6 - Electrical Flashcards

1
Q

On the electrical panel. What does the “battery discharge” light signify?

A

An excessive battery discharge is detected

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2
Q

On the electrical panel. What does the TR UNIT light signify

A: On the ground
B: In the air

A

A: Any TR has failed

B: TR1 or TR2&TR3 has failed

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3
Q

On the electrical panel, what does the ELEC light mean.

Will it display while airborne?

A

Fault in DC or Standby system. Shows only on the ground

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4
Q

On which bus is the Recirc fans connected

A

Connected to the bus controlled by the CAB/UTIL switch

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5
Q

The DRIVE light signifies what exactly?

A

Low oil pressure in the IDG

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6
Q

What is the nominal hz and voltage for the AC system

A

115+/-5, 400+/-10

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7
Q

Which 3 categories is the electrical system divided into

A

AC power, DC power, Standby power

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8
Q

Under what circumstance does the automatic generator on-line feature work?

A

If the APU shuts down, or fails, during/after take-off, with the APU powering both transfer buses, the engine generators are placed online.
Only once per flight.

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9
Q

During single generator operation, what is the sequence of load shedding?

A

Galley and mainbus on transfer bus 2 first, then on transfer bus 1, then the IFE.

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10
Q

What happens if the APU is the only source of power in flight?
Will the same happen on the ground?

A

All galley busss and main buses are automatically shed.

On the ground the APU will try to carry the entire electrical load.

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11
Q

What is the battery voltage range?

A

26 +/- 4

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12
Q

TR1 and TR2 are connected to their respective transfer buses, but what is the normal supply for TR3?

A

Transfer bus 2

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13
Q

During normal non-approach operations, what does TR1 and TR2 power?

A

DC bus 1, DC bus 2, DC Standby bus

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14
Q

TR3 normally powers what?

A

The battery bus

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15
Q

DC bus 1 and DC bus2 are isolated when?

A

Automatically at glide slope capture during a FD or AP ILS approach. Or when the bus transfer switch is off

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16
Q

How long can the two batteries supply standby power?

A

60 minutes

17
Q

The main and aux battery chargers are powered through what?

A

The ground service buses

18
Q

If TR3 fails, what will power the battery bus?

A

The main battery charger

19
Q

What powers the hot battery bus and switched hot battery bus.
A: during normal operations (ac power on)
B: during alternate operations (ac power N/A)

A

A: battery charger
B: battery/batteries

20
Q

Even though the APU is certified to start and operate up to the max altitude, over what altitude is start attempts not recommended when on battery power?

A

25,000 feet

21
Q

When does the STANDBY PWR OFF light illuminate

A

When one or more of these buses are unpowered:

  • AC standby bus
  • DC standby bus
  • Battery bus
22
Q

Where do the battery chargers draw power?

A

Aux: Ground service bus 1
Main: Ground service bus 2

23
Q

With normal power, and switches in normal, what happens when you turn off the battery switch

A

Battery bus, and switched hot battery bus de-energizes

24
Q

Can the ELEC light illuminate in flight?

A

No, it’s inhibited. Ground only

25
Q

AC standby bus is normally powered by

A

AC transfer bus no1

26
Q

Which DUs are powered on standby power

A

Captain inboard/outboard DU, Upper DU

27
Q

Two basic principles of the 737 electrical system

A
  1. No paralleling of AC sources

2. Turning on one AC source, de-powers the other connected one automatically

28
Q

Where is the ground service button located

A

Forward attendant panel