Electrical Flashcards

1
Q

How many batteries and what type are installed

A

2 Lead Acid

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2
Q

What is the AMP Hour Rating for each battery

A

Batt 1: 34
Batt 2: 36 (48 with Mod)

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3
Q

What is the minimum recommended battery temperature for battery start

A

Standard: -10C
Modified: -18C

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4
Q

What is the minimum voltage required for a battery start

A

24V

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5
Q

Configuration: On ground, BATT 1 and BATT 2 in the OFF position, Which buses are powered?

A

HOT BATT BUS 1 and HOT BATT BUS 2

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6
Q

Configuration: On ground, BATT 1 and BATT 2 in the ON position. Which buses are powered?

A

1) HOT BATT BUS 1
2) HOT BATT BUS 2
3) EMERGENCY BUS
4) DC BUS 1
5) DC BUS 2
6) CENTRAL BUS

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7
Q

What is the voltage range for the aircraft to accept GPU power?

A

25-30V

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8
Q

What is the indication that the aircraft is accepting GPU power?

A

GPU AVAIL

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9
Q

What is the function of the 1 OPEN or 2 OPEN position of the BUS TIE switch

A

Forces the respective bus tie open against system logic, The opposite side functions normally.

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10
Q

On the ground, if the BATT 1 and BATT2 are in the on position, the GPU is connected and powered and button pushed in and the electrical system indicates 28V. Which buses are powered

A

All of them

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11
Q

Which buses and equipment are powered by BATT 2 during engine start?

A

1) HOT BATT BUS 2
2) CENTRAL BUS
3) ENGINE STARTER

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12
Q

Which buses are powered by BATT 1 during engine start?

A

1) HOT BATT BUS 1
2) EMERGENCY BUS
3) BOTH DC BUSES

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13
Q

How does DC BUS 2 receive power during engine start

A

Quiet Start Contactor

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14
Q

Which buses are depowered during engine start

A

1) SHED BUS 1
2) SHED BUS 2

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15
Q

What are the positions of the Bus Tie Contactors (BTC 1 and 2) during engine start

A

Both Open

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16
Q

What are the positions of the Bus Tie Contactors (BTC 1 and 2) during normal ops

A

BTC 1: Open
BTC 2: Closed

17
Q

In flight, during normal ops, which buses are powered by GEN 1

A

1) HOT BATT BUS 1
2) EMERGENCY BUS
3) DC BUS 1
4) SHED BUS 1

18
Q

In flight, during normal ops, which buses are powered by GEN 2

A

1) HOT BATT BUS 2
2) CENTRAL BUS
3) DC BUS 2
4) SHED BUS 2

19
Q

In flight, with a GEN 1 failure, what happens to the contactors and what buses are lost (if any)

A

1) Generator Line Contactor 1 Opens
2) Shed Buses 1 and 2 Contactors Open
3) Bus Tie Contractors (BTC) 1 Closes and BTC 2 Remains Closed
4) You lose both the SHED buses only.

20
Q

In flight if GEN 1 already failed and GEN 2 fails (Electrical Emergency) What is the position of the contractors and what buses do you have remaining?

A

1) GLC 1 remains open GLC 2 Opens
2) SBC 1 and 2 remain Open
3) BTC 1 and 2 Open
4) Emer Bus Contactor (EBC) 1 Opens and EBC 2 Closes
5) You only have the HOT BATT BUSES 1 and 2, EMER BUS and CENTRAL BUS

21
Q

What is the battery duration in the Electrical Emergency configuration following automatic or manual electrical transfer

A

45 mins