## FAA Knowledge Test

Last update by Bruno on 11/06/2014
1486770 People have viewed this Quiz

# (Refer to figure 8 on page 159.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97.

1,341 feet MSL.

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• Answered in FAA Knowledge Test
(Refer to figure 8 on page 159.) What is the effect of a temperature increase from 25 to 50 degrees F on the density altitude if the pressure altitude remains at 5,000 feet?
1,650-foot increase.
• Answered in FAA Knowledge Test
(Refer to Figure 8 on page 159.) Determine the pressure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22 at standard temperature.
2.991 feet MSL.
• Answered in FAA Knowledge Test
(Refer to Figure 8 on pg 159.) Determine the density altitude for these conditions:
Altimeter setting: 29.25
Runway temperature: +81 degrees F
Airport elevation: 5,250 ft MSL
8500 feet.
• Answered in FAA Knowledge Test
(Refer to figure 41 on pg. 161.) Determine the total distance required for takeoff to clear a 50-foot obstacle:
OAT: Std
Pressure altitude: 4000 ft
Takeoff weight: 2800 lb
1750 feet.
• Answered in FAA Knowledge Test
(Refer to Figure 41 on pg. 161.) Determine the total distance required for takeoff to clear a 50-foot obstacle.
OAT: Std
Pressure altitude: Sea level
Takeoff Weight: 2,700 lb
1,400 feet.
• Answered in FAA Knowledge Test
(Refer to Figure 36 on pg 163.) What fuel flow should a pilot expect at 11,000 feet on a std day with 65% max continuous power?
11.2 gallons per hour.
• Answered in FAA Knowledge Test
(Refer to Figure 36 on pg. 163.) What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions?
Pressure Altitude: 8,000 ft
Temperature: 22 degrees C
Manifold Pressure: 20.8" Hg
Wind: Calm
70.1 gallons (Use the chart and find the Pressure alt and then go to the right to find the KTS and Fuel flow (1000 NM / 164 knots = 6.09 hr > multiply 6.09 by 11.5 (which is the GPH of fuel flow) and you get 70.1 gallons.)
• Answered in FAA Knowledge Test
(Refer to Figure 36 on pg 161.) What is the expected fuel consumption for a 500 NM flight under the following conditions?
Pressure altitude: 4000 ft
Temperature: +29 degrees C
Wind: Calm
36.1 gallons
• Answered in FAA Knowledge Test
(Refer to Figure 36 on pg. 161.) Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65% max continuous power at 6500 feet with a temp. of 36 degrees F higher than std.
21.0" Hg
• Answered in FAA Knowledge Test
(Refer to Figure 36 on pg. 161.) Approximately what true airspeed should a pilot expect with 65 percent max continuous power at 9500 feet with a temp. of 36 degrees below standard?
183 MPH.
• Answered in FAA Knowledge Test
(Refer to figure 37 on pg. 164.) What is the crosswind component for a landing on runway 18 if the tower reports the wind as 220 degrees at 30 knots?
19 knots.
FAA Knowledge Test
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