Electrical Flashcards

1
Q

What supplies the primary power for the 28 VDC system?

A

A DC Generator installed on each engine.

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2
Q

Both the current and voltage of the two generators are independently controlled and regulated by separate?

A

Generator Control Units (GCUs).

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3
Q

Generator voltage is regulated to _____ VDC.

A

28.5 VDC

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4
Q

Maximum Generator Output is?

A

400 Amps

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5
Q

The APU Starter/Generator supplies which bus?

A

DC Main Bus 2

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6
Q

The maximum rated amperage of the APU Starter/Generator is?

A

400 amps

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7
Q

What type of batteries are on the plane?

A

24 VDC nickel-cadium

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8
Q

Which bus are the batteries connected to?

A

Each is connected to its respective DC Main Bus by a battery relay.

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9
Q

When using 28 VDC ground power, how is it connected to the system?

A

The GPU powers DC Main Bus 1 and DC Bus 2 is powered through the Bus Tie automatically when the DC EXT button is pressed.

Thenonly time the DV bus closes automatically.

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10
Q

What can supply 28 VDC power to the DC ESS BUS in the event of a DC Generator failure?

A

Transformer Rectifier Unit (TRU) can provide 150 amps.

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11
Q

What monitors current and voltage in the electrical system?

A

Bus Power Control Unit (BPCU)

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12
Q

What powers the Emergency Power Supply (EPS)

A

A Lead Acid Battery maintained in the fully charged condition by DC Bus 1.

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13
Q

The DC EMERG PWR BUS is powered by the EPS for approximately?

A

30 minutes.

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14
Q

What does the DC EMERG PWR BUS supply?

A
  1. Standby Horizon
  2. Chronometer
  3. Lighting of the Standby Altitude/Airspeed Indicator and Standby Compass.
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15
Q

If the aircrafts power supply fails, what provides backup power to the BPCU?

A

A backup power supply lead acid battery. (approximately 30 minutes)

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16
Q

During normal operations, what powers the BPCU?

A

DC Essential Bus

17
Q

AC Power is made by?

A

Two fully independent engine driven alternators.

18
Q

The engine driven alternators power which busses?

A

AC BUS 1 and AC BUS 2

19
Q

What equipment does AC provide power to?

A
  1. Main Hydraulic Pumps
  2. Ice Detector
  3. Probe Heat
  4. Windshield Heat
  5. Horn Heat
20
Q

In the event of a single Alternator failure how is AC Bus 1 and AC Bus 2 powered?

A

AC Bus Tie

21
Q

The two static inverters supply 26VAC/400Hz power to what?

A
  1. FDR
  2. CVR
  3. TCAS
  4. EGPWS
  5. Trim Pointers
22
Q

Inverter 1 is supplied by?

Inverter 2 is supplied by?

A

Inverter 1 —DC ESS BUS

Inverter 2–DC NON ESS BUS