Copyright D.P. Browne 2011

 

 

 

 

Home.Cockpit.Aircraft Systems.Worked Example.Program Controls.Before Flight.

Electrical Panel

 

 

Battery buttons

 

Normal operation. Battery connected to the DC ESS bus and DC BAT bus

 

 

In/On

 

Battery disconnected from the DC buses (isolated)

 

 

Out/Off

 

Over/Under voltage

 

 

FAULT

 

Battery disconnected from the DC buses (isolated)

 

 

OFF

 

Generator buttons

 

Normal operation. Generator connected to its AC bus

 

 

In/On

 

Generator disconnected from the AC buses

 

 

Out/Off

 

Failure indication is present, refer to AC / DC System Display and ECAM message

 

 

FAULT

 

Generator disconnected from the AC buses

 

 

OFF

 

IDG buttons ( guarded)

 

Normal operation. IDG connected

 

 

In/On

 

Generator disconnected from the AC buses

 

 

Out/Off

 

Failure indication is present, refer to AC / DC System Display and ECAM message

 

 

FAULT

 

IDG disconnected and cannot be re-connected in flight

 

 

OFF

 

External Power buttons

 

Allows external power to supply the AC busses.

 

 

In/On

 

External power not connected to aircraft electrical system

 

 

Out/Off

 

External power supply available. Can be illuminated if no aircraft electrical AC/DC exists

 

 

AVAIL

 

External power supply some or all the aircraft electrical buses.

 

 

ON

 

Bus Tie button

 

Auto bus tie operates. Will automatically cause AC bus to be powered from the other side in case of generator loss

 

 

In/On

 

Automatic bus tie off.

 

 

Out/Off

 

Automatic bus tie off.

 

 

OFF

 

AC essential Feed

 

Alternate feed (from AC 2 side) is selected

 

 

In/On

 

Normal position, allows AC ESS bus to be feed from AC 1

 

 

Out/Off

 

Failure indication is present, refer to AC / DC System Display and ECAM message

 

 

FAULT

 

AC ESS bus to feed from AC 2

 

 

ALTN

 

Galley and Commercial buttons

 

Normal operation. Galley and cabin entertainment systems active

 

 

In/On

 

Disconnected from the aircraft electrical supply.

 

 

Out/Off

 

Galley Failure indication is present, refer to AC / DC System Display and ECAM message

 

 

FAULT

 

Disconnected from the aircraft electrical supply. This may occur in the case of automatic electrical load shedding

 

 

OFF

 

Apu Starter Panel

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