M15.21 Flashcards

(54 cards)

1
Q

Why are turbine engines operated during maintenance?

A

Fault confirmation, post-maintenance checks, performance investigation, control wear checks, taxi checks, aircraft movement.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Which engine types do ground operation procedures apply to?

A

Turbofan, turboprop, turboshaft engines and APUs.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What does advancing the thrust lever do?

A

Increases engine speed and commands increased fuel flow.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Key pre-start inlet inspection requirement

A

Ensure compressor/turbine rotate freely and no FOD is present.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Common sources of engine starting air

A

Ground air unit, APU, or bleed air from another engine.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Key parameters monitored during engine start

A

RPM (N1/N2/N3), oil pressure, and EGT.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

What is a hot start?

A

Excessive EGT during engine start.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What is a hung start?

A

Insufficient engine acceleration during start.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Aircraft positioning requirement for engine run

A

Aircraft positioned into wind with chocks fitted and brakes applied.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Minimum intake clearance during engine run

A

Approximately 10 m (30 ft) in front of intakes.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Why is engine cool-down at idle required before shutdown?

A

Prevents rotor distortion, bearing damage, and rotor seizure.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Purpose of engine performance indications

A

Allow monitoring of engine operation and limits during start, ground operation, and flight.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Main engine monitoring parameters

A

EPR, N1/N2/N3, fuel flow, and EGT.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Define Engine Pressure Ratio (EPR)

A

Ratio of turbine discharge pressure to compressor inlet pressure.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Advantage of EPR as a thrust indication

A

Largely independent of ambient temperature and accurate for axial-flow engines.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What does N1 indicate?

A

Low-pressure spool speed driving the fan and LP compressor.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Why is N2 important during engine start?

A

Confirms starter cut-out speed and detects hung starts.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Purpose of fuel flow indication

A

Flight planning, trend monitoring, and detecting abnormal fuel usage.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Why is EGT critical?

A

Indicates thermal condition and prevents engine overheating.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Primary power indication on turboprop engines

A

Engine torque.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Torque is proportional to what?

A

Shaft horsepower.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Common torque sensing methods

A

Hydro-mechanical, electronic shaft twist, and phase displacement systems.

23
Q

Purpose of engine trend monitoring

A

Detect abnormal deterioration early and support on-condition maintenance.

24
Q

Main benefit of trend monitoring

A

Prevents failures and reduces operating costs.

25
What system records engine trend data?
Aircraft Condition Monitoring System (ACMS).
26
Role of FADEC in trend monitoring
Measures and provides engine parameter data.
27
Purpose of thermodynamic analysis
Identify efficiency loss and deteriorating engine modules.
28
Purpose of vibration monitoring
Detect imbalance or impending mechanical failure.
29
What does SOAP stand for?
Spectrometric Oil Analysis Programme.
30
Purpose of magnetic chip detectors
Collect ferrous debris for condition monitoring.
31
What do metal chips indicate?
Serious internal engine damage.
32
Why is compressor blade condition critical?
Damage can lead to severe engine failure.
33
Primary cause of compressor blade damage
Foreign Object Damage (FOD).
34
Are cracks permitted in compressor blades?
No, cracks are never permitted.
35
Approved tools for blade blending
Hand files or emery cloth only.
36
Most common hot section defect
Cracking.
37
Why is hot section inspection critical?
It directly affects engine service life.
38
Why are carbon pencils prohibited on hot section parts?
They can cause intergranular corrosion and strength reduction.
39
Primary concern in turbine blade inspection
Stress cracks and over-temperature damage.
40
Why are turbine clearances important?
Incorrect clearances cause performance loss and mechanical damage.
41
Purpose of compressor washing
Restore aerodynamic efficiency and engine performance.
42
Main sources of compressor contamination
Salt, industrial pollution, airborne contaminants.
43
What is a desalination wash used for?
Removing salt contamination using fresh water.
44
When is a performance recovery wash required?
When desalination wash is insufficient.
45
Common abrasive cleaning materials
Crushed walnut shells or apricot stones.
46
Cold weather washing precaution
Use isopropyl alcohol as antifreeze.
47
Why must methanol not be used?
It damages titanium components.
48
Define Foreign Object Damage (FOD)
Damage caused by objects ingested into engines or interfering with aircraft systems.
49
Why are turbine engines vulnerable to FOD?
High intake airflow and ingestion capability.
50
Difference between external and internal FOD
External is ingested from outside; internal is objects left inside aircraft.
51
Why is tool FOD especially serious?
It can cause control interference, short circuits, and engine damage.
52
Examples of common FOD sources
Tools, fasteners, gravel, birds, ice, sand, volcanic ash.
53
Purpose of bird strike certification tests
Ensure engine failure does not cause hazardous aircraft damage.
54
What is fan blade containment?
Fan case designed to contain a released blade.