Aural/ Visual Warning System Flashcards

1
Q

What does DCU stand for?

A

Data Concentrator Unit

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2
Q

What does LDU stand for?

A

Lamp Driver Unit

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3
Q

What does AECU stand for?

A

Audio Electronic Control Unit

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4
Q

What buttons on the EICAS Controller will remain operational even during the event of a complete AC failure?

A

PRI, STAT, STEP, CAS

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5
Q

A triple chime is accompanied with a what?

A

Master warning

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6
Q

Take off configuration warnings are armed when engines are above 70% and?

A
  • Brakes, parking
  • Flaps not set for t/o
  • Autopilot engaged
  • Spoilers not retracted
  • Trim not in t/o range

B.F.A.S.T.

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7
Q

During take off, the DCU inhibits caution messages when?

A
  • Both engines greater than 79% N1
  • IAS >80kts
  • Weight on wheels
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8
Q

During landing, the DCU inhibits caution messages when?

A
  • Less than 400ft AGL
  • Gear down
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9
Q

What does MDC stand for?

A

Maintenance Diagnostic Computer

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10
Q

What does HLIS stand for?

A

Hard landing indication system

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11
Q

If an annunciated system malfunction CAS message suddenly extinguished, it indicates what?

A

The malfunction no longer exists

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12
Q

The master caution lights can be reset:

A

Any time by depressing either master caution switch light

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13
Q

The colour CAS message that indicates requiring attention but not immediate action is?

A

Amber (caution)

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14
Q

Of the aural sounds, the one that can be muted is the?

A

Voice

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15
Q

Most cockpit switch lights are dimmed how?

A

By selecting the BRT/DIM switch to DIM

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16
Q

ED1 displays?

17
Q

ED 2 displays?

18
Q

Clacker sound means?

A

VMO/MMO/ flap overspeed

19
Q

What button will cycle through the main pages if the buttons do not work?

20
Q

When is the cabin pressurisation shown on ED1?

A

Only when it is in the manual mode

21
Q

How long after the gear and flap are up does the indications leave the primary page?

A

30 seconds

22
Q

APU/ EGT displays when?

A

PWR FUEL button selected

23
Q

What are the synoptic pages?

A
  1. ELEC (AC/DC)
  2. Hydraulic
  3. Flight controls

Second “bump” of Elec cycles between AC & DC

24
Q

In the event of ED1 failure, how can you restore the primary page?

A

It automatically transfers to ED2

25
Q

Caution inhibit is cancelled when?

A

Both engines are less than 67.6%
RADALT >400ft with landing gear extended
30 seconds after the inhibit began
30 seconds after air to ground transition

26
Q

Which messages on the EICAS can be cleared from view? How?

A

Cautions with the CAS key of the ECP, Status messages with the STAT key.

27
Q

How can amber CAS messages be hidden?

A

Push CAS button

28
Q

When can CAS messages be hidden?

A

When both main generators are on line

29
Q

Moving EICAS information from one display to an alternate display is done via the:

A

Reversionary Control Panel