Private Pilot - Flight Instruments.txt

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lukemlj
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224981
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Private Pilot - Flight Instruments.txt
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2013-06-25 08:30:07
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Private Pilot Flight Instruments
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Private Pilot - Flight Instruments
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  1. Private Pilot - Flight Instruments
    2013
  2. 3248. Which instrument will become inoperative if the pitot tube becomes clogged?
    Airspeed
  3. 3249. Which instrument(s) will become inoperative if the static vents become clogged?
    Airspeed, altimeter, and vertical speed.
  4. 3247. If the pitot tube and outside static vents become clogged, which instruments would be affected?
    The altimeter, airspeed indicator, and vertical speed indicator.
  5. 3262. The pitot system provides impact pressure for which instrument?
    Airspeed indicator.
  6. 3006. Which V-speed represents maneuvering speed?
    V_A
  7. 3264. What does the red line on an airspeed indicator represent?
    Never-exceed speed.
  8. 3268. (Refer to Figure 4.) Which color identifies the never-exceed speed?
    The red radial line.
  9. 3268. (Refer to Figure 4.) Which color identifies the power-off stalling speed in a specified configuration?
    Lower limit of the green arc.
  10. 3011. Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff?
    V_X
  11. 3012-1. After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?
    V_Y
  12. 3265. (Refer to Figure 4.) What is the full flap operating range for the airplane?
    60 to 100 MPH
  13. 3267. (Refer to Figure 4.) The maximum speed at which the airplane can be operated in smooth air is ___
    208 MPH
  14. 3270. (Refer to Figure 4.) What is the maximum flaps-extended speed?
    100 MPH
  15. 3271. (Refer to Figure 4.) Which color identifies the normal flap operating range?
    The white arc.
  16. 3272. (Refer to Figure 4.) Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration?
    Lower limit of the white arc.
  17. 3273. (Refer to Figure 4.) What is the maximum structural cruising speed?
    165 MPH
  18. 3274. What is an important airspeed limitation that is not color coded on airspeed indicators?
    Maneuvering speed.
  19. 3007. Which V-speed represents maximum flap extended speed?
    V_FE
  20. 3008. Which V-speed represents maximum landing gear extended speed?
    V_LE
  21. 3009. V_NO is defined as the ___
    maximum structural cruising speed.
  22. 3010. V_S0 is defined as the ___
    stalling speed or minimum steady flight speed in the landing configuration.
  23. 3266. (Refer to Figure 4.) What is the caution range of the airplane?
    165 to 208 MPH.
  24. 3105. If an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter?
    The elevation of the departure area.
  25. 3106. 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.
  26. 3107. At what altitude shall the altimeter be set to 29.92, when climbing to cruising flight level?
    18,000 feet MSL
  27. 3254. 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.
  28. 3255. How do variations in temperature affect the altimeter?
    Pressure leveles are raised on warm days and the indicated altitude is lower than true altitude.
  29. 3256. What is true altitude?
    The vertical distance of the aircraft above sea level.
  30. 3392. Under what condition will true altitude be lower than indicated altitude?
    In colder than standard air temperature.
  31. 3257. What is absolute altitude?
    The vertical distance of the aircraft above the surface.
  32. 3258. What is density altitude?
    The pressure altitude corrected for nonstandard temperature.
  33. 3259. What is pressure altitude?
    The altitude indicated when the barometric pressure scale is set to 29.92.
  34. 3260. Under what condition is indicated altitude the same as true altitude?
    When at sea level under standard conditions.
  35. 3261. If it is necessary to set the altimeter from 29.15 to 29.85, what change occurs?
    700-foot increase in indicated altitude.
  36. 3388. Under which condition will pressure altitude be equal to true altitude?
    When standard atmospheric conditions exist.
  37. 3389. Under what condition is pressure altitude and density altitude the same value?
    At standard temperature.
  38. 3390. 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.
  39. 3391. 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 ___
    higher than the actual altitude above sea level.
  40. 3393. Which condition would cause the altimeter to indicate a lower altitude than true altitude?
    Air temperature warmer than standard.
  41. 3250. (Refer to Figure 3.) Altimeter 1 indicates ___
    1500 feet.
  42. 3250. (Refer to Figure 3.) Altimeter 2 indicates ___
    14,500 feet.
  43. 3250. (Refer to Figure 3.) Altimeter 3 indicates ___
    9,500 feet.
  44. 3250. (Refer to Figure 3.) Which altimeter(s) indicate(s) more than 10,000 feet?
    1 and 2 only.
  45. 3387. If a pilot changes the altimeter setting from 30.11 to 29.96, what is the approximate change in indication?
    150 feet lower.
  46. 3278. (Refer to Figure 7.) How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated?
    By the relationship of the miniature airplane (C) to the deflected horizon (B).
  47. 3275. (Refer to Figure 5.) A turn coordinator provides an indication of the ___
    movement of the aircraft about the yaw and roll axis.
  48. 3277. (Refer to Figure 7.) The proper adjustment to make on the attitude indicator during level flight is to align the ___
    miniature airplane to the horizon bar
  49. 3276. (Refer to Figure 6.) To receive accurate indications during flight from a heading indicator, the instrument must be ___
    periodically realigned with the magnetic compass as the gyro precesses.
  50. 3279. Deviation in a magnetic compass is caused by the ___
    magnetic fields within the aircraft distorting the lines of magnetic force.
  51. 3279-1. The angular difference between true north and magnetic north is ___
    magnetic variation
  52. 3282. 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.
  53. 3283. In the Northern Hemisphere, the magnetic compass will normally indicate a turn toward the south when ___
    an aircraft is decelerated while on an east or west heading.
  54. 3283-1. What should be the indication on the magnetic compass as you roll into a standard rate turn to the right from a south heading in the Northern Hemisphere?
    The compass will indicate a turn to the right, but at a faster rate than is actually occuring.
  55. 3284. In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate ___
    correctly while on a north or south heading.
  56. 3280. In the Northern Hemisphere, a magnetic compass will normally indicate initially a turn toward the west if ___
    a right turn is entered from a north heading.
  57. 3281. 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.
  58. 3286. During flight, when are the indications of a magnetic compass accurate?
    Only in straight-and-level unaccelerated flight.

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