,500 feet. 14,500 feet.
14,500 feet.
(Refer to figure 3.) Altimeter 2 indicates 4,500 feet. 1,500 feet. 14,500 feet.
14,500 feet.
At what altitude shall the altimeter be set to 29.92, when climbing to cruising flight level? 14,500 feet MSL. 18,000 feet MSL. 24,000 feet MSL
18,000 feet MSL.
(Refer to Figure 40.) Determine the total distance required for takeoff to clear a 50-foot obstacle. OAT - Std, Pressure altitude - 6,000 ft, Takeoff weight - 2,800 lb, Headwind component - Calm 2,000 feet. 1,750 feet. 1,000 feet.
2,000 feet.
(Refer to Figure 8.) Determine the density altitude for these conditions: Altimeter setting - 30.30, Runway temperature - +25°F, Airport elevation - 3,894 it MSL 3,650 feet MSL. 3,000 feet MSL. 2,200 feet MSL
2,200 feet MSL
(Refer to figure 8.) Determine the pressure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22 at standard temperature. 3,010 feet MSL. 2,991 feet MSL. 2,913 feet MSL.
2,991 feet MSL.
(Refer to figure 8.) Determine the pressure altitude at an airport that is 3,563 feet MSL with an altimeter setting of 29.96. 3,527 feet MSL. 3,599 feet MSL. 3,639 feet MSL.
3,527 feet MSL.
(Refer to figure 22.) Determine the estimated time en route for a flight from Priest River Airport (area 1) to Shoshone County Airport (area 3). The wind is from 030 at 12 knots and the true airspeed is 95 knots. Add 2 minutes for climb-out. 27 minutes. 31 minutes. 29 minutes.
31 minutes.
(Refer to Figure 35.) Determine your fuel consumption for a 500 nautical mile flight using the following conditions? Pressure altitude - 6,000 ft, Temperature - +26°C, Manifold pressure - 21"" Hg, Wind - Calm 36.1 gallons. 35.6 gallons. 40.1 gallons
35.6 gallons.
(Refer to figure 38.) Determine the approximate landing ground roll distance. Pressure altitude: 1,250 ft Headwind: 8 kts Temperature: Std 275 feet. 470 feet. 366 feet
366 feet
Refer to figure 34.) What is the maximum amount of fuel that may be aboard the airplane on takeoff if loaded as follows? WEIGHT (LB) MOM/1000 Empty weight: 1,350 51.5 Pilot and front passenger: 340 --- Rear passengers: 310 --- Baggage: 45 --- Oil, 8 qt: --- --- 24 gallons. 40 gallons. 32 gallons.
40 gallons.
(Refer to figure 38.) Determine the approximate landing ground roll distance. Pressure altitude: Sea level Headwind: 4 kts Temperature: Std 401 feet. 356 feet. 490 feet.
401 feet.
Refer to figures 32, 33.) What is the maximum amount of baggage that can be carried when the airplane is loaded as follows? Front seat occupants: 387 lb Rear seat occupants: 293 lb Fuel:35 gal 63 pounds.. 220 pounds. 45 pounds
45 pounds
Which VFR cruising altitude is acceptable for a flight on a Victor Airway with a magnetic course of 175°? The terrain is less than 1,000 feet. 4,500 feet. 5,500 feet. 5,000 feet.
5,500 feet.
(Refer to figure 38.) Determine the approximate landing ground roll distance. Pressure altitude: 5,000 ft Headwind: Calm Temperature: 101 F 545 feet. 445 feet. 495 feet.
545 feet.
(Refer to figure 40.) Determine the approximate ground roll distance required for takeoff. OAT: 32 C Pressure altitude: 2,000 ft Takeoff weight: 2,500 lb Headwind component: 20 kts 650 feet. 1,000 feet. 850 feet.
650 feet.
Refer to figure 35.) 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 Manifold pressure: 20.8 inches Hg Wind: Calm 73.2 gallons. 70.1 gallons. 60.2 gallons
70.1 gallons.
If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs? 700-foot increase in indicated altitude. 70-foot increase in indicated altitude. 70-foot increase in density altitude.
700-foot increase in indicated altitude.
(Refer to figure 34.) Determine the moment with the following data: WEIGHT (LB) MOM/1000 Empty weight: 1,350 51.5 Pilot and front passenger: 340 --- Fuel (std tanks) Capacity --- Oil, 8 qt: --- --- 74.9 pound-inches. 77.6 pound-inches. 69.9 pound-inches
74.9 pound-inches.
(Refer to figure 34.) Determine the aircraft loaded moment and the aircraft category. WEIGHT (LB) MOM/1000Empty weight: 1,350 51.5 Pilot and front passenger: 380 --- Fuel, 48 gal: 288 --- Oil, 8 qt: --- --- 78.2, normal category. 80.4, utility category. 79.3, normal category.
79.3, normal category.
(Refer to figure 8.) Determine the density altitude for these conditions: Altimeter setting: 29.25 Runway temperature: +81 F Airport elevation: 5,250 ft MSL 4,600 feet MSL. 8,500 feet MSL. 5,877 feet MSL.
8,500 feet MSL
(Refer to figure 34.) Calculate the moment of the airplane and determine which category is applicable. WEIGHT (LB) MOM/1000 Empty weight: 1,350 51.5 Pilot and front passenger: 310 --- Rear passengers: 96 --- Fuel, 38 gal: --- --- Oil, 8 qt: --- -0.2 79.2, utility category. 81.4, utility category. 81.0, utility category
81.0, utility category
(Refer to figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude: 3,750 ft Headwind: 12 kts Temperature: Std 794 feet. 836 feet. 816 feet.
816 feet.
(Refer to figure 3.) Altimeter 3 indicates 15,940 feet. 9,500 feet .10,950 feet.
9,500 feet
(Refer to figure 38.) Determine the total distance required to land over a 50-foot obstacle. Pressure altitude: 5,000 ft Headwind: 8 kts Temperature: 41 F Runway: Hard surface 1,076 feet. 837 feet. 956 feet.
956 feet.
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
Air temperature warmer than standard
The pitot-static system drives the: Airspeed indicator, attitude indicator and heading indicator. Altimeter, vertical speed indicator, and heading indicator. Airspeed indicator, altimeter, and vertical speed indicator.
Airspeed indicator, altimeter, and vertical speed indicator.
The pitot system provides impact pressure for which instrument? Vertical-speed indicator. Altimeter. Airspeed indicator.
Airspeed indicator.
Which instrument is affected if the pitot tube is blocked? Vertical speed indicator. Airspeed indicator. Altimeter.
Airspeed indicator.
Which instrument(s) will become inoperative if the static vents become clogged? Altimeter only. Airspeed, altimeter, and vertical speed. Airspeed only
Airspeed, altimeter, and vertical speed.
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.
Altimeter will indicate 150 feet lower.
Under what condition is pressure altitude and density altitude the same value? At sea level, when the temperature is 0 °F. At standard temperature. When the altimeter has no installation error.
At standard temperature.
An operable 4096-code transponder with an encoding altimeter and ADS-B Out are required in which airspace? Class D and Class E (below 10,000 feet MSL). Class A, Class B (and within 30 miles of the Class B primary airport), and Class C. Class D and Class G (below 10,000 feet MSL).
Class A, Class B (and within 30 miles of the Class B primary airport), and Class C.
An operable 4096-code transponder, Mode C encoding altimeter, and ADS-B-Out are required in Class D airspace. Class E airspace below 10,000 feet MSL. Class B airspace and within 30 miles of the Class B primary airport.
Class B airspace and within 30 miles of the Class B primary airport.
(Refer to figures 32, 33.) Which action can adjust the airplane's weight to maximum gross weight and the CG within limits for takeoff? Front seat occupants: 425 lb Rear seat occupants: 300 lb Fuel, main tanks: 44 gal Transfer 12 gallons of fuel from the main tanks to the auxiliary tanks. Drain 9 gallons of fuel. Drain 12 gallons of fuel
Drain 9 gallons of fuel.
In order to be eligible for BasicMed privileges, the pilot in command must: Either hold or have held a valid medical certificate after July 14, 2006. Either hold or have held a valid medical certificate after April 1, 2016. Have a written statement of good health by a primary-care physician in the preceding 60 calendar months.
Either hold or have held a valid medical certificate after July 14, 2006.
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 temperatures expand 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
Pressure levels are raised on warm days and the indicated altitude is lower than true altitude.
If the pitot tube and outside static vents become clogged, which instruments would be affected? The altimeter, airspeed indicator, and turn-and-slip indicator. The altimeter, airspeed indicator, and vertical speed indicator. The altimeter, attitude indicator, and turn-and-slip indicator
The altimeter, airspeed indicator, and vertical speed indicator.
(Refer to figures 32, 33.) Determine if the airplane weight and balance is within limits. Front seat occupants: 415 lb Rear seat occupants: 110 lb Fuel, main tanks: 44 gal Fuel, aux. tanks: 19 gal Baggage: 32 lb Weight within limits, CG out of limits. 19 pounds overweight, CG out of limits forward. 19 pounds overweight, CG within limits.
Weight within limits, CG out of limits.
Under what condition is indicated altitude the same as true altitude? When at sea level under standard conditions.. If the altimeter has no mechanical error. When at 18,000 feet MSL with the altimeter set at 29.92.
When at sea level under standard conditions.
Aviation Routine Weather reports (METARs) contain: Wind, visibility, and precipitation only. Wind, visibility, precipitation, cloud coverage, temperature, and altimeter setting. Wind, visibility, precipitation, and temperature only.
Wind, visibility, precipitation, cloud coverage, temperature, and altimeter setting.
In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the east if a left turn is entered from a north heading an aircraft is decelerated while on a south heading. an aircraft is accelerated while on a north heading.
a left turn is entered from a north heading
In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if a left turn is entered from a north heading. a right turn is entered from a north heading. an aircraft is accelerated while on a north heading
a right turn is entered from a north heading.
In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward the north if an aircraft is accelerated while on an east or west heading.. an aircraft is decelerated while on an east or west heading. a left turn is entered from a west heading
an aircraft is accelerated while on an east or west heading.
In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate a turn toward the south. correctly when on a north or south heading. a turn momentarily.
correctly when on a north or south heading
Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates true altitude at field elevation. absolute altitude at field elevation. calibrated altitude at field elevation
true altitude at field elevation.