15.21 Operation and Monitoring Flashcards

1
Q

What are the requirements for engine handling, operation, and monitoring during maintenance activities?

A

Detailed understanding of engine operation and safety during ground running

Includes procedures for confirming faults, post-maintenance checks, and ensuring safe operation.

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2
Q

What must be checked before starting any engine?

A

Engine air inlet for free movement, cleanliness of run-up enclosure, and presence of Foreign Object Debris (FOD)

Ensures safe engine operation and prevents damage.

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3
Q

What is a hung start?

A

Successful ignition but the engine does not accelerate to idle RPM

Indicates potential issues with fuel flow or engine performance.

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4
Q

What is a hot start?

A

When fuel burns inside the engine or EGT limit is exceeded during start

Requires immediate abortion of the starting procedure to avoid damage.

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5
Q

What are the safety requirements for engine ground running?

A

Restricted access to the engine, communication with flight deck, and availability of fire extinguisher

Ensures personnel safety and compliance with emergency protocols.

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6
Q

Fill in the blank: The engine is started using an external ground _______ , the APU, or an operating engine.

A

Air Power Unit

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7
Q

What must be checked before positioning the aircraft for engine run-up?

A

Technical logbook, undercarriage position, oil levels, fuel levels, and area clearance

Ensures that all conditions are safe for engine operation.

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8
Q

What communication is necessary before starting the engine?

A

Establish communication with ground crew and ATC for engine start permission

Ensures safety and proper coordination during engine operations.

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9
Q

What is idle trim?

A

Adjustment of idle speed to ensure the engine idles at the lowest RPM authorized by the manufacturer

Important for engine performance testing and efficiency.

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10
Q

What is the recommended cool-down time before shutting down an engine?

A

5 minutes at idle power

Prevents seizure of rotors and ensures even cooling of engine components.

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11
Q

What should be done after retarding the thrust lever to idle for engine shutdown?

A

Use an independent fuel cut-off lever or switch

Ensures safe shutdown and prevents damage to fuel system parts.

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12
Q

What is the role of the APU during engine start on multi-engine aircraft?

A

Supplies air pressure to the pneumatic starter on each engine

Essential for initiating the engine start process.

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13
Q

What must be monitored during the engine start sequence?

A

Engine speed indicator, oil pressure, and Exhaust Gas Temperature (EGT)

Critical for detecting potential issues during startup.

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14
Q

True or False: The fuel cut-off lever should be shut off immediately after the engine starts.

A

False

It should be turned off only after the thrust lever is retarded to idle.

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15
Q

What is the purpose of engine trimming?

A

Adjusting throttle settings and maximum thrust during engine performance testing

Ensures engines operate efficiently and uniformly.

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16
Q

What should be done if an engine does not light off within ten seconds after introducing fuel?

A

Shut off the fuel switch/lever to prevent unburned fuel accumulation

Important for safety and preventing engine damage.

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17
Q

What is the typical pressure required for external ground air during engine start?

A

Approximately 40 - 55 psi

Necessary for proper engine starting conditions.

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18
Q

What should be done after engine shutdown to check oil levels?

A

Wait 30 minutes for pressure to drop and oil to return to the oil tank

Ensures accurate oil level readings.

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19
Q

What is the purpose of engine monitoring systems during ground runs?

A

To monitor engine performance and limitations with the aircraft on the ground.

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20
Q

What types of instruments or displays are used for engine performance indications?

A

Individual instruments or display screens connected to sensors on the engine.

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21
Q

List the key 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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22
Q

What does the Engine Pressure Ratio (EPR) indicate?

A

The ratio of the jet pipe pressure to the compressor inlet pressure, indicating thrust output.

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23
Q

What does the low-pressure rotor speed N1 indicate?

A

The rotor speed of the low-pressure spool as a percentage of the 100% design speed.

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24
Q

How is N1 related to thrust in high bypass engines?

A

N1 is used as a thrust indication because thrust is directly related to fan speed.

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25
Q

What is the purpose of high-pressure rotor speed N2 monitoring?

A

To monitor the high-pressure spool speed limit and control idle speeds.

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26
Q

What is the significance of Fuel Flow (FF) indication?

A

To monitor fuel consumption during flight and confirm positive fuel flow during engine start.

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27
Q

Why is Exhaust Gas Temperature (EGT) critical?

A

It helps recognize and prevent overheating; exceeding the red line requires immediate inspections.

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28
Q

How is gas turbine engine power output indicated for different engine types?

A

It varies between turbo-jet and turbo-prop/turbo-shaft engines.

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29
Q

What method is used to measure engine power for centrifugal compressor engines?

A

By comparing engine RPM and Jet Pipe Temperature (JPT).

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30
Q

What challenge do axial flow bypass engines face in measuring power output?

A

There is no direct relationship between engine RPM and thrust due to ambient temperature effects.

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31
Q

What method was used in early engines to indicate power output?

A

Comparison between static ambient pressure and exhaust gas pressure.

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32
Q

What is the Engine Pressure Ratio (EPR) system used for?

A

To compare inlet plus fan outlet pressure to exhaust gas pressure and present it as a ratio.

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33
Q

What thrust levels are used in a power assurance test?

A
  • 50%
  • 75%
  • 100%
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34
Q

What information do thrust tables provide?

A

Thrust values for different thrust levels and operational limits that must not be exceeded.

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35
Q

What systems are used for torque monitoring in turbo-prop or turbo-shaft engines?

A

Torque monitoring systems indicating power developed to the flight deck.

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36
Q

What are the methods used to display torque in the flight deck?

A
  • Torque oil pressure (in psi)
  • Torque percentage
  • Direct horse-power read-out
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37
Q

What is the function of a torque meter?

A

To indicate torque based on input from the torque sensing unit on the engine.

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38
Q

List the common types of torque sensing systems.

A
  • Hydro-mechanical
  • Electronic
  • Phase displacement
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39
Q

How does the hydro-mechanical torque sensing system work?

A

It converts engine oil pressure to a torque signal.

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40
Q

What does the phase displacement system use to measure torque?

A

A shaft with two phonic wheels to compare phase differences.

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41
Q

What happens to the bleed openings in the torque sensing system under low power conditions?

A

The bleed openings are at their maximum, balancing oil pressure with thrust.

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42
Q

What is the purpose of trend monitoring in turbine engines?

A

To detect abnormal deteriorations in engine efficiency and limit operating costs.

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43
Q

What system is used for data recording on board an aircraft for engine trend monitoring?

A

Aircraft Condition Monitoring System (ACMS)

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44
Q

What additional computer is required for engines with hydro-mechanical fuel controls?

A

Power Plant Data Multiplexer (PMUX)

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45
Q

What does FADEC stand for?

A

Full Authority Digital Engine Control

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46
Q

What type of reports does the ACMS generate?

A
  • Routine reports
  • On request reports
  • Advisory reports
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47
Q

What analysis identifies which engine module is responsible for changes in thermodynamic variables?

A

Thermodynamic Analysis

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48
Q

What information can be derived from oil analysis in engines?

A

Condition of the engine and wear rate of components.

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49
Q

What is the process known as Spectrometric Oil Analysis Program (SOAP) used for?

A

To identify metal particles in oil samples.

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50
Q

What do Magnetic Chip Detectors (MCD) monitor?

A

Ferrous material in the oil.

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51
Q

What are the four primary groups of magnetic particles?

A
  • Swarf
  • Magnetic fines
  • Metal flakes
  • Chip
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52
Q

What is swarf?

A

Unwanted material caused during the machining of engine components.

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53
Q

What kind of damage can boroscope inspections identify?

A
  • Cracks
  • Burn marks
  • Hot spots
  • Missing protective coatings
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54
Q

How do modern engines monitor vibration levels?

A

Using piezoelectric accelerometers.

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55
Q

What happens if engine vibration exceeds a predetermined limit?

A

An annunciator light will illuminate.

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56
Q

Fill in the blank: The data from the ACMS is sent to the _______ for analysis.

A

ground-based computer system

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57
Q

What triggers the decision for an engine change?

A

Development of a defect or significant deterioration in engine efficiency.

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58
Q

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

A

To record data and compile ACMS reports.

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59
Q

What is the significance of monitoring metal particle sizes in oil?

A

To detect changes in wear rates and potential system failures.

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60
Q

What is the purpose of a visual inspection of Magnetic Chip Detectors (MCD)?

A

To indicate the internal condition of the engine and gearbox.

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61
Q

How can metal flakes be identified?

A

By examining their shape and source.

62
Q

What can an increase in magnetic fines indicate?

A

A bearing skid has occurred.

63
Q

What should be done with all material found during inspections that does not require immediate rejection?

A

It should be retained to provide a history of wear types.

64
Q

What is the main function of vibration monitoring equipment in gas turbine engines?

A

To continuously monitor the vibration level of the engine.

65
Q

What does the analysis of thermodynamic data allow engineers to plan?

A

Engine removal and overhaul.

66
Q

What is the typical frequency for generating cruise reports?

A

Approximately every four flight hours.

67
Q

True or False: The initial quantities of metal particles in newly overhauled engines should decrease with increased engine hours.

68
Q

What is the purpose of the ACMS take-off reports?

A

To calculate the basic take-off performance of the engine.

69
Q

What are the two main sections of a turbine engine for inspection purposes?

A

Cold section and hot section

70
Q

Why is maintenance of the compressor section important?

A

Damage to the blades can cause severe engine failure

71
Q

What can cause damage to compressor blades?

A

Foreign object matter being sucked into the turbine engine air intakes

72
Q

What is the effect of accumulation of dirt on compressor blades?

A

Reduces aerodynamic efficiency and deteriorates engine performance

73
Q

How can poor engine acceleration and high exhaust gas temperature be rectified?

A

Periodic inspection, cleaning, and repair of compressor components

74
Q

What is the maximum extent of minor damage that can be repaired on compressor blades?

A

Without exceeding the allowable limits recommended by the engine manufacturer

75
Q

What inspection methods are used for repaired compressor blades?

A

Magnetic particle or fluorescent penetrant inspection methods

76
Q

What is the recommended method for reworking damage on compressor blades?

A

By hand using files or emery cloth

77
Q

What should be inspected when examining compressor inducers?

A

Cracks along the leading edges

78
Q

What is Foreign Object Damage (FOD)?

A

Damage caused by loose objects entering the engine

79
Q

What are the usual causes of compressor blade damage?

A

Foreign objects, excessive heat levels, and corrosive agents

80
Q

What type of damage is usually acceptable on compressor stator vanes?

A

Corrosion pitting within allowed tolerance

81
Q

What should be used to blend out damage on compressor vanes?

A

Appropriate blending tools to minimize material removal

82
Q

What should be inspected closely on guide and swirl vanes?

A

Cracks and dents due to impingement of foreign particles

83
Q

What is the appearance of a ‘dent’ in compressor blades?

A

Small, smoothly rounded hollow

84
Q

What is the definition of ‘gouging’ in relation to blade damage?

A

Material displaced from the surface; cutting or tearing effect

85
Q

What should be done if cracks branch or fork on guide vanes?

A

Vane replacement is required

86
Q

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

A

Crucial for prolonging the service life of the engine

87
Q

What should be inspected on the combustion case before opening?

A

Evidence of hotspots, exhaust leaks, and distortions

88
Q

How are cleaning operations typically performed in the hot section?

A

Using emulsion-type cleaners or chlorinated solvents

89
Q

What is the acceptable method of marking parts during assembly?

A

Lightly applied layout dye or chalk

90
Q

What inspection method is used for combustion chambers?

A

Visible dye or fluorescent penetrant inspection method

91
Q

What is the acceptable limit for cracks in combustion chambers?

A

Two cracks progressing from a free edge must not meet

92
Q

What should be done if cracks in the baffle connect more than two holes?

A

Repair is required

93
Q

What is the procedure for cleaning fuel nozzles?

A

Wash with cleaning fluid and remove deposits with a soft bristle brush

94
Q

What is the significance of inspecting the turbine disk?

A

Cracks are not normally permitted and require removal and replacement

95
Q

What should be used to inspect turbine blades for stress cracks?

A

Strong light and magnifying glass

96
Q

What indicates a potential over-temperature condition in turbine blades?

A

Stress cracks or deformation of the leading edges

97
Q

What should be done if the turbine blade outer shroud shows wear?

A

Measure the thickness of the shroud

98
Q

What should be suspected when stress cracks or deformation are found on the leading edges of the first-stage turbine blades?

A

An over-temperature condition must be suspected.

99
Q

What must be checked for each individual blade when inspecting turbine blades?

A

Stretch and the turbine disk for hardness and stretch.

100
Q

What should be done before removing turbine blades for detailed inspection?

A

Number each blade prior to removal.

101
Q

What should be inspected on the turbine blade outer shroud?

A

Air seal wear.

102
Q

What tool should be used to measure the thickness of the shroud at the worn area?

A

A micrometer or another accurate measuring device.

103
Q

What is the consequence if the remaining radial thickness of the shroud is less than specified?

A

The stretched blade must be replaced.

104
Q

Is blade tip curling within a one-half-inch square area on the leading edge usually acceptable?

A

Yes, if the curling is not sharp.

105
Q

What is the cause for removal and replacement of a turbine blade?

A

Any sharp bends that may result in cracking or a piece breaking out.

106
Q

What should each turbine blade be inspected for?

107
Q

What are turbine blades subject to when it comes to replacement?

A

Moment-weight limitations.

108
Q

What may be more economical than replacing several damaged blades?

A

Replacing the entire turbine assembly.

109
Q

How are turbine blades made during the manufacturing build-up process?

A

In coded pairs and laid out in order of moment-weight.

110
Q

What is marked on the rear face of the fir-tree section of the blade?

A

Code letters indicating the moment-weight balance.

111
Q

What must be done if a blade requires replacement?

A

The diametrically opposite blade must also be replaced.

112
Q

What determines the location for turbine blades on modern engines?

A

Computer programs.

113
Q

What is accessible for inspection after removing the required components?

A

The first-stage turbine blades and turbine nozzle vanes.

114
Q

What should be followed for blade limits during inspection?

A

The engine manufacturers overhaul manual.

115
Q

Are slight nicks and dents permissible on turbine blades?

A

Yes, if the depth of damage is within limits.

116
Q

What should be inspected on the nozzle vanes?

A

Nicks or cracks.

117
Q

What indicates a malfunctioning fuel nozzle or combustion chamber in the exhaust section?

A

Hotspots on the tail cone.

118
Q

What must be done to obtain accurate readings when checking clearances?

A

Use special tools provided by each manufacturer.

119
Q

What should be thoroughly inspected in the exhaust section of the turbine engine?

A

Exhaust cone and exhaust nozzle for cracks, warping, buckling, or hotspots.

120
Q

How should turbine engine accessories be inspected and maintained?

A

In accordance with the engine or aircraft manufacturers maintenance manual.

121
Q

What is usually carried out within an engine overhaul shop?

A

Overhaul of turbine engine accessories.

122
Q

What is the primary effect of contaminants in the compressor and turbine sections of an engine?

A

Reduces the efficiency of the engine and can seriously affect its performance.

123
Q

What are the main types of contaminants found in the compressor?

A

Salt and pollution from industrial areas.

124
Q

What is sulfidation in the context of turbine contamination?

A

A build-up of sulphur deposits from burning fuel that destroys the aerodynamic shape of turbine blades and nozzle guide vanes.

125
Q

What is the purpose of a scheduled rinsing of the compressor with fresh water?

A

To avoid harsher chemical treatment required due to salt ingestion.

126
Q

What is a desalination wash?

A

A procedure to rinse the compressor with fresh water while motoring the engine over on the starter or running at idle speed.

127
Q

What is a performance recovery wash?

A

The application of an emulsion-type surface cleaner into the engine intake when a desalination wash is not sufficient.

128
Q

How does heated water affect the cleaning action during compressor washing?

A

Heated water has a better cleaning action than cold water.

129
Q

What is the purpose of injecting abrasive grit into the engine intake?

A

To provide a more vigorous treatment for cleaning, especially in centrifugal compressor engines.

130
Q

What materials are commonly used for abrasive grit in engine cleaning?

A

Broken walnut shells or broken stones from apricots.

131
Q

Why might the abrasive grit cleaning method not effectively clean turbine components?

A

Because the grit is mostly burnt in the combustion chambers.

132
Q

What is one recommended method for cleaning fan blades?

A

Spraying coke, a very fine filtered abrasive, into the eye of the fan while it is rotating.

133
Q

What is a critical warning regarding compressor cleaning?

A

All cleaning must be carried out strictly in line with the engine manufacturers’ instructions.

134
Q

What type of anti-freeze should be used during low-temperature conditions with water for washing?

A

Isopropyl alcohol.

135
Q

True or False: Methanol is safe to use as an anti-freeze during compressor washing.

136
Q

What is Foreign Object Damage (FOD)?

A

An ongoing issue for the safe operation of aircraft engines, particularly turbine engines that can ingest objects from the environment.

137
Q

What can ingestion of foreign matter into a turbine engine cause?

A

Detrimental damage and degradation of engine performance, leading to a shortened engine life.

138
Q

Who must be vigilant for foreign objects in hangar and ramp areas?

A

All maintenance personnel.

139
Q

What are the two types of FOD?

A
  • Internal FOD
  • External FOD
140
Q

What is an example of internal FOD?

A

Loose items in the flight deck that can jam or restrict the operation of control levers.

141
Q

What is Tool FOD?

A

A hazard caused by tools left inside the aircraft after maintenance.

142
Q

What procedures do aircraft maintenance organizations have to prevent Tool FOD?

A

Strict tool control procedures including toolbox inventories.

143
Q

What must tools used during manufacturing have?

A

A serial number for traceability.

144
Q

Give examples of FOD.

A
  • Aircraft parts
  • Rocks
  • Broken pavement
  • Ramp equipment
  • Parts from ground vehicles
  • Rubbish
  • Ice
  • Bird strikes
  • Dust or ash
  • Tools and metal shavings
145
Q

What can small parts lost by an aircraft during take-off and landing cause?

A

Damage to aircraft tires, fuselage, windshield, or can be ingested into another engine.

146
Q

What do airport operations regularly do regarding FOD?

A

Inspect and clear the runways of aircraft FOD.

147
Q

What type of damage can jet engines suffer from FOD?

A

Major damage from even small objects.

148
Q

What test must all manufactured engines pass?

A

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

149
Q

What must the engine fan case be able to do during the FOD test?

A

Contain a detached engine fan blade and prevent damage to the aircraft.

150
Q

What design feature did Boeing add to the early B737 to prevent FOD?

A

Gravel deflectors on the landing gear.

151
Q

What devices were included in the B737 design to reduce FOD risk?

A

Vortex dissipation devices.