15.21 Operation and Monitoring Flashcards

(58 cards)

1
Q

What are common reasons for running a turbine engine on the ground?

A

Fault diagnosis, post-maintenance checks, engine deterioration, control linkage checks, repositioning aircraft, or system taxi checks.

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2
Q

What are the sources of air for engine starting?

A

APU, external ground power unit (GPU), or bleed air from another engine.

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3
Q

What key parameters must be monitored during engine start?

A

: Engine speed (N1/N2), oil pressure, and EGT.

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4
Q

What must be checked before starting a turbine engine?

A

Engine intakes/exhausts for FOD, oil/fuel levels, panel security, undercarriage down and locked, and clear ground area (10m in front, aircraft-specific distance behind).

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5
Q

Why is the aircraft positioned into wind before engine start?

A

To improve airflow into the engine and reduce the risk of hot starts or FOD ingestion.

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6
Q

What safety measures are required during an engine ground run?

A

Apply brakes, fit chocks, fire extinguisher on hand, wear ear protection, maintain flight deck communication, and restrict access to engine danger zones.

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7
Q

When may the fire service be required during engine runs?

A

If cowlings are open or for high-power/pressure runs—depends on local airport rules.

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8
Q

What’s the purpose of allowing an engine to idle before shutdown

A

To cool it down and prevent rotor seizure after high-power operation.

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9
Q

How is a turbine engine shut down after ground running?

A

Retard thrust lever to idle, then move fuel cut-off lever to OFF.

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10
Q

What is EPR and what does it indicate?

A

Engine Pressure Ratio – it measures jet pipe pressure vs inlet pressure to indicate thrust output.

This is for centrifugal compressor

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11
Q

What does the N1 rotor speed represent?

A

Speed of the low-pressure spool.

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12
Q

Why is EGT a critical engine parameter?

A

It helps detect overheating; exceeding red line requires immediate inspection.

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13
Q

How do turboprop- turboshaft engines measure power output?

A
  • using torque indicators
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14
Q

How is turboprop/ shaft engine power output displayed?

A

Torque oil pressure (in psi)
Torque percentage
Sometimes a direct horse-power read-out

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15
Q

In turboprop/ shaft where does the torque meter get its input from?

A

Torque sensing unit in the engine

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16
Q

What are the types of torque sensing system sused in turboprop/shaft engines#?

A

Hydromechanical: converts engine oil pressure to a torque signal
Electronic: converts twist of the power output shaft into a torque signal
Phase displacement: One shaft is reference, second is allowed to twist. Phase difference tells you how much torque engines producing

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17
Q

Why can’t axial bypass engines use RPM for thrust measurement?

A

Because ambient conditions affect thrust, so RPM doesn’t directly reflect power output.

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18
Q

What was used in early axial engines to estimate thrust?

A

A pressure comparison between ambient pressure (Pamb) and exhaust pressure (P7), in inches of mercury.

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19
Q

What system collects engine performance data in modern aircraft?

A

Aircraft Condition Monitoring System (ACMS).

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20
Q

What is the role of FADEC in trend monitoring?

A

It measures engine parameters and sends them to the data system.

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21
Q

What are the three types of ACMS reports?

A

Routine, on-request, and advisory reports.

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22
Q

What is the purpose of thermodynamic analysis?

A

To identify which engine module is causing performance changes.

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23
Q

What is mechanic-dynamic analysis used for?

A

To identify vibration-related faults using filtered sensor signals.

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24
Q

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

A

To compile and transmit ACMS reports.

25
How often are take-off reports generated in normal operation?
Every 35 take-offs after the initial four baseline reports.
26
Whats the main method of oil analysis?
Spectrometric Oil Analysis Program (SOAP): Uses a spectrometer to detect and identify microscopic particles suspended in oil.
27
What does oil analysis help detect in aircraft engines?
Internal wear and potential damage through the presence of metal particles in oil.
28
How are ferrous metals detected in oil?
Using a magnet
29
How are non-ferrous particles identified?
By chemical reaction, e.g. boiling in nitric acid and observing colour changes.
30
What might large metal flakes or chips in oil suggest?
: Serious internal engine or gearbox damage.
31
When are oil analysis inspections carried out?
Routinely, or after events like heavy landings or lightning strikes.
32
What does a boroscope inspection allow engineers to check?
Internal engine components like turbine blades and combustors for damage or wear.
33
What type of sensors are used in vibration monitoring?
Piezoelectric accelerometers Measured in ips or mm per sec indicated as a broadband reading on the flight deck
34
What are the two main turbine engine sections for inspection?
The cold section (compressor) and hot section (combustion/turbine).
35
What is the main cause of compressor blade damage?
Foreign Object Damage (FOD) and dirt build-up from air intake.
36
How should compressor blade repairs be made?
By hand (files/emery cloth), with smooth blending and no cracks.
37
What tool should not be used for compressor blade repair?
Power tools — they can damage surface finish and integrity.
38
What is a common inspection method for cracks in the hot section?
Dye penetrant inspection (visible or fluorescent).
39
Can a wax pencil be used to mark turbine rotors or liners?
No — wax pencils are for non-gas path parts only.
40
What are stress cracks and where are they found?
Fine cracks on turbine blade edges, caused by heat and stress.
41
How should fuel nozzles be cleaned?
With approved cleaning fluid and a soft brush — no scraping.
42
What causes galling in turbine components?
Severe rubbing, which transfers metal between surfaces.
43
What should be inspected in the exhaust section?
Cracks, warping, buckling, and hotspots from heat stress.
44
Where are blade cracks most often found?
: Leading or trailing edges, appearing as hairline fractures.
45
How are turbine component clearances verified?
Using tolerances specified in the manufacturer's overhaul manual.
46
What is the main effect of contamination in the compressor section?
Reduced aerodynamic efficiency and engine performance.
47
What is sulfidation?
A build-up of sulphur from burned fuel that causes hot corrosion on turbine blades.
48
What is a desalination wash?
A fresh water rinse to remove salt, done while motoring or idling the engine.
49
When is a performance recovery wash required?
When salt and dirt contamination is too severe for a desalination wash.
50
What cleaning method uses emulsion-type cleaner?
Performance recovery wash
51
Why is heated water preferred in compressor washes?
It has a more effective cleaning action than cold water.
52
What material is used in abrasive grit washing?
Broken walnut shells or apricot stones.
53
Why is abrasive grit washing limited to compressor cleaning?
Because the grit burns off in combustion and does not reach turbine components.
54
What is sprayed into fan blades for abrasive cleaning?
Fine filtered abrasive called coke.
55
What alcohol is safe to use as antifreeze during washing in cold temperatures?
Isopropyl alcohol.
56
Why must methanol be avoided in engine washing?
It severely damages titanium components.
57
Who provides the proper procedures for compressor washing?
The engine manufacturer.
58
whats the purpose of vortex dissipaters on an aircraft?
To reduce engine intake from below and prevent debris ingestion