M15.21 Operation and Monitoring Flashcards

1
Q

What are the circumstances when maintenance personnel are required to operate a gas turbine engine?

A
  • Confirming a flight crew reported fault
  • Post-maintenance basic engine or aircraft system checkout
  • Deterioration of engine performance
  • Aircraft control linkage wear
  • Moving an aircraft from one maintenance location to another
  • To taxi-check an aircraft system
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2
Q

What types of engines do the engine operating procedures apply to?

A
  • Turbofan
  • Turboprop
  • Turboshaft
  • Auxiliary Power Units (APU)
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3
Q

What must be checked before any engine start?

A

The engine air inlet must be checked to confirm free movement of the compressor and turbine assembly, and that the engine run-up area is clean and free of Foreign Object Debris (FOD)

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4
Q

How is a turbofan engine controlled?

A

By one control thrust lever for each engine

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5
Q

What must be ensured before starting the engine?

A
  • Undercarriage is down and locked
  • Engine oil levels are satisfactory
  • All panels are secure
  • Sufficient fuel for the ground run
  • Intakes and exhausts are inspected for foreign objects and damage
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6
Q

What is the appropriate fire extinguisher needed during engine ground running?

A

CO2 fire extinguisher

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7
Q

What must be done during engine start monitoring?

A
  • Engine speed indicator (tachometer)
  • Oil pressure
  • Exhaust Gas Temperature (EGT)
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8
Q

What is the recommended cool-down time before shutting down an engine that has been operated at high power levels?

A

5 minutes at idle power

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9
Q

What does the Engine Pressure Ratio (EPR) indicate?

A

The thrust output of the engine

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10
Q

What are the indications used for engine monitoring?

A
  • Engine Pressure Ratio (EPR)
  • Rotor speed, N1 and N2 (and N3)
  • Fuel Flow (FF)
  • Exhaust Gas Temperature (EGT)
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11
Q

What is the purpose of torque monitoring systems in turbo-prop or turbo-shaft engines?

A
  • Indicate power developed by the engine
  • Automatically operate the propeller feathering system
  • Assist in the automatic operation of a water injection system
  • Limit engine power output
  • Balance power output between engines
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12
Q

What is the function of the Aircraft Condition Monitoring System (ACMS)?

A

To record operating parameters and generate reports for engine trend monitoring

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13
Q

What is the purpose of oil analysis in engine monitoring?

A

To provide information about the condition of the engine by identifying wear particles in the oil

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14
Q

What is the Spectrometric Oil Analysis Program (SOAP)?

A

A process used to detect wear particles in engine oil

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15
Q

What are the four primary groups of magnetic particles?

A
  • Swarf
  • Magnetic fines
  • Metal flakes
  • Chip
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16
Q

Fill in the blank: The ___________ must be checked to confirm sufficient fuel for the ground run.

A

fuel tanks

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17
Q

True or False: It is acceptable to start the engine without ensuring that the areas in front and behind the aircraft are clear.

A

False

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18
Q

What is the purpose of the torque meter in a turbo-prop or turbo-shaft engine?

A

To provide continuous indication of the horsepower output of the engine

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19
Q

What is required to identify metal particles in engine oil?

A

Spectrometric Oil Analysis Program (SOAP)

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20
Q

What must be established with the ground crew before starting the engine?

A

Communications for clearance and safety confirmation

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21
Q

What is the significance of monitoring Exhaust Gas Temperature (EGT)?

A

To recognize and prevent overheating conditions

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22
Q

What happens if the EGT exceeds the red line?

A

Immediate inspections of the critical engine are required

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23
Q

What is the role of the Data Management Unit (DMU)?

A

To record and compile ACMS reports

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24
Q

What should be done if abnormal deteriorations in engine efficiency are detected?

A

Schedule engine removal before the defect fully develops

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25
Q

What is a common method for identifying ferrous particles?

A

Using a magnet to separate ferrous from non-ferrous particles

26
Q

What is the purpose of engine and gearbox inspections?

A

To assess the condition of the engine and gearbox, usually at regular intervals or after specific events like heavy landings or lightning strikes.

Inspections can also aid in troubleshooting issues.

27
Q

Name the four primary groups of magnetic particles.

A
  • Swarf
  • Magnetic fines
  • Metal flakes
  • Chip

These groups help categorize the types of contamination in engine components.

28
Q

What is swarf?

A

Unwanted material caused by machining engine components, which can remain in the engine/gearbox after assembly.

29
Q

How do magnetic fines appear on an MCD?

A

As black sludge when oil is present.

They originate from worn areas in the engine/gearbox.

30
Q

What do metal flakes indicate in an engine?

A

They come from ball bearings, roller bearings, bearing tracks, and gear teeth, and their shape can indicate the source.

31
Q

Describe gear teeth flakes.

A

They are shiny, irregularly shaped flakes that can resemble solder splashes.

32
Q

What are chips in the context of engine components?

A

Thick flakes or pieces of metal with one smooth machined surface.

33
Q

What is a boroscope inspection?

A

An internal visual inspection of the engine using a rigid boroscope, flexible fibrescope, or electronic imaging video probe.

34
Q

Why is vibration monitoring important in gas turbine engines?

A

Because changes in vibration levels may indicate impending failure that could otherwise go unnoticed.

35
Q

What do modern engines use to monitor vibration?

A

Piezoelectric accelerometers.

36
Q

What sections is a turbine engine divided into for inspection purposes?

A
  • Cold section (Compressor Section)
  • Hot section (Turbine and Combustion Section)

This division aids in focused maintenance procedures.

37
Q

What can cause damage to compressor blades?

A

Foreign object matter entering the turbine engine air intakes.

38
Q

What is the effect of dirt accumulation on compressor blades?

A

It reduces the aerodynamic efficiency of the blades, resulting in deterioration in engine performance.

39
Q

What are the allowable limits for minor damage to compressor blades?

A

Damage can be repaired if it can be removed without exceeding the limits set by the engine manufacturer.

40
Q

What tools are recommended for reworking damage on compressor blades?

A

Hand tools such as files or emery cloth.

Power tools should not be used for buffing.

41
Q

What is Foreign Object Damage (FOD)?

A

Damage caused by foreign objects entering the engine, which can degrade performance and shorten engine life.

42
Q

List some typical causes of blade damage.

A
  • Loose objects entering the engine
  • Foreign Object Damage (FOD)
  • Excessive heat levels
  • Corrosive agents

These causes can lead to various types of damage.

43
Q

What is the definition of ‘blend’ in the context of blade repair?

A

Smooth repair of ragged edges or surface to match the contour of the surrounding area.

44
Q

What is the significance of inspecting the combustion section of a turbine engine?

A

Inspection and cleaning are crucial for prolonging service life.

45
Q

How should cracks in turbine blades be detected?

A

Primarily through visual inspection, possibly supplemented by structural inspection techniques like dye penetrant methods.

46
Q

What must be considered when replacing turbine blades?

A

Moment-weight limitations as specified in the engine manufacturer’s technical instructions.

47
Q

What is the recommended method for cleaning fuel nozzles?

A

Washing with a cleaning fluid approved by the engine manufacturer and using a soft bristle brush.

48
Q

What is the purpose of a desalination wash?

A

To remove salt contamination from the compressor to maintain engine efficiency.

49
Q

What should be done before starting a turbine engine?

A

Inspect the engine inlet ducts to ensure no Foreign Object Damage (FOD) items are left.

50
Q

What types of materials can be used for temporary marking during assembly?

A
  • Layout dye or chalk for gas path exposed parts
  • Wax marking pencil for non-gas path parts

Avoid using materials that may cause corrosion.

51
Q

What is the risk associated with tools left inside an aircraft?

A

They can interfere with safe flight by jamming controls or shorting electrical connections.

52
Q

What is Tool FOD?

A

A serious hazard caused by tools left inside the aircraft following maintenance.

53
Q

What can Tool FOD interfere with?

A

Safe flight operations, including control cables and electrical connections.

54
Q

Give examples of FOD.

A
  • Aircraft parts
  • Rocks
  • Broken pavement
  • Ramp equipment
  • Parts from ground vehicles
  • Rubbish on ramp/runway
  • Ice on wings/propellers/intakes
  • Bird strikes
  • Dust/ash in air intakes
  • Tools and metal shavings left inside aircraft
55
Q

What does airport operations do regarding FOD?

A

Regularly inspect and clear the runways of aircraft FOD.

56
Q

What can happen to jet engines from FOD?

A

They can suffer major damage from even small objects being sucked into the engine.

57
Q

What type of test must all manufactured engines pass?

A

A test involving firing a frozen chicken into a running jet engine.

58
Q

What is the requirement for engines after the bird strike test?

A

The engine must not cause significant damage to the rest of the aircraft.

59
Q

What was Boeing’s solution for early B737s to avoid FOD?

A

A gravel runway kit with gravel deflectors and screens on landing gear.

60
Q

What do vortex dissipation devices do?

A

Reduce airflow into the engine from the bottom to decrease the likelihood of sucking up gravel.

61
Q

True or False: The engine must remain operational after the bird strike test.