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Quiz 5

Quiz 5. Gleim, Sections 1, 2, 3. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability.

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Quiz 5

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1. Quiz 5 Gleim, Sections 1, 2, 3

2. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability. B. neutral longitudinal dynamic stability. C. positive longitudinal static stability.

3. 2. [21] Gleim #: 1.9.56 -- Source: PHAK Chap 3 Airplane wing loading during a level coordinated turn in smooth air depends upon the A. rate of turn. B. true airspeed. C. angle of bank.

4. 3. [24] Gleim #: 1.5.34 -- Source: FTH Chap 17 Lift on a wing is most properly defined as the A. reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber. B. force acting perpendicular to the relative wind. C. differential pressure acting perpendicular to the chord of the wing.

5. 4. [31] Gleim #: 1.8.49 -- Source: FTH Chap 17 While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will A. decrease the rate of turn resulting in a decreased load factor. B. decrease the rate of turn resulting in no change in load factor. C. increase the rate of turn resulting in no change in load factor.

6. 5. [35] Gleim #: 1.1.2 -- Source: PHAK Chap 4 Which is true regarding the use of flaps during level turns? A. The raising of flaps increases the stall speed. B. The lowering of flaps increases the stall speed. C. Raising flaps will require added forward pressure on the yoke or stick.

7. 6. [49] Gleim #: 2.4.16 -- Source: PHAK Chap 5 At high altitudes, an excessively rich mixture will cause the A. fouling of spark plugs. B. engine to overheat. C. engine to operate smoother even though fuel consumption is increased.

8. 7. [57] Gleim #: 2.6.28 -- Source: PHAK Chap 5 Detonation may occur at high-power settings when A. an excessively rich fuel mixture causes an explosive gain in power. B. the fuel mixture ignites instantaneously instead of burning progressively and evenly. C. the fuel mixture is ignited too early by hot carbon deposits in the cylinder.

9. 8. [69] Gleim #: 2.3.10 -- Source: PHAK Chap 6 What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments? A. It will not tumble as will vacuum-driven turn indicators. B. It is more reliable than the vacuum-driven indicators. C. It is a backup in case of vacuum system failure.

10. 9. [72] Gleim #: 2.2.8 -- Source: PHAK Chap 6 Calibrated airspeed is best described as indicated airspeed corrected for A. non-standard temperature. B. instrument error. C. installation and instrument error.

11. 10. [83] Gleim #: 2.1.1 -- Source: PHAK Chap 6 Which statement is true about magnetic deviation of a compass? Deviation A. varies for different headings of the same aircraft. B. varies over time as the agonic line shifts. C. is the same for all aircraft in the same locality.

12. 11. [87] Gleim #: 3.4.29 -- Source: FTH Chap 14 What is the general direction of movement of the other aircraft if during a night flight you observe a steady white light and a rotating red light ahead and at your altitude? The other aircraft is A. approaching you head-on. B. crossing to your left. C. headed away from you.

13. 12. [93] Gleim #: 3.4.30 -- Source: AIM Para 4-4-14 When in the vicinity of a VOR which is being used for navigation on VFR flight, it is important to A. pass the VOR on the right side of the radial to allow room for aircraft flying in the opposite direction on the same radial. B. exercise sustained vigilance to avoid aircraft that may be converging on the VOR from other directions. C. make 90° left and right turns to scan for other traffic.

14. 13. [98] Gleim #: 3.1.14 -- Source: FAR 91.157 To operate an airplane under SPECIAL VFR (SVFR) within Class D airspace at night, which is required? A. The pilot must hold an instrument rating, and the airplane must be equipped for instrument flight. B. The Class D airspace must be specifically designated as a night SVFR area. C. The pilot must hold an instrument rating, but the airplane need not be equipped for instrument flight, as long as the weather will remain at or above SVFR minimums.

15. 14. [112] Gleim #: 3.1.1 -- Source: FAR 91.135 Which is true regarding flight operations in Class A airspace? A. Aircraft must be equipped with approved distance measuring equipment (DME). B. Aircraft must be equipped with an approved ATC transponder. C. Must conduct operations under instrument flight rules.

16. 15. [143] Gleim #: 3.1.8 -- Source: FAR 91.117 Unless otherwise authorized or required by ATC, the maximum indicated airspeed permitted when at or below 2,500 feet AGL within 4 NM of the primary airport within Class C or D airspace is A. 180 knots. B. 230 knots. C. 200 knots.

17. Quiz 5 Five seconds each, review

18. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability. B. neutral longitudinal dynamic stability. C. positive longitudinal static stability.

19. 2. [21] Gleim #: 1.9.56 -- Source: PHAK Chap 3 Airplane wing loading during a level coordinated turn in smooth air depends upon the A. rate of turn. B. true airspeed. C. angle of bank.

20. 3. [24] Gleim #: 1.5.34 -- Source: FTH Chap 17 Lift on a wing is most properly defined as the A. reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber. B. force acting perpendicular to the relative wind. C. differential pressure acting perpendicular to the chord of the wing.

21. 4. [31] Gleim #: 1.8.49 -- Source: FTH Chap 17 While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will A. decrease the rate of turn resulting in a decreased load factor. B. decrease the rate of turn resulting in no change in load factor. C. increase the rate of turn resulting in no change in load factor.

22. 5. [35] Gleim #: 1.1.2 -- Source: PHAK Chap 4 Which is true regarding the use of flaps during level turns? A. The raising of flaps increases the stall speed. B. The lowering of flaps increases the stall speed. C. Raising flaps will require added forward pressure on the yoke or stick.

23. 6. [49] Gleim #: 2.4.16 -- Source: PHAK Chap 5 At high altitudes, an excessively rich mixture will cause the A. fouling of spark plugs. B. engine to overheat. C. engine to operate smoother even though fuel consumption is increased.

24. 7. [57] Gleim #: 2.6.28 -- Source: PHAK Chap 5 Detonation may occur at high-power settings when A. an excessively rich fuel mixture causes an explosive gain in power. B. the fuel mixture ignites instantaneously instead of burning progressively and evenly. C. the fuel mixture is ignited too early by hot carbon deposits in the cylinder.

25. 8. [69] Gleim #: 2.3.10 -- Source: PHAK Chap 6 What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments? A. It will not tumble as will vacuum-driven turn indicators. B. It is more reliable than the vacuum-driven indicators. C. It is a backup in case of vacuum system failure.

26. 9. [72] Gleim #: 2.2.8 -- Source: PHAK Chap 6 Calibrated airspeed is best described as indicated airspeed corrected for A. non-standard temperature. B. instrument error. C. installation and instrument error.

27. 10. [83] Gleim #: 2.1.1 -- Source: PHAK Chap 6 Which statement is true about magnetic deviation of a compass? Deviation A. varies for different headings of the same aircraft. B. varies over time as the agonic line shifts. C. is the same for all aircraft in the same locality.

28. 11. [87] Gleim #: 3.4.29 -- Source: FTH Chap 14 What is the general direction of movement of the other aircraft if during a night flight you observe a steady white light and a rotating red light ahead and at your altitude? The other aircraft is A. approaching you head-on. B. crossing to your left. C. headed away from you.

29. 12. [93] Gleim #: 3.4.30 -- Source: AIM Para 4-4-14 When in the vicinity of a VOR which is being used for navigation on VFR flight, it is important to A. pass the VOR on the right side of the radial to allow room for aircraft flying in the opposite direction on the same radial. B. exercise sustained vigilance to avoid aircraft that may be converging on the VOR from other directions. C. make 90° left and right turns to scan for other traffic.

30. 13. [98] Gleim #: 3.1.14 -- Source: FAR 91.157 To operate an airplane under SPECIAL VFR (SVFR) within Class D airspace at night, which is required? A. The pilot must hold an instrument rating, and the airplane must be equipped for instrument flight. B. The Class D airspace must be specifically designated as a night SVFR area. C. The pilot must hold an instrument rating, but the airplane need not be equipped for instrument flight, as long as the weather will remain at or above SVFR minimums.

31. 14. [112] Gleim #: 3.1.1 -- Source: FAR 91.135 Which is true regarding flight operations in Class A airspace? A. Aircraft must be equipped with approved distance measuring equipment (DME). B. Aircraft must be equipped with an approved ATC transponder. C. Must conduct operations under instrument flight rules.

32. 15. [143] Gleim #: 3.1.8 -- Source: FAR 91.117 Unless otherwise authorized or required by ATC, the maximum indicated airspeed permitted when at or below 2,500 feet AGL within 4 NM of the primary airport within Class C or D airspace is A. 180 knots. B. 230 knots. C. 200 knots.

34. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability. B. neutral longitudinal dynamic stability. C. positive longitudinal static stability.

35. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability. B. neutral longitudinal dynamic stability. C. positive longitudinal static stability.

36. 2. [21] Gleim #: 1.9.56 -- Source: PHAK Chap 3 Airplane wing loading during a level coordinated turn in smooth air depends upon the A. rate of turn. B. true airspeed. C. angle of bank.

37. 2. [21] Gleim #: 1.9.56 -- Source: PHAK Chap 3 Airplane wing loading during a level coordinated turn in smooth air depends upon the A. rate of turn. B. true airspeed. C. angle of bank.

38. 3. [24] Gleim #: 1.5.34 -- Source: FTH Chap 17 Lift on a wing is most properly defined as the A. reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber. B. force acting perpendicular to the relative wind. C. differential pressure acting perpendicular to the chord of the wing.

39. 3. [24] Gleim #: 1.5.34 -- Source: FTH Chap 17 Lift on a wing is most properly defined as the A. reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber. B. force acting perpendicular to the relative wind. C. differential pressure acting perpendicular to the chord of the wing.

40. 4. [31] Gleim #: 1.8.49 -- Source: FTH Chap 17 While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will A. decrease the rate of turn resulting in a decreased load factor. B. decrease the rate of turn resulting in no change in load factor. C. increase the rate of turn resulting in no change in load factor.

41. 4. [31] Gleim #: 1.8.49 -- Source: FTH Chap 17 While maintaining a constant angle of bank and altitude in a coordinated turn, an increase in airspeed will A. decrease the rate of turn resulting in a decreased load factor. B. decrease the rate of turn resulting in no change in load factor. C. increase the rate of turn resulting in no change in load factor.

42. 5. [35] Gleim #: 1.1.2 -- Source: PHAK Chap 4 Which is true regarding the use of flaps during level turns? A. The raising of flaps increases the stall speed. B. The lowering of flaps increases the stall speed. C. Raising flaps will require added forward pressure on the yoke or stick.

43. 5. [35] Gleim #: 1.1.2 -- Source: PHAK Chap 4 Which is true regarding the use of flaps during level turns? A. The raising of flaps increases the stall speed. B. The lowering of flaps increases the stall speed. C. Raising flaps will require added forward pressure on the yoke or stick.

44. 6. [49] Gleim #: 2.4.16 -- Source: PHAK Chap 5 At high altitudes, an excessively rich mixture will cause the A. fouling of spark plugs. B. engine to overheat. C. engine to operate smoother even though fuel consumption is increased.

45. 6. [49] Gleim #: 2.4.16 -- Source: PHAK Chap 5 At high altitudes, an excessively rich mixture will cause the A. fouling of spark plugs. B. engine to overheat. C. engine to operate smoother even though fuel consumption is increased.

46. 7. [57] Gleim #: 2.6.28 -- Source: PHAK Chap 5 Detonation may occur at high-power settings when A. an excessively rich fuel mixture causes an explosive gain in power. B. the fuel mixture ignites instantaneously instead of burning progressively and evenly. C. the fuel mixture is ignited too early by hot carbon deposits in the cylinder.

47. 7. [57] Gleim #: 2.6.28 -- Source: PHAK Chap 5 Detonation may occur at high-power settings when A. an excessively rich fuel mixture causes an explosive gain in power. B. the fuel mixture ignites instantaneously instead of burning progressively and evenly. C. the fuel mixture is ignited too early by hot carbon deposits in the cylinder.

48. 8. [69] Gleim #: 2.3.10 -- Source: PHAK Chap 6 What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments? A. It will not tumble as will vacuum-driven turn indicators. B. It is more reliable than the vacuum-driven indicators. C. It is a backup in case of vacuum system failure.

49. 8. [69] Gleim #: 2.3.10 -- Source: PHAK Chap 6 What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments? A. It will not tumble as will vacuum-driven turn indicators. B. It is more reliable than the vacuum-driven indicators. C. It is a backup in case of vacuum system failure.

50. 9. [72] Gleim #: 2.2.8 -- Source: PHAK Chap 6 Calibrated airspeed is best described as indicated airspeed corrected for A. non-standard temperature. B. instrument error. C. installation and instrument error.

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