Electrical - DC 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 voltage required for a battery start?

A

24v

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4
Q

What is the minimum recommended battery temperature for battery start?

A

Standard: -10 C
Modified: -18 C

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5
Q
A
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6
Q

On ground, BATT 1, BATT 2 in the OFF position. Which buses are powered?

A

HOT BATT BUS 1
HOT BATT BUS 2

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7
Q

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

A

-HOT BATT BUS 1
-HOT BATT BUS 2
-EMERGENCY BUS
-DC BUS 1
-DC BUS 2
-CENTRAL BUS

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8
Q

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

A

25-29v

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9
Q

What is the indication that the aircraft will accept GPU power?

A

GPU AVAIL (white) switch illuminated

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10
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 logic. The opposite side functions normally.

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11
Q

On ground, BATT 1 & BATT 2 in the ON position, GPU connected/powered, and GPU button pushed in, electrical system indicates 28V. Which buses are powered?

A

-HOT BATT BUS 1
-HOT BATT BUS 2
-EMERGENCY BUS
-DC BUS 1
-DC BUS 2
-CENTRAL BUS
-SHED BUS 1
-SHED BUS 2

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12
Q

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

A

-HOT BATT BUS 2
-CENTRAL BUS
-ENGINE STARTER

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13
Q

Which buses are powered by BATT 1 during engine start?

A

-HOT BATT BUS 1
-EMERGENCY BUS
-DC BUS 1
-DC BUS 2

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14
Q

How does DC BUS 2 receive power during engine start?

A

Quiet Start Contactor

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15
Q

Which buses are depowered during engine start?

A

-SHED BUS 1
-SHED BUS 2

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16
Q

What is the position of the following contactors during engine start?

A

-Bus Tie Contactor (BTC) 1: Open
-Bus Tie Contactor (BTC) 2: Open

17
Q

What is the position of the following contactors during normal operation?

A

-Bus Tie Contactor (BTC) 1: Open
-Bus Tie Contactor (BTC) 2: Closed

18
Q

In flight , normal operation. Which buses are powered by GEN 1?

A

-HOT BATT BUS 1
-EMERGENCY BUS
-DC BUS 1
-SHED BUS 1

19
Q

In flight, normal operation. Which buses are powered by GEN 2?

A

-HOT BATT BUS 2
-CENTRAL BUS
-DC BUS 2
-SHED BUS 2

20
Q

In flight, GEN 1 failure. What is the position of the following contactors?

A

-Generator Line Contactor 1: OPENS
-Shed Bus Contactor 1: OPENS
-Shed Bus Contactor 2: OPENS
-Bus Tie Contactor 1: CLOSES
-Bus Tie Contactor 2: REMAINS CLOSED

21
Q

In flight, GEN 1 already failed, now GEN 2 fails (Electrical Emergency). What is the position of the following contactors?

A

-Generator Line Contactor 1: REMAINS OPEN
-Generator Line Contactor 2: OPENS
-Shed Bus Contactor 1: REMAINS OPEN
-Shed Bus Contactor 2: REMAINS OPEN
-Bus Tie Contactor 1: OPENS
-Bus Tie Contactor 2:OPENS
-Emergency Bus Contactor 1:OPENS
-Emergency Bus Contactor 2:CLOSES

22
Q

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

A

45 Min

23
Q

What is the purpose of the ELEC EMER button?

A

The ELEC EMER button manually forces the contactors into the electrical emergency configuration in the event system logic fails to complete transfer.