Aural and Visual Warnings Flashcards

1
Q

What happens if ED1 fails in flight?

A

The PRI page is automatically transferred to ED 2.

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2
Q

When are N1 vibration gauges displayed?

A

After engine start after both engines are stabilized at idle and oil pressure is normal.

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3
Q

When is APU door position displayed?

A

Always

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4
Q

What are the conditions for a takeoff config. warning?

A

Power is advanced more than 70% N1, and the aircraft is not in takeoff configuration.

Takeoff Config warning system monitors the positions of the flaps, flight spoilers, parking brake, autopilot, aileron/rudder/stab trims.

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5
Q

When EICAS displays are operated on the ground without AC power, what limitation should be taken into account?

A

Do not operate for more than 5 minutes without AC power, as ED 1 and 2 will not be cooled.

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6
Q

What is the function of the DCU?

A

Collect data from various aircraft systems and relay it to the proper component or display.

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7
Q

Should the ECP fail, there are four mechanical buttons which will retain their function, what are they?

A

PRI, STAT, CAS, STEP

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8
Q

When are landing gear and flaps removed from the PRI display page?

A

Landing gear is up and locked.
Flaps are up.
BTMS is normal.

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