Powerplant System Flashcards

1
Q

Low oil level produces what CAS message?

A

Amber OIL LEVEL LOW message.

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2
Q

Ignition buttons in Normal on MFD GTC Propulsion page cause ignition to be controlled by what?

A

FADEC

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3
Q

If N1 shaft fails, ____ automatically shutdown the engine.

A

Mechanical Emergency fuel shutoff valve.

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4
Q

FADEC is powered by ____ during normal operation.

A

PMA, Permanent Magnet Alternator.

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5
Q

N1 Gauge indication of cruise (CRU).

A

Inward pointing white line.

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6
Q

N1 Gauge indication. If Max Continuous Thrust (MCT).

A

Outward Pointing white line.

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7
Q

T Bug indicates.

A

Throttle position.

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8
Q

T Bug determines where FADEC sets ____ bug.

A

V bug.

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9
Q

Battery power should not be turned off for ____ , to allow data transfer from EEC to EDU.

A

30 seconds.

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10
Q

Is Engine Sync manual or automatic?

A

Automatic.

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11
Q

Green ignition indicators (IGN) indicate what?

A

Power to Exciter boxes, not actual ignition firing.

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12
Q

EVENT MARKER records ____ before and ____ after.

A

1:45 before and after, total 3.5 minutes of data recording.

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13
Q

RUN pushed at ____ % N2 Minimum during start.

A

9%

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14
Q

FADEC aborts if?

A

1: No ITT rise within 15 seconds of RUN.
2: Exceeds ITT Limit.

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15
Q

Pilot aborts Start if?

A

1: No Oil Pressure within 20 seconds of ITT rise.
2: No N1 rotation by 40% N2.
3: No stabilized idle by 90 seconds of ITT rise. (Ground Idle is 57% N2)

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16
Q

Inflight engine starts aborted by ____?

A

Pilot.

17
Q

Inflight Engine starts aborted of stabilized flight idle is not ____% within 90 seconds of ____ .

A

65%, ITT rise.

18
Q

What signifies complete engine start sequence?

A

1: N1 Gauge T and V bugs
2: White ENGINE SHUTDOWN CAS message clears.

19
Q

What does a White ENGINE SHUTDOWN CAS message indicate?

A

Pilot initiated engine shutdown versus failure.

20
Q

Ground IDLE occurs ____ after touchdown.

A

8 seconds.

21
Q

Automatic engine shutdown by FADEC if N1 or N2 reaches ____%

A

110%

22
Q

Inflight Engine failure causes halo around ____ Button to flash.

A

RUN/STOP

23
Q

Takeoff Thrust limits.

A

5 minutes with 2 engines, 10 minutes with 1 engine.

24
Q

Wait ____ at idle power prior to shutdown on ground for ITT to stabilize.

A

2 minutes.

25
Q

To cool generators, idle Thrust with load < 75 amps for ____ prior to shutdown OR do not restart engines for ____ .

A

4 minutes, 35 minutes.

26
Q

Thrust Reversers are ____ controlled and ____ actuated.

A

Electrically. Hydraulically.

27
Q

Thrust Reversers will not operate without ____ squat switches indicating WOW.

A

3

28
Q

Throttles aft of idle inflight has what effect on Thrust Reversers? On landing?

A

No effect inflight. Deployment on ground.

29
Q

T/R EMER STOW Button does what?

A

1: Opens Isolation Valve.
2: Direct control valve to stow position which causes T/R ARM indication until EMER STOW is deselected.

30
Q

Thrust Reverser deployment inflight causes FADEC to command engine to ____ .

A

Idle.

31
Q

Thrust Reverser deployment inflight cause T/R EMER STOW Button to come on steady or flashing?

A

Flashing until pushed, then steady.

32
Q

Max speed with thrust Reverser deployment inflight?

A

150 Knots. Allows aerodynamics Forces to stow easier.

33
Q

True or False: Thrust Reverser check required before every flight.

A

False. Once per day, or after maintenance or TR required for landing numbers.

34
Q

Idle reversers by ____ Knots.

A

65 Knots.

35
Q

Thrust Reverser deployment limited to ____ with APU operating.

A

30 Seconds.

36
Q

Thrust Reverser deployment limited to ____ without APU Operating.

A

5 minutes.