E175 Electric System Flashcards

1
Q

How many networks make up the electrical system on the Airplane?

A
  • 2 independent networks

- redundancy and fault isolation

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2
Q

What happens if a power-generating surface fails?

A
  • bus ties automatically connect to provide no system degradation
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3
Q

What components power the AC system?

A
  • 2 integrated drive generators IDG
  • APU
  • inverter
  • the RAT
  • AC GPU receptacle
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4
Q

What components power the DC system?

A
  • 2 NiCad batteries
  • 3 transformer rectifiers units TRU
  • 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 IDG’s

A

Each has a GCU generator control unit

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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 light on the O/H 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- it’s a maintenance thing

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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 transformer rectifier units TRU 1, 2 and ESS

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11
Q

What is the purpose of the transform rectifier units TRU?

A

To convert 115vac to 28DC

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12
Q

Can the APU replace a failed IDG?

A

Yes- up to 33,000 feet

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13
Q

What is the AC electrical systems priority?

A
  • Onside IDG
  • Inside APU
  • Outside GPU
  • Cross-Side (other IDG)

Note: the plane uses an onboard AC power source before 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 synoptic 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 planes 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 VDC or,

- if battery temp is < -20c

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 of the inverter?

A

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

24
Q

What is on the AC STANDBY BUS?

A

Engine exciters 1A and 2A

25
What powers the RAT?
Airflow turns the RAT propeller which spins the turbine inside
26
When will the RAT deploy?
- auto if AC BUSSES are not powered | - manually by pilot
27
How long once deployed does it take for the RAT to supply power?
8 seconds
28
Is there 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 minimum airspeed for the RAT?
- 130k | - load shedding occurs below this speed
31
When is the RAT icon displayed on the electrical synoptic 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 plane 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 maintenance on the ground | - SPDA CB’s can be reset via the MCDU