Electrical Flashcards

0
Q

What makes up the DC system

A
  • 2 NiCd batteries
  • 3 Transformer Rectifier Units (TRUs)
  • 1 DC external input
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1
Q

What makes up the AC system

A
  • 2 IDGs
  • 1 APU generator
  • 1 Inverter
  • 1 Ram Air Turbine (RAT)
  • 1 AC external power unit
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2
Q

What are the IDGs and APU generator rated at

A

40 kVa, 115 V, 400Hz, 3 phase

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3
Q

What does the static inverter do

A

It converts 28v DC to 115v AC to power the STANDBY AC BUS when an AC power source is not available

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4
Q

What type of power is produced by the RAT

A

15kVa, 115v AC, 400Hz, 3 phase

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5
Q

When is the RAT automatically deployed

A

Whenever AC power sources are not powering AC buses

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6
Q

How long after deployment will the RAT begin to supply power

A

8 sec

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7
Q

Which bus does the RAT power when in use

A

AC ESS BUS

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8
Q

During the timespan prior to RAT supplying power, what happens in order to maintain power

A

The batteries power the DC ESS BUS and the STANDBY AC BUS

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9
Q

Which hydraulic pump does the RAT power

A

ACMP 3A

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10
Q

Below what speed will the RAT be unable to continue to supply sufficient power

A

130kts

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11
Q

What happens if airspeed drops below that required to utilize the RAT

A

The batteries power the DC ESS BUSSES and the STANDBY AC BUS through the static inverter

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12
Q

What is a DC GPU used solely for

A

Powering the APU START BUS on the ground

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13
Q

What are the TRUs rated to

A

300A

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14
Q

What does TRU1 power

A

DC BUS1, DC ESS BUS1, DC GND SVC BUS, HOT BATT BUS 1, battery #1 charging

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15
Q

What does TRU2 power

A

DC BUS 2, DC ESS BUS 2, HOT BATT BUS 2 and battery #2 charging

16
Q

What does the ESS TRU power

A

DC ESS BUS 3

17
Q

What kind of power do the batteries supply

A

22.8VDC, 27A

18
Q

When is the BATT 1 (2) OVERTEMP warning triggered

A

When the battery temp reaches 70C for 2 secs

19
Q

When do you use a DC GPU

A

When the battery is no longer available or the Battery #2 is below -20C

20
Q

What do the Integrated Control Centers (ICCs) do

A

Provide power distribution and protection for the airplane electrical loads, the secondary power distribution assemblies (SPDAs) and the circuit breakers

21
Q

How many ICCs does the plane have

A

4
• Left Integrated Control Center (LICC).

  • Right Integrated Control Center (RICC).
  • Emergency Integrated Control Center (EICC).
  • Auxiliary Integrated Control Center (AICC).
22
Q

How are the circuit breakers classified

A

Thermal or electronic

23
Q

Where are the electronic CBs located

A

inside the SPDAs, in the electronics bays.

24
Q

Where are the thermal CBs located

A

In the cockpit and in the ICCsin the electronics bays

25
Q

What is the source priority order for powering the airplane

A
  • Respective IDG.
  • APU generator.
  • GPU (on ground without APU).
  • Opposite IDG.

If required the DC GPU can be used for the APU start

26
Q

What controls load shedding and when does it occur

A

The SPDAs shed load whenever electrical load increases beyond the system limit

27
Q

Which items are load shed

A

Galleys and right windshield heating

28
Q

What is the chain of electrical power

A

AC sources (IDGs, APU, external AC) -> electrical busses in the ICCs -> SPDAs -> individual components

29
Q

Which battery powers the APU starter

A

Batt 2

30
Q

What does the static inverter do

A

Converts 28v DC from the batteries to 115v AC to power the STANDBY AC BUS when an AC power source is not avail.