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A320 Systems > Power Plant > Flashcards

Power Plant Flashcards

1
Q

When the Engine is Running, what causes the Igniters to Operate Automatically?

A

EIU failure, flame-out detected and ignition delay during start.

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2
Q

What does FADEC do following an Automatic Start Abort?

Hot, Hung, Stall, No Light-off

A

Runs an abort sequence, if a start aborts on the ground, the FADEC:
Closes the HP valve.
Closes the start valve.
Turns off ignition.
Cranks the engine, after the start abort in order to clear out fuel vapours.
Controls any additional start attempts.

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3
Q

During a Normal (Auto) Start what happens at 16%, 22% and 50% N2?

A 
@ 16% ignition starts.
> 22% HP fuel valve opens -> EGT increases -> N1 increases
> 50% start valve closes, Igniter off
- APU speeds returns to normal
- Pack valves reopen
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4
Q

Which is the only Malfunction, which will cause an Auto-abort of an Engine MAN START?

A

On the ground, if the start EGT limit is exceeded before reaching 50% N2, the FADEC aborts the start, in this case only.

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5
Q

Man Start: When should the MSTR switch be selected ON?

A

At max N2, at least 20%.

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6
Q

Man Start: What happens when the MASTER switch is selected ON?

A

Both igniters comes, LP + HP fuel valves open, when N2 > 50% start valve closes and if on the ground, ignition stops. APU speed returns to normal if APU was used.

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7
Q

Man Start: what closes the start valve? And When?

A

FADEC at approximately 50% N2, on the ground, then cutting off the ignition.

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8
Q

What causes the FAULT light to illuminate on the engine panel?

A

Amber light comes on, caution appears on ECAM, if there is an automatic start abort, or a disagreement between the HP fuel valve position and its commanded position.

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9
Q

What do MAN START pushbuttons control?

A

ON: start valve opens if the ENG MODE selections is set to CRANK or IGN/START and N2 < 20%, both packs valves close during the start sequence, start valves closes when N2 > 50%.

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10
Q

What is at One End of the TRANSIENT N1, and what is at the other?

A

Actual N1 (Green) and N1 command (N1 trend) in green.

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11
Q

On the EGT what does the amber index indicate?

A

The amber index appears at 725 degrees during engine start, then 915 degrees (max EGT).

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12
Q

What does REV in amber / green indicate?

A

Amber: when nay one blocker door is unstowed or unlocked.
Green: when all four doors are fully deployed.

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13
Q

How can you tell that the Start Sequence has finished?

A

Amber arc increases from 725 degrees to 915 degrees (max start – max continuous EGT).
Grey background N2 box disappears.

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14
Q

When does IDLE flash (between the N1 gauges)?

A

When both engines are idle, it flashes f

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15
Q

When is fuel used seat to zero?

A

The green number is computed by the FADEC, it resets when the engine starts on the ground.

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16
Q

What is the maximum taxi speed?

A

30kts

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17
Q

What are the limiting EGT, and operating time, at TOGA power?

A

635 degrees: 5 mins (2-engines) or 10 mins (1-engine)

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18
Q

What are the starter limitations?

A

3 consecutive cycles, 15 sec pause between each attempts.
(Maximum 2 min start cycle time for manual start)

No running engagement of the starter, when N2 is above 10% on the ground and 18% in flight.

30 min cooling period, following 3 starts attempts or 5 min of continuous cranking.

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19
Q

What is the minimum IAS for Full Reverse Thrust?

A

70kts

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20
Q

Why should Engines be operated at Idle for several minutes before take-off?

A

> 2 mins to ensure centre tank pump test finished, engine wear, to prevent thermal shock.

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21
Q

When, and for how long, are FADECs powered?

A

First 5 mins after aircraft is powered, then self-powered above 58% N2 until 5 mins after 2nd engine shutdown.

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22
Q

IAE V2524-A5 (24,000#)

A

What engine is in the A319?

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23
Q

IAE V2527-A5 (27,000#)

A

What engine is in the A320?

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24
Q

IAE V2530-A5 (32,500#)

A

What engine is in the A321?

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25
Q

Fan, LP compressor and LP turbine

A

What is on the N1 shaft?

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26
Q

HP compressor and HP turbine

A

What is on the N2 shaft?

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27
Q

Fuel PumpOil PumpAlternatorPowered by the N2 shaft

A

What is on the accessory gearbox and what are they powered b

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28
Q

Fuel flow, thrust reverser and ignition controlN1, N2 and EPR limits protectionEGT limits protectionStarter engagement time and speed protectionFuel and Thrust limit computationsComputation of thrust penaltiesAccelleration and deceleration schedulesIdle settingsEngine information to cockpit

A

What are the functions of the FADECs?

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29
Q

Controls start sequenceProvides full protectionsHas start abort authority

A

What does the FADEC control during ground starts?

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30
Q

Start abort authorityEGT protection

A

What FADEC feature is only available during ground starts?

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31
Q

Monitors and provides cautions and warnings

A

What does the FADEC do during manual starts?

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32
Q

Modulated Idle: on ground and in-flight when slats retracted (lowest idle, long spool up times)Approach idle: in-flight when slats are extended (low spool up time for go arounds)Reverse Idle: REV IDLE position (slightly higher than modulated idle)

A

What are the 3 idle settings?

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33
Q

P5 (LP turbine exhaust) vs P2 (engine inlet pressure)

A

How is (EPR) Engine Pressure Ratio calculated?

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34
Q

EPR (Engine Pressure Ratio)N1

A

What are the 2 modes of the FADEC for setting thrust?

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35
Q

Thrust Lever Angle (TLA)AltitudeMach NumberAmbient TemperatureAir inlet total temperatureAir bleed demands

A

When the FADEC regulates thrust in EPR mode, what are the pa

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36
Q

No AutothrustNo Alpha Floor

A

When EPR mode fails, the FADEC reverts to N1 mode. What impo

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37
Q

Rated N1 modeUnrated N1 mode

A

What are the 2 types of N1 mode?

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38
Q

Rated N1 Mode: N1 limits and protections are displayed on E/WD, can be selected manuallyUnrated N1 Mode: Used with EPR and Rated N1 mode failures. N1 limits not displayed and FADEC provides limited overspeed protection. (emergency)

A

What is the difference between Rated and Unrated N1 modes?

39
Q

Channels A and B provide backup and redundancy

A

What is the redundancy within the FADEC?

40
Q

N2>10%

A

When does the engine alternator provide power to the FADEC?

41
Q

By heat exchange with the fuel

A

How is the IDG and Engine Oil cooled?

42
Q

ENG ANTI ICE ONTake off thrust selectedEngine Interface Unit (EIU) failsApproach Idle (slats extended)Engine flameout or surge detectedENG MASTER cycled on-off-on

A

When does the FADEC command continuous ignition?

43
Q

Translating Sleeve, which redirects Fan Air only

A

What type of reverse thrust is used?

44
Q

At least 1 FADEC channel opLanding Gear Control and Interface Unit (LGCIU) detects aircraft is on the ground.

A

What does the thrust reversers require prior to activation?

45
Q

Auto start is abortedStart valve faultHP fuel valve not in commanded position

A

When would you get a FAULT light on the engine control secti

46
Q

Manually selects continuous ignitionPrepares the engine for the start process

A

What does the IGN/START switch do?

47
Q

Prepares the engine for dry cranking (no ignition or fuel flow)Starter will engage when MAN START is selected

A

What does the CRANK switch do?

48
Q

5 minutes

A

How long is TOGO powered limited to?

49
Q

Max reverse should not be used below 70 kts

A

What is the speed limitation of Max Reverse?

50
Q

Armed: during TOGO or FLX or when Thrust levers not in active range (between CLB and IDLE)Active: pushing the FCU A/THR pb

A

What are the 2 auto-thrust modes?

51
Q

The lever now become thrust limiters, therefore us leave them at the CL detent to give auto-thrust full authority.Note: the exception is when Alpha Floor is activated in which TOGA power is activated regardless of lever position

A

When auto-thrust is activated, what do the levers do?

52
Q

Disengage buttons on the leversSelecting A/THR pb offMoving the thrust levers to idle (landing)

A

How can you disengage auto-thrust?

53
Q

TOReverseAlpha floor

A

The amber tick mark on the EGT gauge is the calculated max E

54
Q

Highest value achieved

A

What is the red tick mark on the EGT gauge?

55
Q

N1 went above 100%

A

What does a + by N1 mean?

56
Q

<80psi

A

When will the oil pressure be amber?

57
Q

<60psi

A

When will the oil pressure be red?

58
Q

> 155C

A

When will oil temp be amber?

59
Q

> 155C for 15 minutes or >165C

A

When will oil temp be red?

60
Q

5 units

A

When will vibration pulse?

61
Q

2 because it provides pressure for the yellow hydraulic system which provides parking brake pressure

A

Which engine is started first and why?

62
Q

2,4,6,8,1020% N1400 EGT60% N2800 Fuel Flow1.0 EPR

A

What is the memory air for ensuring a stabilized engine star

63
Q

To allow the engine to reach its max motoring speed prior to ignition and fuel flow

A

Why would you manually start an engine?

64
Q

Engine StallEGT overlimitLO START AIR PRESSNo N1 rotationHungstartIGN A/B Fault

A

When is a manual start recommended?

65
Q

15% N2

A

What is the minimum N2% required for a manual start prior to

66
Q

N2 between 43-48%

A

When does the FADEC close the start valve?

67
Q

Extending engine lifeless fuel

A

What are the advantages to a FLEX TO?

68
Q

Prevents N1 from stabilizing 60-74% N1, thus when you advance thrust levers, it will skip this range

A

What does the FADEC do to reduce Fan Flutter?

69
Q

1.1 EPR

A

What EPR valve do you aim for to ensure proper engine indica

70
Q

Only the LP fuel valve is closed causing a 40 second delay as the fuel in the line is burned.

A

When shutting down the engine using the ENG FIRE button what

71
Q

Starter time exceededEGT overtempNo light offLower than normal N1Starter failureHung Start

A

When will the FADEC abort a start on the ground and indicate

72
Q

Loss of the max N1% tick mark

A

How can you tell if the FADEC reverted to UNRATED N1 mode?

73
Q

When FLEX temp is within 10 degrees of OAT to avoid asymmetrical thrust (EPR/N1 discrepancy)

A

At what OAT would you select TOGA rather than FLEX?

74
Q

The FADEC system is self-powered above 10% N2. In case of a FADEC self-power loss the aircraft electrical network automatically supplies the FADEC.

A

When does the self powering of the FADEC start?

IAE Engines

75
Q

The FMV controls the fuel flow protects against overspeeding controls the shut off valve and supplies high pressure fuel to the various actuators.

A

What is the function of the fuel metering valve (FMV)?

IAE Engines

76
Q

The ignition system is used to start the engine on ground and to restart it in flight. it consists of two identical independent circuits for each engine normally controlled by the FADEC channel A with channel B on standby. Each FADEC channel can control both igniters.

A

How does the ignition system work?

IAE Engines

77
Q

Control of gas generator protection against engine exceeding limits power management automatic engine starting sequence manual starting sequence thrust reverser control fuel recirculation control transmission of engine parameters and engine monitoring information detection isolation and recording of failures FADEC cooling and protection against fan flutter.

A

The FADEC system performs the following functions…

IAE Engines

78
Q

The engine start system consists of an air turbine starter and a start valve. The start valve admits air supplied by the pneumatic system to operate the starter. The FADEC controls the start valve electrically. If electrical control fails when the aircraft is on the ground a handle allows the start valve to operate manually.

A

How does the engine start system work?

IAE Engines

79
Q

There are 5 thrust lever positions: TO/GA, FLX/MCT, CL, IDLE and MAX REV.

A

How many thrust lever positions are there and how are they labeled?
(IAE Engines)

80
Q

If no EPR is available (either sensed or computed) the affected FADEC will automatically revert to N1 mode.

A

Is a N1 mode available?

IAE Engines

81
Q

When on ground at low speed the EEC protects against fan flutter. In so doing the EEC prevents the engine from being stabilized between an approximate range of 60% to 74% N1 (depending on the outside air temperature). Therefore during engine acceleration on ground the pilot may notice a non-linear thrust response to thrust lever movement.

A

How does the protection against fan flutter work?

IAE Engines

82
Q

The oil system contains the oil tank the lube and scavenge pump modules the fuel/oil heat and air/oil heat exchangers the filters chip detectors pressure relief and bypass valves.

A

What are the main components of the oil system?

IAE Engines

83
Q

The FADEC has two-channel redundancy with one channel active and one channel in standby. If one channel fails the other automatically takes control.

A

How many channels has the FADEC?

IAE Engines

84
Q

Approach idle allows the engine to accelerate rapidly from idle to go-around thrust.

A

What is the purpose of approach idle?

IAE Engines

85
Q

These numbers are normally green. They become amber and an associated warning appears on the ECAM if the temperature exceeds 165°C or exceeds 155°C for more than 15 minutes or is below -10°C.

A

When does the oil temperature indication become amber?

IAE Engines

86
Q

Modulated idle approach idle and reverse idle.

A

What are the idle modes of the FADEC?

IAE Engines

87
Q

The engine thrust setting is made through the control of the Engine Pressure Ratio (EPR).

A

What is the main parameter to control the engine thrust?

IAE Engines

88
Q

The fuel oil heat exchanger enables fuel to be heated by the oil to reduce temperature of the oil and prevent fuel icing.

A

What is the function of the fuel oil heat exchanger?

IAE Engines

89
Q

The oil tank the lube and scavenge pump modules the fuel/oil heat exchangers the filters chip detectors pressure relief and bypass valves.

A

What are the components of the engine oil system?

IAE Engines

90
Q

The reverse thrust is obtained by deflecting the fan airstream. This is done when the translating sleeves are fully deployed rearward thus enabling the pivoting blocker doors to forward divert the fan flow through the cascades.

A

How does the reverse thrust system work?

IAE Engines

91
Q

FLEX/MCT and TO/GA.

A

Take off can be done using which power settings?

IAE Engines

92
Q

EPR, EGT and N1.

A

What are the primary parameters on the upper E/WD display?

IAE Engines

93
Q

Approach idle is selected in flight when the flaps are extended (FLAPS lever not at zero position).

A

When is approach idle selected?

IAE Engines

94
Q

A dry cranking cycle ventilates the engine to remove fuel vapours after an unsuccessful start attempt on the ground. The flight crew can manually select cranking by setting the ENG MODE selector to CRANK and the MAN START pushbutton to ON (MASTER switch OFF).

A

What is the purpose of engine ventilation (dry cranking)?

IAE Engines

A320 Systems (21 decks)

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