Electrical System Flashcards

1
Q

What is the function of the Standby Battery?

A

Powers the Hot Busbar and provides power to initialise the EPCU. The Hot busbar powers the Extinguisher squibs, boarding lights and dome lights.

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2
Q

What is the function of the Avionics Battery Bus?

A

Powers the emergency standby radio, Integrated Standby Instrument (ISI), Storm lights and Standby Compass Light

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3
Q

Where do the engine driven DC Generators supply power directly to:

A

L and R Main Feeder Bus respectively

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4
Q

When are the Main Busbars normally tied?

A

Automatically by the ECPU when GPU/APU power connected and for engine starting

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5
Q

If both AC generators fail in flight, how can the Secondary Busbars be powered?

A

Vertically tied to each respective Main Feeder Bus

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6
Q

With the engines shut down on the ground, how can the AC services be powered?

A

AC external power connected via a on the inboard RH

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7
Q

What systems can be powered by an AC GPU?

A

All services

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8
Q

What does the moving the Batt Master Switch to ON achieve?

A

Connects the Main Battery, Aux and Standby to the Essential Busbars.

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9
Q

Where is the DC GPU Connection Socket located?

A

Left side of the nose

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10
Q

What does a reading of +1.2 mean on a Battery Load Indication?

A

Battery has exceeded max load of +1.0 (overload)

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11
Q

When would a Battery Temperature Readout be Amber?

A

50-65C

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12
Q

If the aircraft is being powered from a DC GPU, how is this indicated?

A

Top left of the ELEC SYS page - reads DC EXT PWR ON

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13
Q

Where on the flight deck are the Avionics CBs located?

A

Top left behind the captain’s seat

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14
Q

What is the effect of switching on the Standby Battery Switch?

A

Connects the Standby battery to the left Main feeder bus but does not power it

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15
Q

How is the Electrical System protected from GPU/APU over-voltage?

A

Generator control units on both disconnect GPU/APU

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16
Q

What is the correct sequence for applying DC GPU Power to a “cold” aircraft?

A

Master Battery On, Aux switches on, GPU power connected, EXT PWR ON

17
Q

What will prevent the APU Generator from coming on line?

A

Selecting EXT PWR switch to ON before switching on the APU Gen.

18
Q

In a fully powered electrical system, what is the Bus Tie Configuration?

A

Disconnected

19
Q

What would happen to the DC Generators were to fail in flight?

A

TRUs will power whole system through L+R Bus Tie Contacters

20
Q

What is the minimum Busbar Voltage for a engine start using GPU or APU?

A

26 v DC minimum

21
Q

What is the minimum Battery Temperature for take off?

22
Q

How can a BATT HOT Warning be confirmed?

A

Select ELEC SYS page

23
Q

What does a BATTERY Caution indicate?

A

The associated battery is not connected to the Main Bus for charging.

24
Q

What power supplies are available if the EPCU reverts to emergency Mode?

A

Essential Busbars, Main and Auxiliary batteries if required for engine start.

25
If Battery Essential Services Only is selected, what Flight Instruments are available?
ADC 1, AHRS 1 and 2, COMM 1, NAV 1, ISI, ED.
26
What is the Battery Duration if operating on Battery Essential Services in flight?
45 minutes
27
Which systems are powered by the Avionics Battery Bus?
Standby Emergency Radio, ISI (Integrated Standby Instrument), Storm Lights, Standby Compass Light