Electrical Flashcards

1
Q

How can external power be used by the ground crew when the cockpit door is locked?

A

Press the AC PUSH switchlight on the external service panel.

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2
Q

What might the DC Service switch be used for?

A

External aircraft lights while repositioning the aircraft without the battery master on.

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3
Q

In an aircraft with no power switched on, which buses are powered?

A

The APU and Main battery direct buses, and the emergency bus.

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4
Q

How many volts must be present prior to APU start?

A

22 volts minimum.

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5
Q

What is the time limit on battery power without the APU or external power and why?

A

5 minutes, to prevent over heating the CRTs without cooling fans.

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6
Q

How many AC buses are there?

A

Four.

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7
Q

How many DC buses are there?

A

Nine.

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8
Q

What normally powers AC Bus 1 & 2 and what is the switching priority in an abnormal situation?

A
  • G - Onside Generator
  • A - APU
  • G - Offside Generator
  • E - External Power
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9
Q

How many TRUs are there and what is their maximum power rating?

A

Four rated at 120 amps 28 vDC.

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10
Q

How many DC bus ties are there and what are their names?

A

Five:

  • Main Tie
  • Cross Tie
  • Utility Tie
  • Essential Tie
  • Essential TRU Tie
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11
Q

If the Cross Tie closes, what else will close?

A

The Main and Essential Ties will always close if the Cross Tie closes.

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12
Q

When is the DC Utility Bus shed?

A

When the Main Tie or Cross Tie closes.

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13
Q

What items are on the Utility Bus?

A

The Passenger Service Units.

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14
Q

How are the DC bus ties controlled?

A

DC bus tie control is automatically accomplished through the two DC Power Centers (DCPCs).

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15
Q

When will the ESS TRU 2 TIE close (causing it to display on the DC synoptic page)?

A

With the loss of AC BUS 2 and ESS TRU 1.

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16
Q

What does the DC ESS bus primarily provide power for?

A

The Captain’s flight instruments.

17
Q

When will the ADG automatically deploy?

A

During a complete AC power failure.

18
Q

What buses are powered by the ADG?

A

The ADG bus, AC Essential bus, DC Essential bus, and the DC Battery bus.

19
Q

What items are powered by the ADG?

A
  • H - Hydraulic Pump 3B
  • E - Essential Bus
  • F - Flaps and slats at half speed
  • A - ADG Bus
  • S - Stab Trim channel 2
20
Q

How much power does the ADG produce?

A

115v, 15 kVA.

21
Q

What is the minimum airspeed for ADG operation?

A

135 KIAS?

22
Q

Why must the ADG handle be pulled after an auto deployment?

A

After landing the WOW internal logic will cause the loss of power to the DC ESS bus if the handle is not pulled.

23
Q

How is normal power restored after an ADG deployment if a generator returns?

A

By stowing the ADG handle and pressing the PWR TXFR OVERRIDE button.

24
Q

Can Hydraulic Pump 3B be deselected after an ADG deployment?

A

No. It is hardwired to the ADG bus for continuous operation.

25
Q

What items are powered by the DC Emergency bus?

A
  • Engine Fire Extinguishers
  • APU Fire Extinguisher
  • Fuel SOVs
  • Hyd SOVs
26
Q

What powers the DC Emergency bus?

A

The APU battery direct bus and the DC battery bus.

27
Q

When is the DC Emergency bus displayed on the DC synoptic page?

A

When power is lost from one or both of its power sources.

28
Q

When operating only off the batteries in an emergency power situation, how many minutes of battery life does each APU start attempt cost?

A

6 minutes.

29
Q

Where is the main battery located?

A

In the forward nose compartment.

30
Q

Where is the APU battery located?

A

In the aft equipment bay.