Electrical Flashcards

1
Q

What does an External Power “AVAIL” light indicate when illuminated?

A

External power is available and is of acceptable quality (voltage and frequency).

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2
Q

When selected manually, what electrical power source will trip off any existing power source?

A

External power.

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3
Q

What does an illuminated APU Gernerator “OFF” light indicate?

A

APU generator control breaker is open because of a fault with the APU running.

APU Generator control switch is selected OFF.

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4
Q

What does an Engine Generator “OFF” light indicate when illuminated?

A

The generator control breaker is open.

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5
Q

What does an illuminated Generator “DRIVE” light indicate?

A

The respective generator oil temperature is high
or
The respective generator oil pressure is low.

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6
Q

When can a disconnected IDG be reconnected?

A

On the ground by maintenance only.

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7
Q

What happens during an AUTOLAND if one of the Generators fails below 200 ft.?

A
  • Both bus tie breakers remain open (L/Standby/R systems are isolated for autoland).
  • The autopilot associated with a failed generator is unpowered.
  • The flight instruments remain powered through the flight instrument transfer buses.
  • The autoland continues using the remaining two autopilots.
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8
Q

What is the purpose of the Bus Tie System in AUTO?

A

Arms automatic transfer of buses in case of bus or power failures.

Arms automatic AC bus tie circuits.
Arms automatic DC bus tie circuits.
Arms automatic flight instrument transfer buses.

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9
Q

What are the priorities for automatically powering the left and right main buses?

A
  1. Respective Generator
  2. APU
  3. Opposite Generator
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10
Q

What happens to the Electrical System when the engines are started with APU electrical power in use?

A

When the associated IDG’s come online, the bus tie closes powering the main AC bus from that IDG.

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11
Q

What does an illuminated AC bus “ISLN” light indicate when the Bus Tie switch is in the “AUTO” position?

A

Fault has occured, automatically opening the AC bus tie breaker.

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12
Q

With a left AC bus fault, witll the Captain’s Flight Instruments lose power?

A

No, the FO instrument bus will automatically provide power to the Captain’s flight instruments.

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13
Q

With the Bus Tie Switches in “AUTO,” what happens to a DC bus if it’s respective T/R fails?

A

The DC tie switch closes allowing the other bus to provide power to the bus.

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14
Q

What items are normally powered by the Ground Handling Bus?

A

Lower cargo doors and equipment (aircraft fueling panel) and is energized only on the ground and only from the APU generator or external power.

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15
Q

How is the Ground Handling Bus powered?

A

APU or External power.

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16
Q

What is the normal source of power for the Aircraft Battery Charger?

A

Ground Service Bus

17
Q

What items are normally powered by the Ground Service Bus?

A

Main Battery Charger
APU Battery Charger
Miscellaneous cabin and system loads

18
Q

What is the normal source of power for the Ground Service Bus?

A

Right Main AC Bus.

19
Q

What are the alternate sources of power for the Ground Service Bus?

A

APU Generator & External Power

20
Q

What normally powers the left and right utility buses?

A

Their respective main AC bus.

21
Q

What conditions would cause Utility Bus Load shedding?

A

The loss of a generator or engine.

22
Q

What happens to the utility buses when a single engine generator is powering the electrical system and an additional power source becomes available?

A

They are load shed. If load permits the system will automatically restore power to the shed utility bus with the addition of another power source.

23
Q

What is the purpose of Automatic Load Shedding?

A

To ensure power to critical components critical to flight.

24
Q

What is the function of the “OFF” position of the STBY power selector?

A

The standby busses are unpowered.

25
Q

What is the function of the “BAT” position of the STBY power selector?

A

The standby busses are powered by the main battery.

26
Q

How is the STBY DC bus normally powered (electrical power established on all busses)?

A

Left DC bus via the left AC bus.

27
Q

How is the STBY AC bus normally powered(electrical power established on all busses)?

A

Left main AC bus via the left engine generator.

28
Q

How is the STBY AC bus powered during standby power operations?

A

The main battery and standby inverter.

29
Q

What electrical component is capable of providing temporary power to the Standby Power System should a loss of all generators occur?

A

The main battery.

30
Q

How long is the Main Battery capable of powering the Standby Power System?

A

30 minutes.

31
Q

What causes the Standby Power Bus “OFF” light to illuminate?

A

Either the DC or AC stand by bus(es) are unpowered.

32
Q

What items remain powered when operating on Standby Power?

A

Right IRU, Fuel Indicators, Electrical Standby Instrument System, Capt. Marker Beacon/Audio, Manual Speedbrakes, Alternate Stab Trim, Engine/APU Fire Detection & Protection, Left VHF (PA and Intercom), Manual Pressurization, Master Warning Lights, Standby Engine Instruments, Gear Lights, Flap Handle serves as Indicator, Fuel Control Switches, Center ILS & Control Head.