Electrical Flashcards

1
Q

A FAULT light in the GALY & CAB pb appears when any generator load is above 100% of its rated output.

A

True

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2
Q

When external power is connected to the aircraft, a green AVAIL light indicates:

A

External power is connected with acceptable voltage and frequency.

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3
Q

The RAT automatically deploys when:

A

Power is not available for AC Bus 1 and AC Bus 2 and airspeed greater than 100 knots.

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4
Q

You can deploy the RAT and activate the emergency generator using the MAN ON pb.

A

True

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5
Q

The AVAIL light illuminated on the EXT PWR pb means:

A

Voltage and frequencies are acceptable

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6
Q

What electric source has priority with the engines off, APU available and the EXT PWR pb switch is ON.

A

EXT PWR

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7
Q

Disconnecting an IDG:

A

Renders the associated electrical generator inoperative

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8
Q

The RAT OUT memo appears on the E/WD to indicate:

A

The RAT has deployed.

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9
Q

The RAT automatically deploys when:

A

Power is not available for AC Bus 1 and AC Bus 2 and airspeed greater than 100 knots.

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10
Q

You can deploy the RAT and activate the emergency generator using the MAN ON pb.

A

True

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11
Q

The APU generator always takes priority over an engine driven generator and/or external power.

A

False

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12
Q

The APU driven generator:

A

Can be used as the sole source of electrical power on the ground.

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13
Q

When the APU generator is on and no other AC sources are available, the APU can power the entire electrical system on the ground.

A

True

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14
Q

AC ESS Bus ensures:

A

Essential equipment will remain powered during an electrical emergency

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15
Q

DC ESS Bus ensures that essential DC powered equipment remains operational during an electrical emergency.

A

True

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16
Q

On battery power only, the AC and DC ESS SHED Busses are shed to conserve battery life.

17
Q

The indication highlighted is displayed when the Emergency Generator:

A

Is not in use

18
Q

The “RAT OUT” memo on the E/WD indicates:

A

The RAT has deployed

19
Q

The SMOKE light illuminates in GEN 1 LINE pb when:

A

Smoke is detected in the avionics ventilation duct.

20
Q

AC Bus 1 normally powers:

A

AC ESS Bus and TR 1

21
Q

AC Bus 2 normally powers: