Module 15.14 Engine Indication Systems Flashcards

1
Q

What is the exhaust gas temperature (EGT) used to monitor?

A

High temperatures experienced by the turbine.

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2
Q

Where is the exhaust gas temperature measured?

A

A colder location in the engine. Either between the high and low-pressure turbine or directly behind the low-pressure turbine.

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3
Q

Where are temperature thermocouples inserted?

A

At the turbine discharge.

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4
Q

What is used to measure exhaust gas temperature (EGT)?

A

Thermocouples

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5
Q

What does the exhaust gas temperature indicator scale range from?

A

0 °C to 1200 °C

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6
Q

What do engine indicators monitor?

A

Parameters of the engine and its systems.

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7
Q

The engine indications can be divided into what three groups?

A

Performance indications

System Indications

Engine trend monitoring

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8
Q

What are performance indications used to monitor?

A

The performance and the limits of the engine and to set the thrust for the different flight phases (primary indications).

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9
Q

What are system indications used to monitor?

A

The operation of engine systems such as the oil or fuel system. They also detect malfunctions quickly (secondary indications).

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10
Q

What does engine trend monitoring do?

A

Detects engine problems at an early stage.

Not usually shown in the flight deck.

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11
Q

What are engine parameters recorded by?

A

Aircraft Condition Monitoring System (ACMS).

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12
Q

How can engine indications be displayed?

A

Gauge type analogue displays and digital readouts.

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13
Q

Engine performance indications are located where?

A

Top ECAM/EICAS display.

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14
Q

Can thrust be measured directly?

A

No

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15
Q

What two indications give equivalent thrust value?

A

Fan rotational speed (N1)

Engine Pressure Ratio (EPR)

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16
Q

What does thermodynamic analysis check for?

A

Pressures and temperatures along the gas flow path.

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17
Q

What does mechanic-dynamic analysis check for?

A

Failures in the rotor system.

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18
Q

When does the oil consumption analysis generate an alert?

A

When oil consumption exceeds a certain level.

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19
Q

How does the Engine Pressure Ratio (EPR) indicator/gauge work?

A

It compares the engine turbine discharge pressure to the pressure of the ram air at the inlet of the engine.

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20
Q

To determine EPR, what are pressure measurements taken by?

A

Probes

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21
Q

Where are EPR probes located?

A

In the engine inlet and turbine exhaust.

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22
Q

What does an AMBER or RED line on the EPR indicator/gauge mean?

A

EPR for the maximum available thrust.

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23
Q

What does a BLUE circle on the EPR indicator/gauge mean?

A

EPR that corresponds to the actual throttle position.

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24
Q

What is the standard take-off thrust setting used on Airbus aircraft.

A

Flexible Take-Off (“FLEX”).

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25
Q

When is the TOGA (full) take-off thrust setting on Airbus aircraft used?

A

When taking off on a contaminated runway or if there’s performance constraints.

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26
Q

Why is FLEX the take-off setting used?

A

To preserve engine wear and life.

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27
Q

What does the FLEX take-off setting use?

A

Assumed temperature thrust reduction

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28
Q

What does the FLEX take-off temperature used reflect?

A

The thrust which would be achieved from a TOGA take-off with that outside air temperature. E.g. 40 °C.

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29
Q

What does the oil pressure indicator show?

A

Engine oil pump discharge pressure.

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30
Q

List the two main types of oil pressure transmitters.

A

Bourdon Tube type

Strain Gauge type

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31
Q

What warning does the pressure switch give?

A

Low oil pressure warning.

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32
Q

What is the pressure switch connected to?

A

Oil supply line and the oil tank vent line.

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33
Q

What does the pressure switch do when oil pressure decreases below the set limit?

A

The switch closes.

34
Q

What primary component is responsible for measuring the engine oil temperature?

A

Oil temperature sensor.

35
Q

What is the oil temperature sensor designed to do?

A

Respond to changes in temperature and convert this information into an electrical signal.

36
Q

What is the most common temperature sensors used in aircraft engines?

A

Resistance Temperature Detector (RTD) or Thermocouple.

37
Q

How is an oil over-temperature warning given?

A

Visual (warning light) and audible (warning sound or alert).

38
Q

Where is the low-pressure sensor positioned?

A

After the low-pressure filter.

39
Q

What sensor is fitted across the fuel filter?

A

A differential pressure sensor.

40
Q

What do low-pressure sensors give a warning of?

A

Imminent filter blockage.

41
Q

What can a filter blockage cause?

A

HP fuel pump cavitation.

42
Q

How is a warning of low fuel pressure displayed?

A

Warning light or EICAS/ECAM status message.

43
Q

What type of electric fuel temperature sensor is used in the main fuel tank?

A

Resistance type

44
Q

What two indications does the fuel flow indicating system show?

A

Actual fuel flow to the engines.

Fuel used since the engine was started.

45
Q

What calculates fuel flow and fuel used?

A

The FADEC system computer.

46
Q

What can fuel be indicated in?

A

Kg, lbs, or tons.

47
Q

What does the fuel flow transmitter measure?

A

Mass flow of fuel between the fuel control unit and fuel nozzles.

48
Q

What two types of fuel flow transmitters are used as mass flow meters?

A

Synchronous mass flow

Motorless mass flow

49
Q

What rotor does the N1 indicator display?

A

Low-pressure rotor

50
Q

What rotor does the N2 indicator display?

A

High-pressure rotor

51
Q

When would and N3 indication be needed?

A

If the engine has 3 rotors.

52
Q

What are rotor speed indications expressed as?

A

A percentage of 100% max speed (rpm).

53
Q

What are the three main parts to each rotor speed indication?

A

The sensor

Data transmission

Indication

54
Q

What two types of sensor can measure rotor speed on engines?

A

Variable reluctance type

Tachometer generator type

55
Q

Where is the tachometer generator type rotor speed sensor located?

A

On the gearbox.

56
Q

List the three different types of rotor speed indication.

A

Clock-type scale

Moving vertical bar

Electromechanical indicator

57
Q

What does the speed limit indication protect the engine against?

A

Overspeed (red line limit).

58
Q

What does the N1 red line limit mean?

A

Maximum permitted rotor speed.

59
Q

What do modern engines do if the engine speed exceeds the N1 red line limit?

A

The speed and duration is recorded and initiates a report from the engine trend monitoring.

60
Q

What does an indication for engine vibration allow flight crew and maintenance to identify

A

Rotor imbalance

61
Q

How is the indication for engine vibration given?

A

Units from 0 to about 6.

62
Q

How many vibration sensors deliver electrical signals to a computer.

A

One or two.

63
Q

What does the computer do to engine vibration data?

A

Collects and filters the data for indication and engine trend monitoring.

64
Q

What is the engine vibration computer called?

A

Engine Vibration Monitoring Unit (EVMU).

65
Q

What is used to sense engine vibrations?

A

Accelerometers

66
Q

Where are the two vibration sensors located?

A

One in the compressor area and the other in the turbine area.

67
Q

What two types of accelerometers are used on engines to measure vibration?

A

Electromagnetic accelerometer

Piezoelectric-crystal type

68
Q

What is the vibration indication on modern aircraft is automatically controlled by?

A

The engine vibration monitoring unit.

69
Q

How many vibration values are there for each engine?

70
Q

How can engine vibration be decreased?

A

Fan balancing

71
Q

What does the engine balancing system do?

A

Identifies the balance weights that are required to be removed and replaced

72
Q

What are torque measuring systems called?

A

Torque meters

73
Q

What are the two types of torque meters?

A

Electrical

Hydraulic

74
Q

What is does the power assurance test check?

A

That the engine can accelerate from idle to a given Engine Pressure Ratio (EPR) value within a specific time and de-accelerate back to idle within a specific time.

75
Q

How long does the engine operate at idle for during the power assurance test check?

76
Q

What should be set to off during the power assurance test check?

A

Engine anti-ice and bleed air switches.

77
Q

How quickly must the engine accelerate to the required speed during the power assurance test check?

78
Q

How quickly must the engine decelerate to idle speed (N1)?

A

8 seconds or less.

79
Q

After engine operation over 70% N1, how long must the engine be at idle for?

A

Minimum 10 minutes.

80
Q

What are the three analysis used for engine trend monitoring?

A

Thermodynamic

Mechanical-dynamic

Oil consumption

81
Q

What analysis is used to monitor engine vibration?

A

Mechanical-dynamic analysis