Engines Flashcards

1
Q

What engines are used on the e190?

A

CF34-10E5A1

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2
Q

Describe the CF34-10E5A1 engine

A

High bypass, axial flow, dual rotor turbofan

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3
Q

How are the engines controlled?

A

By a FADEC

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4
Q

How many channels does the engine FADEC have?

A

2

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5
Q

What are the two possible paths fuel can take?

A
  • through the high pressure pump and back to the fuel tank
  • through the FOHE, through the filter and into the FMU
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6
Q

What does the engine starting system consist of?

A
  • air turbine starter
  • starter control valve
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7
Q

How many igniters are there per engine?

A

2

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8
Q

How many igniters are used when starting an engine?

A

On ground = 1
In flight = 2

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9
Q

What does the OVRD position do on the ignition selector knob?

A

Ignites both igniters

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10
Q

What are the 4 stages to an on ground engine start?

A

1) FADEC initiates ignition at 7% N2
2) fuel flow metering valve (FMV) opens between 20-25% N2
3) after light off, FADEC commands starter cut out at approx 50% N2
4) FADEC commands FMV to accelerate engine to ground idle speed

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11
Q

During an on ground engine start what happens if there is no light off within 15 seconds of fuel on?

A

FADEC turns ignition off and dry motors for 30 seconds

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12
Q

What is the only difference between a cross bleed start and an on ground start?

A

FMV opens if N2 has not reached 15% after 15 seconds

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13
Q

What is the only difference between an on ground start and a windmill start?

A

FMV opens at min 7.2% N2 or 15 seconds (whichever comes first)

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14
Q

During a windmilling start when should the start be manually aborted?

A

If no light off within 15 seconds of fuel on

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15
Q

What does the FADEC not protect for during starts in flight?

A

Hot, hung or no light off starts

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16
Q

What icon is shown on the EICAS during an auto relight?

A

WML

17
Q

When should an auto relight be manually aborted?

A

If no light off within 30 seconds or N2 falls below 7.2%

18
Q

If one thrust reverser has failed what happens if both thrust levers are selected to max reverse?

A

Only minimum reverse thrust is available

19
Q

If one thrust reverser has failed what happens if the operative thrust lever is selected to max reverse?

A

Max reverse is given on the operative engine

20
Q

What is the configuration of the FADEC channels?

A

2 channels in active/standby configuration. The active one is switched at every engine start

21
Q

How is the FADEC powered?

A
  • PMA above 50% N2
  • 28V DC below 50% N2
22
Q

When does ATTCS command reserve power?

A
  • difference between n1 values is greater than 15%
  • one engine failure during takeoff
  • one engine failure during go around
  • windshear detection
23
Q

How can ATTCS be manually activated?

A

By moving the thrust levers to max

24
Q

What is minimum flex takeoff thrust?

A

75% max rate takeoff thrust or CLB-2 +1% (whichever is highest)

25
Q

What are the 4 idle modes?

A

Flight
Approach
Final approach
Ground

26
Q

What is indicated by a cyan line on the n1 display?

A

Minimum n1 needed for anti ice

27
Q

What does the FADEC give protection against during ground starts?

A

Hung, hot and no light off starts

28
Q

When does the FADEC command engine shutdown?

A

If n2 reaches 102%

29
Q

What is max ITT for fuel flow on ground?

A

120 Celsius