Electrical Questions Flashcards

1
Q

How many networks make up the electrical system on the airplane? why?

A

2 independent networks

Redundancy and fault isolation

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2
Q

What happens if a power generating source fails?

A

Bus ties automatically connect to provide no system degradation

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3
Q

What components powers the AC system?

A

1) 2 IDGs
2) APU
3) Inverter
4) Ram Air Turbine (RAT)
5) AC GPU receptacle

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4
Q

What components power the DC system?

A

1) 2 NiCad Batteries
2) 3 TRU’s
3) DC GPU receptacle

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5
Q

How does the IDG maintain a stable power output?

A

a Constant Speed Drive (CSD) attaches the IDG to the AGB (Accessory Gear Box)

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6
Q

What monitors and controls the IDGs?

A

Each has a Generator Control UNit (GCU)

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7
Q

Can one IDG supply the entire electrical system?

A

Yes

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8
Q

What will cause the amber IDG on the overhead panel to illuminate?

A

High Oil Temp

Low Oil Pressure

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9
Q

If an IDG is manually disconnected, can the flight crew reconnect it?

A

No. MX function on the ground

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10
Q

What is the primary purpose of the AC Generators?

A

To power the AC busses and the AC ESS BUS which…

Power the 3 TRU’s, 1,2, and ESS

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11
Q

what is the purpose of the TRU’s?

A

To convert 115VAC to 28 VDC

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12
Q

Can the APU replace a failed IDG?

A

Yes up to 33,000ft

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13
Q

What is the AC electrical systems priority?

A
Onside (IDG)
Inside (APU)
Outside (GPU)
Cross side (other IDG)
***the airplane uses an onboard AC power source beofre an external AC source
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14
Q

How is it known that an AC GPU is hooked up to the airplane and ready to provide electricity?

A
  • GPU button displays AVAIL and the GPU icon is presented on the electrical Syn Page
  • Once the GPU button is pushed in, the button will display IN USE provided another AC power source is not available
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15
Q

What does it mean if the AC GPU is plugged in and the outside GPU panel button displays IN USE?

A
  • Ground service Bus is In Use

- Cockpit GPU button will display AVAIL even though the ground service bus is in use

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16
Q

If the airplane is using the AC GPU and the APU is started, what should the pilot be sure to do?

A

Deselect the GPU button

17
Q

What will charge the batteries?

A

Any AC Power source

18
Q

How long will the aircrafts batteries last with no recharging?

A

10 minutes

19
Q

What is the purpose of the DC GPU receptacle?

A

For APU start when batteries

20
Q

What is the Min battery temp for APU start?

21
Q

What is the Minimum battery voltage to close the battery bus ties?

22
Q

What battery is used for the APU start?

A
  • BATT 2 powers the APU Start Bus

- BATT 1 powers the FADEC & EICAS for monitoring

23
Q

What is the purpose for the inverter?

A

Converts 28 VDC from the batteries to 115 VAC to power the AC STANDBY BUS whan an AC souce is not available

24
Q

What is on the AC STANDBY BUS?

A

Engine Igniters 1A and 2A

25
What powers the Ram Air Turbine (RAT)?
Airflow turns the RAT prop which spins the turbine inside
26
When will the RAT deploy?
- Automatically deploys if AC BUSSES are not powered | - Manually by the pilot
27
How long after deployment before the RAT will supply power?
8 Seconds
28
Is there is a total loss of power during the 8 second RAT deployment?
No. Batteries supply power to the DC ESS BUSSES and AC STANDBY BUS
29
What does the RAT power?
ESS BUSSES
30
What is the Min airspeed for the RAT?
- 130 kts | - Load shedding occurs below this speed
31
When is the RAT icon displayed on the Electrical Syn Page?
When the RAT is deployed
32
What manages the electrical system?
- 4 Integrated Control Centers (ICC) | - 2 Secondary Power Distribution Assemblies (SPDA)
33
What is an ICC?
An Electrical Control device, which provides power distribution and protection for electrical loads
34
What is a SPDA?
An electrical load management unit (powered by the ICC's) that distributes electrical loads to aircraft systems according to distribution logic
35
Can the flight crew reset the ICC and SPDA remote electronic CB's?
- ICC CB's can only be reset by MX on the ground | - SPDA CB's can be reset via the MCDU