Review Questions - Electrical Flashcards

1
Q

What starts the battery charging cycle on the ground?

A

Selecting the BATT pushbuttons to AUTO with EXT PWR ON.

Charging cycle takes approximately 20 minutes

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2
Q

Will the batteries completely drain if you leave the BAT switches in AUTO after AC power is removed?

A

No. Battery cut-off logic prevents complete discharge when the aircraft is on the ground and unpowered – 22VDC

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3
Q

How is the BATTERY BUS normally powered?

A

DC BUS 1 through a DC tie contactor

DC BUS 1 is supplied from TR1

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4
Q

What does the amber FAULT light in the GALY & CAB pb indicate?

A

At least 1 generator load is above 100% rated output

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5
Q

How does the GALY & CAB pb work in AUTO?

A

a. Sheds main galley and in-seat power supply if:
b. Only 1 generator (APU or Engine) is available in FLIGHT, or
c. Only 1 ENGINE generator is available on the GROUND

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6
Q

What does a FAULT on the ENG GEN pushbutton indicate?

A

The generator line contactor is open because of a fault detected by the Generator Control Unit (GCU) which could include:

a. Overload
b. Over/under voltage
c. Differential fault (short), and/or;
d. The generator line contactor is open

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7
Q

What does the APU GEN FAULT light indicate?

A

The generator line contactor is open because of a fault detected by the GCU

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8
Q

What is the function of the BUS TIE in the AUTO position?

A

a. Allows the BUS TIE CONTACTORS to open and close automatically to maintain power to both AC BUS 1 & 2:
b. Allows a single source to power the entire system
c. Allows connection of the APU GEN or EXT PWR to the system
d. Inhibits multiple sources to connect simultaneously

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9
Q

What does an IDG FAULT light indicate?

A

OOL

a. Oil pressure low (inhibited when N2 < 14%)
b. Oil outlet temperature overheat
c. Light is inhibited when IDG is disconnected

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10
Q

What precautions must be taken when disconnecting an IDG?

A

a. Disconnect only when the engine is running or windmilling
b. Do not hold button longer than 3 seconds

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11
Q

How can an IDG be reset?

A

On the ground by maintenance

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12
Q

What is the function of the AC ESS FEED pushbutton in the normal position?

A

Allows AC BUS 1 to power the AC ESS BUS

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13
Q

How is AC ESS FEED transferred from AC BUS 1 to AC BUS 2?

A

Manually by selecting ALTN on the AC ESS FEED pushbutton or automatically if AC BUS 1 is lost and the switch is in the normal position.

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14
Q

What does the AC ESS FEED pushbutton white ALTN light indicate?

A

AC BUS 2 is powering the AC ESS BUS

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15
Q

What is the purpose of the static inverter?

A

To provide AC power to the AC ESS bus from the battery when the EMER GEN is not online when in the Emergency Electrical Configuration

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16
Q

What are the 3 times the batteries are connected to the BATTERY BUS?

A

a. APU start
b. Battery charging
c. AC BUS 1 & 2 not powered and airspeed below 100 knots

17
Q

What is the priority sequence for electrical power?

A

GEARB

Generators - Engine

EXT PWR (manually selected)

APU Generator

RAT Emergency Generator

Batteries

18
Q

What is the significance of the green and red collared circuit breakers on the Flight Deck?

A

Green – Monitored by ECAM system

Red – Wing tip brake C/B

Black – Not monitored by ECAM

19
Q

What buses are powered by the emergency generator?

A

AC ESS and AC ESS SHED

DC ESS and DC ESS SHED

20
Q

What is the function of the MAN ON pb on the EMER ELEC PWR Panel?

A

AUTO - RAT will automatically extend if AC BUS 1 & 2 are not powered and airspeed > 100 knots

MAN - extend the RAT at any time

21
Q

How long does it take the RAT to extend and provide power?

A

8 seconds (3 seconds for RAT extension, 5 seconds to pressurize the Blue hydraulic system and power the EMER GEN)

22
Q

What does the red RAT & EMER GEN fault light on the EMER ELEC PWR Panel indicate?

A

The emergency generator is not supplying power when AC BUS 1 and AC BUS 2 are not powered

23
Q

What powers the emergency generator?

A

Blue hydraulic power from the RAT

24
Q

What is the difference in functionality of the MAN ON pb (EMER ELEC PWR Panel) and the RAT MAN ON pb (HYD Panel)?

A

Deploying the RAT with the RAT MAN ON pb on the HYD panel only provides Blue Hydraulic pressure - No emergency generator.

25
Q

What happens when you push the GEN 1 LINE pushbutton?

A

a. GEN 1 Line Contactor opens and the white OFF light illuminates
b. AC BUS 1 is powered by GEN 2 through the BUS TIE CONTACTOR
c. GEN 1 continues to power 1 fuel pump in each wing tank

26
Q

When is the GEN1 Line pushbutton used?

A

During smoke procedures

27
Q

What does the amber SMOKE light in the GEN 1 LINE pushbutton indicate?

A

Smoke is detected in the avionics bay

28
Q

How would you know if the Blower and Extract fault lights were due to smoke?

A

SMOKE Light on the EMER ELEC PWR Panel and an ECAM warning