15.21 Operating & Monitoring Flashcards

1
Q

What must be done when positioning the aircraft for an engine run?

A

Face aircraft into the wind.
Apply brakes.
Clear obstructions.
No aircraft 10m infornt of engine intake.
Check oil levels
Position CO2 extinguisher.

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2
Q

During acceleration checks, what is the datum (reference)?

A

The oldest engine.

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3
Q

After operating at high power, how long should an engine cool down for?

A

5 mins at idle power.

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4
Q

What is the purpose of engine cool down period?

A

Prevents rotor seizures.

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5
Q

When do you do engine trimming?

A

When engines are running.

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6
Q

When must engine asymmetry be considered?

A

When you’re only running 1 engine.

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7
Q

What are the 3 parameters indication groups?

A

Performance monitoring.
System monitoring.
Condition monitoring.

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8
Q

What indications are used for engine monitoring?

A

EPR
Rotor speed, N1, N2, (N3)
Fuel Flow
EGT

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9
Q

What is the low pressure rotor speed?

A

N1

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10
Q

What is the high pressure rotor speed?

A

N2, N3 on 3 spool engine.

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11
Q

How do axial flow bypass engines indicate thrust?

A

Using EPR as rotor speed is not proportional.

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12
Q

What do torque monitoring systems indicate?

A

Power developed by a turboprop or turboshaft engine.

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13
Q

What can the torque monitoring system be used for?

A

To automatically operate propeller feathering system.
Assist automatic operation of water injection system.
Limit engine power output.
Balance power between engines.

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14
Q

What ways can torque be displayed?

A

Torque oil pressure.
Torque percentage.
Direct horsepower read out.

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15
Q

What instrument is used to indicate torque?

A

Torque meter

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16
Q

What are the 2 sensing systems used on turboshaft and turboprop engines?

A

Hydro mechanical.
Electronic /Phase displacement.

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17
Q

How does the electronic sensing system work?

A

The phase difference is measured between 2 shafts, which is converted to an electronic signal to indicate torque.

18
Q

When is an engine removed?

A

Only for change of life limited parts or damage repairs.

19
Q

What records data onboard the aircraft?

A

Aircraft Condition Monitoring System (ACMS)

20
Q

Where is ACMS data transmitted?

A

To Data Management Unit (DMU)

21
Q

What does the DMU do?

A

Records data and complies a ACMS report.

22
Q

How are ACMS reports accessed?

A

Printed or sent to the ground via link.

23
Q

What does thermodynamic analysis do?

A

Identifies wear of gas path components.

24
Q

What does mechanic dynamic analysis do?

A

Identifies vibration caused by the fan and turbine rotor system.

25
Q

When is a inflight data report generated?

A

During first 4 take offs.
Then every 35 take offs.
If results are critical.

26
Q

What are the 4 groups of magnetic particles?

A

Swarf.
Magnetic fines.
Metal flakes.
Chips.

27
Q

What solution are metal particles boiled in?

A

A nitric acid solution.

28
Q

How can magnetic fines be identified?

A

Black sludge on Magnetic Chip Detectors.

29
Q

What are metal flakes produced by?

A

Bearings.

30
Q

Define boroscope inspections?

A

Internal visual inspection.

31
Q

What do modern engines use to detect engine vibration?

A

Piezoelectric accelerometer.

32
Q

Where are accelerometers fitted?

A

Fan.
LP compressor casing
Turbine casing.

33
Q

Can compressor blades be repaired?

A

Yes, can be blent out if within manufacturer limits.

34
Q

What can be used to mark materials directly exposed to gas path?

A

Layout dye or chalk.

35
Q

What can be used to mark materials not directly exposed to the gas path?

A

Wax marking pencil.

36
Q

What is the most common defects in the hot section of the combustion section?

A

Cracking.

37
Q

What is used to inspect the combustion chamber?

A

Visible dye or fluorescent penetrant.

38
Q

What can fuel nozzles be cleaned with?

A

Approved cleaning fluid.
Soft bristle brush.

39
Q

What does deformation in turbine due to high temperatures present as?

A

Waviness along LE.

40
Q

How is the compressor cleaned?

A

A desalination wash with fresh water.