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Question 1 of 54
1. Question
Which unit most accurately indicates fuel consumption of a reciprocating engine?
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Question 2 of 54
2. Question
The fuel flowmeter used with a continuous-fuel injection system installed on an aircraft horizontally opposed reciprocating engines measures the fuel pressure drop across the
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Question 3 of 54
3. Question
The principal fault in the pressure type fuel flowmeter indicating system, installed on a horizontally opposed continuous-flow fuel injected aircraft reciprocating engine, is that a plugged fuel injection nozzle will cause a
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Question 4 of 54
4. Question
Motor-driven impeller and turbine fuel flow transmitters are designed to transmit data
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Question 5 of 54
5. Question
The fuel flowmeter indicator rotor and needle for a motor-impeller and turbine indicating system is driven by
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Question 6 of 54
6. Question
On a twin-engine aircraft with fuel-injected reciprocating engines, one fuel flowmeter reads considerably higher than the other in all engine operating configurations. What is the probable cause of this indication?
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Question 7 of 54
7. Question
The fuel flow indication system used with many fuel-injected opposed engine airplanes utilizes a measure of
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Question 8 of 54
8. Question
In addition to fuel quantity, a computerized fuel system (CFS) with a totalizer-indicator provides indication of how many of the following?
- Fuel flow rate.
- Fuel used since reset or initial start-up.
- Fuel time remaining at current power setting.
- Fuel temperature.
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Question 9 of 54
9. Question
The fuel low indication data sent from motor driven impeller and turbine, and motorless type fuel flow transmitters is a measure of
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Question 10 of 54
10. Question
In an aircraft equipped with a pressure-drop type fuel flow indicating system, if one of the injector nozzles becomes restricted, this would cause a decrease in fuel flow with
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Question 11 of 54
11. Question
A manifold pressure gauge is designed to
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Question 12 of 54
12. Question
The purpose of an exhaust gas analyzer is to indicate the
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Question 13 of 54
13. Question
Which of the following types of electric motors are commonly used in electric tachometers?
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Question 14 of 54
14. Question
Where are the hot and cold junctions located in an engine cylinder temperature indicating system?
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Question 15 of 54
15. Question
Basically, the indicator of a tachometer system is responsive to change in
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Question 16 of 54
16. Question
Which statement is correct concerning a thermocouple-type temperature indicating instrument system?
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Question 17 of 54
17. Question
Which statement is true regarding a thermocouple-type cylinder head temperature measuring system?
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Question 18 of 54
18. Question
What basic meter is used to indicate cylinder head temperature in most aircraft?
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Question 19 of 54
19. Question
Which of the following is a primary engine instrument?
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Question 20 of 54
20. Question
A complete break in the line between the manifold pressure gauge and the induction system will be indicated by the gauge registering
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Question 21 of 54
21. Question
Engine oil temperature gauges indicate the temperature of the oil
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Question 22 of 54
22. Question
Why do helicopters require a minimum of two synchronous tachometer systems?
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Question 23 of 54
23. Question
If the thermocouple leads were inadvertently crossed at installation, what would the cylinder temperature gauge pointer indicate?
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Question 24 of 54
24. Question
A common type of electrically operated oil temperature gauge utilizes
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Question 25 of 54
25. Question
The indication on a thermocouple-type cylinder head temperature indicator is produced by
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Question 26 of 54
26. Question
(1) Powerplant instrument range markings show whether the current state of powerplant operation is normal, acceptable for a limited time, or unauthorized.
(2) Powerplant instrument range markings are based on installed engine operating limits which may not exceed (but are not necessarily equal to) those limits shown on the engine Type Certificate Data Sheet.
Regarding the above statements,
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Question 27 of 54
27. Question
Thermocouple leads
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Question 28 of 54
28. Question
The thermocouple leads used to measure cylinder temperature on an aircraft reciprocating engine
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Question 29 of 54
29. Question
(1) Engine pressure ratio (EPR) is a ratio of the exhaust gas pressure to the engine inlet air pressure, and indicates the thrust produced.
(2) Engine pressure ratio (EPR) is a ratio of the exhaust gas pressure to the engine inlet air pressure, and indicates volumetric efficiency.
Regarding the above statements,
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Question 30 of 54
30. Question
What unit in a tachometer system sends information to the indicator?
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Question 31 of 54
31. Question
(1) Generally, when a turbine engine indicates high EGT for a particular EPR (when there is no significant damage), it means that the engine is out of trim.
(2) Some turbine-powered aircraft use RPM as the primary indicator of thrust produced, others use EPR as the primary indicator.
Regarding the above statements,
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Question 32 of 54
32. Question
Engine pressure ratio is determined by
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Question 33 of 54
33. Question
Turbine engine EGT thermocouples are constructed of
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Question 34 of 54
34. Question
Which of the following instrument discrepancies require replacement of the instrument?
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Question 35 of 54
35. Question
A Bourdon-tube instrument may be used to indicate
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Question 36 of 54
36. Question
An indication of unregulated power changes that result in continual drift of manifold pressure indication on a turbo supercharged aircraft engine is known as
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Question 37 of 54
37. Question
Which of the following instrument conditions is acceptable and does not require immediate correction?
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Question 38 of 54
38. Question
A change in engine manifold pressure has a direct effect on the
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Question 39 of 54
39. Question
What instrument on a gas turbine engine should be monitored to minimize the possibility of a “hot” start?
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Question 40 of 54
40. Question
In regard to using a turbine engine oil analysis program, which of the following is NOT true?
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Question 41 of 54
41. Question
On an aircraft turbine engine, operating at a constant power, the application of engine anti-icing will result in
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Question 42 of 54
42. Question
Engine pressure ratio is the total pressure ratio between the
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Question 43 of 54
43. Question
What would be the possible cause if a gas turbine engine has high exhaust gas temperature, high fuel flow, and low RPM at all engine power settings?
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Question 44 of 54
44. Question
What is the primary purpose of the tachometer on an axial-compressor turbine engine?
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Question 45 of 54
45. Question
The engine pressure ratio (EPR) indicator is a direct indication of
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Question 46 of 54
46. Question
The exhaust gas temperature (EGT) indicator on a gas turbine engine provides a relative indication of the
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Question 47 of 54
47. Question
What instrument indicates the thrust of a gas turbine engine?
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Question 48 of 54
48. Question
In a turbine engine, where is the turbine discharge pressure indicator sensor located?
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Question 49 of 54
49. Question
In what units are turbine engine tachometers calibrated?
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Question 50 of 54
50. Question
Instruments that provide readings of low or negative pressure, such as manifold pressure gauges are usually what type?
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Question 51 of 54
51. Question
Instruments that measure relatively high fluid pressures, such as oil pressure gauges, are usually what type?
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Question 52 of 54
52. Question
The RPM indication of a synchronous AC motor-tachometer is governed by the generator.
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Question 53 of 54
53. Question
The EGT gauge used with reciprocating engines is primarily used to furnish temperature readings in order to
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Question 54 of 54
54. Question
A red triangle, dot, or diamond mark on an engine instrument face or glass indicates
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