Flight Instruments Chapter 2 Section C
Settings
Private Pilot Flight Instruments Chapter 2 Section C
- 1.2-34 Which V-speed represents maneuvering speed?
- A.
Va
- B.
Vlo
- C.
Vne
- 2.2-35If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter.
- A.
The elevation of the nearest airport corrected to mean sea level.
- B.
The elevation of the departure area
- C.
Pressure altitude corrected for nonstandard temperature
- 3.2-36Prior to take off, the altimeter should be set to which altitude or altimeter setting?
- A.
The current local altimeter setting, if available, or the departure airport elevation.
- B.
The corrected density altitude of the departure airport.
- C.
THe corrected pressure altitude for the departure airport.
- 4.2-37If the pitot tube and outside static vents become clogged, which instruments would be affected
- A.
The altimeter, airspeed indicator, and turn-and-slip indicator
- B.
The altimeter, airspeed indicator, and vertical speed indicator
- C.
The altimeter, attitude indicator, and turn-and-slip indicator
- 5.2-38Which instrument will become inoperative if the pitot tube becomes clogged?
- A.
Altimeter
- B.
Vertical Speed
- C.
Airspeed
- 6.2-39Which instrument(s) will become inoperative if the static vents become clogged?
- A.
Airspeed only
- B.
Altimeter only
- C.
Airspeed, altimeter, and vertical speed
- 7.
![2-40 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 1 indicates - ProProfs]( "2-40 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 1 indicates")
2-40 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 1 indicates- A.
500 Feet
- B.
1,500 Feet
- C.
10,500 feet
- 8.
![2-41 2-41Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 2 indicates - ProProfs]( "2-41 2-41Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 2 indicates")
2-41 2-41Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 2 indicates- A.
1,500 feet
- B.
4,500 feet
- C.
14,500 feet
- 9.
![2-42 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 3 indicates - ProProfs]( "2-42 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 3 indicates")
2-42 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Altimeter 3 indicates- A.
9,500 feet
- B.
10,950 feet
- C.
15,940 feet
- 10.
![2-43 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Which altimeter(s) indicate(s) more than 10,000 feet - ProProfs]( "2-43 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Which altimeter(s) indicate(s) more than 10,000 feet")
2-43 - Figure 3 Page 2-13 Test Guide(Refer to figure 3. Which altimeter(s) indicate(s) more than 10,000 feet- A.
1,2, and 3
- B.
1 and 2 only
- C.
1 only
- 11.2-44Altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates
- A.
Calibrated altitude at field elevation
- B.
Absolute altitude at field elevation
- C.
True altitude at field elevation
- 12.2-45How do variations in temperature affect the altimeter
- A.
Pressure levels are raised on warm days and the indicated altitude is lower than true altitude
- B.
Higher temperatures expand the pressure levels and the indicated altitude is higher than ture altitude
- C.
Lower temperatures lower the pressure levels and the indicated altitude is higher than true altitude
- 13.2-46What is true altitude
- A.
The vertical distance of the aircraft above sea level
- B.
The vertical distance of the aircraft above the surface
- C.
The height above the standard datum plane
- 14.2-47What is absolute altitude
- A.
The altitude read directly from the altimeter
- B.
The vertical distance of the aircraft above the surface
- C.
The height above the standard datum plane
- 15.2-48What is density altitude
- A.
The height above the standard datum plane
- B.
The pressure altitude corrected for nonstandard temperature.
- C.
The altitude read directly from the altimeter
- 16.2-49What is pressure altitude?
- A.
The indicated altitude corrected for position and installation error.
- B.
The altitude indicated when teh barometeric pressure scale is set to 29.92
- C.
The indicated altitude corrected for nonstandard temperature and pressure
- 17.2-50Under what condition is indicated altitude the same as true altitude.
- A.
If the altimeter has no mechanical error.
- B.
When at sea level under standard conditions
- C.
When at 18,000 feet MSL with the altimeter set at 29.92
- 18.2-51If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs
- A.
70-foot increase in indicated altitude
- B.
70-foot increase in density altitude
- C.
700-foot increase in indicated altitude
- 19.2-52The pitot system provides impact pressure for which instrument
- A.
Altimeter
- B.
Vertical-speed indicator
- C.
Airspeed indicator
- 20.2-53As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will
- A.
Decrease as the true airspeed decreases
- B.
Decrease as the true airspeed increases
- C.
Remain the same regardless of altitude.
- 21.
![2-54What does the red line on an airspeed indicator represent? - ProProfs]( "2-54What does the red line on an airspeed indicator represent?")
2-54What does the red line on an airspeed indicator represent?- A.
Maneuvering Speed
- B.
Turbulence or rough-air speed.
- C.
Never-exceed speed
- 22.
![2-55(Refer to figure 4 on page 2-17.) What is the full flap operating range for the airplane? full flap operating range for the airplane? - ProProfs]( "2-55(Refer to figure 4 on page 2-17.) What is the full flap operating range for the airplane? full flap operating range for the airplane?")
2-55(Refer to figure 4 on page 2-17.) What is the full flap operating range for the airplane? full flap operating range for the airplane?- A.
60 to 100 MPH
- B.
60 - 208 MPH
- C.
65 to 165 MPH
- 23.
![2 - 56What is the caution range of the airplane? - ProProfs]( "2 - 56What is the caution range of the airplane?")
2 - 56What is the caution range of the airplane?- A.
0 to 60 MPH
- B.
100 to 165 MPH
- C.
165 to 208 MPH
- 24.
![2 - 57The maximum speed at which the airplane can be operated in smooth air is - ProProfs]( "2 - 57The maximum speed at which the airplane can be operated in smooth air is")
2 - 57The maximum speed at which the airplane can be operated in smooth air is- A.
100 MPH
- B.
165 MPH
- C.
208 MPH
- 25.
![2-58Which color identifies the never-exceed speed? - ProProfs]( "2-58Which color identifies the never-exceed speed?")
2-58Which color identifies the never-exceed speed?- A.
Lower limit of the yellow arc.
- B.
Upper limit of the white arc.
- C.
The red radial line.
Back to top