Electric 747-400 Flashcards

1
Q

Is it possible to switch off the HOT BAT BUSSES?

A

No. They are fixed to the batteries.

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2
Q

Is DC BUS 2 still powered with an open DCIR 2?

A

Yes. DC BUS 2 will be powered by the T/R unit 2. No connection to the tie bus.

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3
Q

What does the SSB light mean?

A

Different power sources feed the two halves of the synchronus bus.

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4
Q

Do the STBY BUSSES loose power when you switch the STANDBY POWER selector OFF?

A

Yes. It disconnects STBY BUSSES from all sources.

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5
Q

After the successful start of Engine 4, what powers the synchronous bus?

A

IDG 4 feeds the synchronous bus.

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6
Q

After engine start, do the IDGs supply all busses?

A

No.

The IDGs don’t power the GND HANDLING BUS, and Main deck cargo Handling bus.

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7
Q

What does an OFF light in the GEN CONT 3 switch mean?

A

The Generator control Breaker (GCB) 3 is open.

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8
Q

If the GEN CONT 3 OFF light is illuminated, which bus powers the CAPT X-FER BUS?

A

AC BUS 3.

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9
Q

If APU GEN 1 and APU GEN 2 are available, will they connect automatically to the synchronous bus, when the engines are cut?

A

No. Manual connection is required.

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10
Q

If the APU is on, and the Battery switch is turned off. What will happen if anything?

A

The APU will shut down without time delay.

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11
Q

After an automatic trip of a BYB (BUS TIE BREAKER) will the respective DCIR open too?

A

No. The DCIR remains closed.

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12
Q

What happens if you select the BATTERY switch to OFF in flight?

A

All busses remain powered.

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13
Q

Which AC busses have to fail, to start the APU STBY INVERTER?

A

AC BUS 1, and AC BUS 3 cause the APU STBY INV to start.

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14
Q

What does an OFF light on a utility bus that is ON mean?

A

That an ELCU disconnected at least one utility bus.

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15
Q

Both APU GENS supply the aircraft. What happens, if APU GEN 2 fails?

A

The SSB closes and all busses remain powered.

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16
Q

On what page are the APU parameters displayed?

A

STAT. (STATUS page)

17
Q

In order to operate the APU, does it require to switch on a fuel pump?

A

No. APU fuel is supplied by system logic.
Main 2 aft
Main 3 aft
APU DC pump

  • One of the aircrafts doesn’t use both 2, and 3 pumps.
18
Q

Which condition is described by the APU DOOR message?

A

1) APU door not full open at start or fully closed during shutdown.