Power Plant Flashcards

1
Q

How many FADECs does each engine have

A

Two single channel FADECs

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2
Q

Where are the engine indications and alerts displayed

A

On the EICAS

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3
Q

Which position of the ignition selector knob allows the FADEC to control the ignition system depending on engine requirements

A

Auto

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4
Q

Which thrust position provides the maximum thrust rating available for dual or single engine operation

A

Max

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5
Q

Which thrust lever position selects the takeoff and go-around thrust and mode settings

A

TO/GA

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6
Q

What does pressing the EVENT MARKER button cause the ECU (FADEC) to do

A

Records a total of 3 mins (two before and one after the button is pressed)

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7
Q

When is the OAT in the EICAS indication displayed?

A

Up until the takeoff run

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8
Q

What are the thrust reversers used for and during what condition of flight

A

An on ground additional braking device used for landing and RTO only

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9
Q

Is backing up the airplane in reverse thrust allowed?

A

No

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10
Q

Upon landing, when should the thrust reversers be stowed

A

40 KIAS

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11
Q

When are the TRs available

A

With WOW and a wheel speed

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12
Q

What icon on the EICAS indicates the current status of the TRs

A

a REV icon

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13
Q

What color icon indicates that the TRs are commanded and in transition.

A

an amber REB icon

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14
Q

Where is the IGNITION status displayed

A

on the EICAS

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15
Q

What does a green IGN indicate

A

The ignitions are commanded on

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16
Q

What icon on the EICAS indicates that the ignitors are commanded to OFF

A

A cyan IGN OFF

17
Q

Where can the oil level be accurately read

A

Either in the sight glass or measured via the Remote Oil Level Sensor (ROLS)

18
Q

When can the oil level be accurately read

A

from 5 to 30 mins after shutdown

19
Q

Is the engine oil quantity indication visible with an engine running or in flight

A

No

20
Q

What is the maximum oil consumption rate of the engine per hour

A

.04 qts per hour

21
Q

List the three sources of air pressure that the ATS can use for start

A

1) APU
2) Cross side engine
3) Huffer cart

22
Q

What is the purpose of the ATTCS

A

To provide automatic thrust increase if the ATTCS is previously armed and any of the following conditions is true on takeoff or go-around:

1) OEI condition detected (N2 Delta of more than 15%)
2) Loss of engine cross communication
3) Wind shear
4) TL is moved to the MAX position

23
Q

When is ATTCS function available

A

When WAI is on “ICE PROT” mode is in the ALL position.

24
Q

Which takeoff ratings may be selected by the flight crew prior to takeoff

A

The full rate mode (TL-1) and the one de-rated mode (TL-2)

25
Q

List the engine power settings that may be selected by the flight crew

A
Takeoff/ Go Around (TOGA)
Max Continuous (CON)
Climb (CLB) 
Cruise (CRZ)
Max Reverse (for RTO)
26
Q

When can HP thermal bow occur. If an engine re-start is desired within that period of time, what is the recommended procedure.

A

When engine starts are initiated between 15 and 180 mins after an engine shutdown. Dry motor the procedure in accordance with the checklist procedure.