AC system Flashcards

1
Q

What does the 115V variable frequency AC system supply power to?

A

TRUs
Electrical pumps (SPU and aux fuel)
Anti icing heaters for windshields, elevator horn, AoA vanes, Prop De-ice

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2
Q

How are the AC generators powered/mounted? When do the generators come online?

A

On the propeller Reduction gear box

Come online after engine start when props brought out of the feather position

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3
Q

Where is the AC GCU located?

A

AC contactor Box in the engine nacelle.

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4
Q

Why might the #1 AC GEN caution light illuminate in flight?

A
#1 generator output exceeded 125v causing it to shut down, 
#1 generator may have failed,
#1 generator may have been switched off by pilot
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5
Q

is there a checklist for loss of both AC generators?

A

No, it’s unlikely this would happen. The QRH lists services that would be lost in the L and R AC buses.

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6
Q

When external AC power is connected, what buses are powered?

A

Both variable frequency AC buses, then power sent to all 28v DC buses through TRUs

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7
Q

Can external AC power be used to start the engines?

A

No, it can be used to set the aircraft up for an engine start, but not too start the engine.

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8
Q

Why must extreme caution be exercised before connecting external AC power to the aircraft?

A

Once applied, if either SPU switch on, the hydraulic system will be activated and gear doors will Snap closed.

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9
Q

What is the maximum AC loadmeter reading allowed on the ground if the temp is above 10 degrees Celsius?

A

0.33

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10
Q

What do the inverters do? What power and buses do they supply?

A

They invert 28v DC power to 115 400 hertz AC power to 2 buses. The fixed frequency 115v AC bus send power through a transformer to power the 26v AC buses.

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11
Q

What is a possible cause of all 3 inverter caution lights as well as both 26v AC caution lights being Illuminated?

A

A faulty paralleling control box or possibly one faulty inverter had caused the paralleling control box to take all inverters off line.

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12
Q

What are some things powered by the 26v AC buses?

A
ADF 1 and 2
ADI 1 and 2 
HSI 1 and 2 
ALT 1 and 2 
HYD quantity ind and transfer 
RMI (powered by opposite bus) 
PFCS ind
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