cfi Airplane Instruments, Engines, and Systems
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Question 1 of 97
1. Question
Deviation error of the magnetic compass is caused by
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Question 2 of 97
2. Question
Which statement is true about magnetic deviation of a compass
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Question 3 of 97
3. Question
In the Northern Hemisphere, a magnetic compass will normally indicate a turn toward the north if
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Question 4 of 97
4. Question
In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate
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Question 5 of 97
5. Question
In the Northern Hemisphere, which would be correct about starting the rollout from a turn using a magnetic compass? Start the rollout
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Question 6 of 97
6. Question
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?
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Question 7 of 97
7. Question
Which instrument would be affected by excessively low pressure in the airplane’s vacuum system?
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Question 8 of 97
8. Question
If both the ram-air input and drain hole of the pitot system are blocked, what airspeed indication can be expected?
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Question 9 of 97
9. Question
The Pitot system provides impact pressure for which instrument?
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Question 10 of 97
10. Question
Pitot-static system errors are generally the greatest in which range of airspeed?
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Question 11 of 97
11. Question
During power-off stalls with flaps full down, the stall occurs and the pointer on the airspeed indicator shows a speed less than the minimum limit of the white arc on the indicator. This is most probably due to
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Question 12 of 97
12. Question
If a pitot tube is clogged, which instrument would be affected?
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Question 13 of 97
13. Question
What does the lower limit of the white arc on an airspeed indicator represent?
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Question 14 of 97
14. Question
What does the lower limit of the green arc on an airspeed indicator represent?
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Question 15 of 97
15. Question
What airspeed indicator marking identifies the maximum structural cruising speed of an aircraft?
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Question 16 of 97
16. Question
Which airspeed is identified by color coding on an airspeed indicator?
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Question 17 of 97
17. Question
What is an important airspeed limitation not color coded on airspeed indicators?
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Question 18 of 97
18. Question
If the static pressure tubes are broken inside a pressurized cabin during a high-altitude flight, the altimeter would probably indicate
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Question 19 of 97
19. Question
Which statement is true about the effect of temperature changes on the indications of a sensitive altimeter?
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Question 20 of 97
20. Question
A possible result of using the emergency alternate source of static pressure inside the cabin of an unpressurized airplane is the
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Question 21 of 97
21. Question
Excessively high engine temperatures, either in the air or on the ground, will
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Question 22 of 97
22. Question
What action can a pilot take to aid in cooling an engine that is overheating during a climb?
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Question 23 of 97
23. Question
Excessively high engine temperatures will
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Question 24 of 97
24. Question
An abnormally high engine oil temperature indication may be caused by
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Question 25 of 97
25. Question
For internal cooling, air-cooled engines are especially dependent on
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Question 26 of 97
26. Question
If, during flight, you notice that the cylinder head temperature (CHT) indication exceeds the normal operating range, how would you proceed to cool the engine?
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Question 27 of 97
27. Question
If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, you may have been
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Question 28 of 97
28. Question
An abnormally high engine oil temperature indication may be caused by
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Question 29 of 97
29. Question
Air cooled engines dissipate heat
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Question 30 of 97
30. Question
Coolant in a liquid cooled engine is normally circulated by
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Question 31 of 97
31. Question
What is the primary advantage of a constant speed propeller?
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Question 32 of 97
32. Question
To absorb maximum engine power and to develop maximum thrust, a constant-speed propeller should be adjusted to a blade angle which will produce a
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Question 33 of 97
33. Question
When operating an aircraft with a constant-speed propeller, which procedure places the least stress on cylinder components?
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Question 34 of 97
34. Question
Which statement is true regarding propeller efficiency? Propeller efficiency is the
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Question 35 of 97
35. Question
The distance a propeller actually advances in one revolution is
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Question 36 of 97
36. Question
Propeller slip is the difference between the
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Question 37 of 97
37. Question
Blade angle of a propeller is defined as the angle between the
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Question 38 of 97
38. Question
The reason for variations in geometric pitch (twisting) along a propeller blade is that it
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Question 39 of 97
39. Question
Prior to starting the engine, the manifold pressure gauge usually indicates approximately 29″ Hg. This is because the
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Question 40 of 97
40. Question
In addition to an added safety factor, dual ignition systems also provide
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Question 41 of 97
41. Question
If the ground wire between the magneto and the ignition switch becomes disconnected, the most noticeable result will be that the engine
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Question 42 of 97
42. Question
What should be the first action after starting an aircraft engine?
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Question 43 of 97
43. Question
If the ground wire between the magneto and the ignition switch becomes disconnected, the engine
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Question 44 of 97
44. Question
Fuel injection systems, compared to carburetor systems, are generally considered to be
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Question 45 of 97
45. Question
The operating principle of float-type carburetors is based on the
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Question 46 of 97
46. Question
One advantage of fuel injection systems over carburetor systems is
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Question 47 of 97
47. Question
The presence of carburetor ice in an aircraft equipped with a fixed-pitch propeller can be verified by applying carburetor heat and noting
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Question 48 of 97
48. Question
The first indication of carburetor ice in an aircraft with a fixed-pitch propeller is
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Question 49 of 97
49. Question
Which condition is most favorable to the development of carburetor icing?
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Question 50 of 97
50. Question
The first indication of carburetor icing in an aircraft equipped with a constant-speed propeller would most likely be a
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Question 51 of 97
51. Question
Concerning carburetor icing, which statement is true?
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Question 52 of 97
52. Question
The low temperature that causes carburetor ice in an engine equipped with a float-type carburetor is normally the result of the
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Question 53 of 97
53. Question
Generally speaking, the use of carburetor heat tends to
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Question 54 of 97
54. Question
In an aircraft equipped with a fixed-pitch propeller and a float-type carburetor, the first indication of carburetor ice would most likely be
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Question 55 of 97
55. Question
Carburetor ice
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Question 56 of 97
56. Question
Leaving the carburetor heat on during takeoff
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Question 57 of 97
57. Question
What energy source is used to drive the turbine of a turbocharged airplane?
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Question 58 of 97
58. Question
During climbing flight using a turbocharged airplane, the manifold pressure will remain approximately constant until the
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Question 59 of 97
59. Question
During which stroke of a reciprocating engine is the gaseous mixture expanding within the cylinder?
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Question 60 of 97
60. Question
Fuel and exhaust enter and exit a 4-cycle engine
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Question 61 of 97
61. Question
Four-cycle engines are lubricated by
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Question 62 of 97
62. Question
Many 4-cycle engines utilize what type of lubrication system?
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Question 63 of 97
63. Question
Which statement is true regarding fouling of the spark plugs of an aircraft engine?
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Question 64 of 97
64. Question
Fuel/air ratio is the ratio between the
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Question 65 of 97
65. Question
Proper mixture control and better economy in the operation of a fuel injected engine can be achieved best by use of
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Question 66 of 97
66. Question
The main purpose of the mixture control is to
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Question 67 of 97
67. Question
When the pilot leans the mixture control, what is being accomplished?
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Question 68 of 97
68. Question
The best power mixture is that fuel/air ratio at which
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Question 69 of 97
69. Question
As flight altitude increases, what will occur if no leaning is made with the mixture control?
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Question 70 of 97
70. Question
The basic purpose of adjusting the fuel/air mixture control at altitude is to
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Question 71 of 97
71. Question
The pilot controls the air/fuel ratio with the
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Question 72 of 97
72. Question
At high altitudes, an excessively rich mixture will cause the
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Question 73 of 97
73. Question
Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel
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Question 74 of 97
74. Question
Fouling of spark plugs is more apt to occur if the aircraft
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Question 75 of 97
75. Question
What is the main reason fuel tank vents must be open? To allow
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Question 76 of 97
76. Question
During preflight, the fuel vent system should always be checked
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Question 77 of 97
77. Question
Detonation in an aircraft engine is most likely to occur whenever the
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Question 78 of 97
78. Question
The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as
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Question 79 of 97
79. Question
If the grade of fuel used in an aircraft engine is lower than that specified, it may cause
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Question 80 of 97
80. Question
Detonation occurs at high power settings when the
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Question 81 of 97
81. Question
If a pilot suspects that the engine (with a fixed pitch propeller) is detonating during climb-out after takeoff, the initial corrective action to take would be to
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Question 82 of 97
82. Question
Detonation occurs in a reciprocating aircraft engine when
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Question 83 of 97
83. Question
Detonation can be caused by
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Question 84 of 97
84. Question
Detonation occurs in a reciprocating aircraft engine when
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Question 85 of 97
85. Question
To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the
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Question 86 of 97
86. Question
The amount of water absorbed in aviation fuels will
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Question 87 of 97
87. Question
Running a fuel tank dry before switching tanks is not a good practice because
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Question 88 of 97
88. Question
When refueling aircraft, which precaution would be adequate for eliminating the potential hazard of static electricity?
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Question 89 of 97
89. Question
Concerning the advantages of an aircraft generator or alternator, select the true statement.
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Question 90 of 97
90. Question
An electrical system failure (battery and alternator) occurs during flight. In this situation, you would
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Question 91 of 97
91. Question
What precautions should be taken with respect to aircraft oxygen systems?
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Question 92 of 97
92. Question
What type of oxygen should be used to replenish an aircraft oxygen system?
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Question 93 of 97
93. Question
What type of oxygen system is most commonly found in general aviation aircraft?
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Question 94 of 97
94. Question
What is the purpose of the rebreather bag on an oxygen mask in a continuous-flow system?
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Question 95 of 97
95. Question
Which statement is true regarding preheating of an aircraft during cold-weather operations?
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Question 96 of 97
96. Question
Crankcase breather lines of an aircraft engine should receive special attention during preflight in cold weather because they are susceptible to being clogged by
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Question 97 of 97
97. Question
During preflight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by
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