Chapter 6 - Electrical Flashcards

1
Q

What do the APU GEN and GEN CONT switches do ?

A

They ARM to close the breaker when power is available.

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2
Q

When do the APU GEN and GEN CONT OFF light illuminate ?

A

Whenever the breaker is open (because power is not available).

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3
Q

What does the BUS TIE switch do ?

A

It arms:

  • The AC bus tie
  • The DC bus tie
  • The respective flight instrument transfer bus
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4
Q

When does the bus tie ISLN light illuminate ?

A

When the AC bus tie breaker is open.

Not in case of the DC bus tie.

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5
Q

How can the load shed circuitry be reset ?

A

By recycling the UTILITY BUS switch.

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6
Q

When does the generator DRIVE light illuminate ?

A

When the oil pressure is low OR oil temperature is high.

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7
Q

Can a generator disconnect be reset in-flight ?

A

No.

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8
Q

When does the standby power OFF light illuminates ?

A

When the AC or DC standby bus or the battery bus is not powered.

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9
Q

When does the battery OFF light illuminate ?

A

When the battery switch is off.

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10
Q

Can one AC source power the whole electrical load ?

A

No. Two sources are required for the full load.

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11
Q

If APU is running and external power is connected, is the APU powering the main busses ?

A

No.

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12
Q

What is priority of AC power sources ?

A
  • Ground power
  • IDG
  • APU
  • Opposite IDG
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13
Q

Are there any indications or EICAS messages for a galley bus which is not powered.

A

No. Only when the utility bus is not powered as well.

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14
Q

Which bus powers the GND SVC bus ?

A

R MAIN AC BUS.

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15
Q

How is the GND HANDLING bus powered ?

A

From the APU GEN or from external power.

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16
Q

What happens above 200 ft in case of loss of a generator during an autoland ?

A

> 200ft, the bus ties close again. The L main AC system powers the center autopilot. NO LAND 3 is shown.

17
Q

During autoland, how is the center autopilot powered ?

A

By the standby power system.

18
Q

What happens with the AC bus ties during autoland ?

A

They open.

19
Q

How are the flight instruments powered in case of loss of both generators ?

A

By the HDG.

20
Q

Are the transfer busses powered in case of loss of both generators ?

A

Yes, by the HDG.

21
Q

What is the order of AC load shedding ?

A
  • Galley bus
  • Utility bus
  • Main AC items
22
Q

Is load shedding automatically reverted ?

A

Yes.

23
Q

Before engine start, two load sheddings may occur:

A
  • one electric hydraulic pump

- center tank fuel pumps

24
Q

During engine start, one load shedding may occur:

A

Utility busses

25
Q

What happens on the ground, when the engines are shut down, and the thrust levers are advanced ?

A

It may cause inadvertent load shedding of the utility busses. Solution: return the thrust levers to idle, and recyle the UTILITY BUS switches.

26
Q

Is the DC bus tie armed when only one BUS TIE switch is in auto ?

A

No.

27
Q

The standby power system consists of:

A

battery bus
hot battery bus
AC standby bus
DC standby bus

28
Q

How is the battery bus powered ?

A

By the L DC bus or the main battery.

29
Q

How is the DC standby bus powered ?

A

By the L DC bus or by a combination of:

- the main battery AND APU battery.

30
Q

How is the AC standby bus powered ?

A

By the L AC TRANSFER BUS or by a combination of:

- the main battery AND APU battery + inverter

31
Q

When is the HDG activated ?

A

When the L AND the R MAIN AC bus are not powered.

32
Q

Is the amount of power of the HDG more than that of full batteries ? What is the consequence ?

A

No. Consequence is that initially BAT DISCH for both batteries may occur.

33
Q

What busses are lost in case of a failure of L AC main bus ?

A

L AC transfer bus
L utility bus
L galley bus