Explore the A320's electrical system through targeted questions assessing knowledge on battery checks, power source priorities, and system operations. This quiz is ideal for aerospace professionals and students, enhancing understanding of aircraft electrical functions.
All systems return to normal and the RAT must be restored .
The APU would now power both sides of the electrical system.
Eng gen 1continues to power AC bus 1 and downstream systems . The APU powers AC bus 2 and downstream systems.
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Green collared circuitbreakers are monitored by the ECAM
GREEN COLLARED CIRCUIT BREAKERS ARE PULLED WHEN flying on battery poer only
Green collared circuit breakers are not be reset.
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APU , External power , Gen 1 or Gen 2 .
APU ,Gen 2 or 1, External power
Gen 1 or Gen 2, External power (if selected ) , APU .
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NO
Only when operating in the Emergency Electrical Configuration.
Yes , press the ECAM ELEC , push button and view the electrical schematic on the ECAM .
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Between 22 and 30 minutes depending on equipment in use .
Until the APU IS STARTED
TWO HOURS AND 30 MINUTES DEPENDENT ON THE EQUIPMENT IN USE
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Yes , but only after contacting maintenance control .
Yes , push and hold the IDG pb until the GEN fault light is no longer illuminated .
NO
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Depress and hold the specific ECAM page push button on the ECAM control panel.
Transfer occurs automatically.
This is not posible .Use the cockpit operating manual.
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Never disconnect an IDG in flight or push the IDG disconnect push button for more then 30 seconds.
Never disconnect an IDG in flight or push the IDG disconnect push button for more then 5 seconds.
Never disconnect an IDG unless the engine is running , nor push the IDG isconnect push button for more then 3 seconds.
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When selected OFF the avionics compartment isolation valves close .
When selected OFF the 1 Generator powers all AC busses
When selected OFF generator 1 is removed from all busses but continues to power one fuel pump in each wing.
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Yes.
Only with the RAT deployed.
The electrical system will not allow paralleling of generators.
Alternate
Manual
Backup.
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Once
Once , if authorized by the procedure
Twice
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Emergency path lights only.
Right side Dome light , main panel flood lights ( left two columns only )and the stanby compass light .
Right side dome light , main panel flood lights and the stanby compass.
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Less than 60 amps in 10 seconds.
Greater than 34 volts.
Greater than 25 volts.
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Electrical power to both AC BUS 1 and 2 is lost and the aircraft speed 100 knots
With the loss of two Hydraulic systems.
A or B
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Backup
Direct
Alternate
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Battery charging current increases at an abnormal rate .
Battery voltage drops below a predeterminate level.
The batteries have auto disconnected due to low voltage.
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The power transfer would switch to the opposite bus.
All power would be lost and the aircraft would be powered by the batteries until the RAT was up to speed.
None
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If the APU is not operating it should be started at this time .
The APU will not start until the aircraft has come to a complete stop and all power has been removed for 15 seconds .
On the ground bellow 100 knots , the DC BATTERY BUS automatically reconnects to the batteries allowing APU start.
When the EMER GEN is not supplying electrical power ,AC busses 1 and 2 are unpowered and the nose gear is up
When the RAT is displayed using hydraulic RAT MAN ON push button .
Both A and B are correct
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Push this button to automatically start the APU
When selected to OFF the APU generator field is de_energized.
Both A and B are correct.
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They are not monitored by ECAM.
Can not be reset.
They may be operational in the Emergency Electrical Configuration .
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SEC 1
FÁC 1
ELAC 1
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No , but some loads are shed in both main galleys .
Only the AC ESS shed bus .
None of the above .
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External power is supplying all electrical needs.
Eng Gen 1 is supplying Ac bus 1 and the downstream system and AC bus 2 through the bus tie contractors.
Gen 1 supplies AC bus 1 and (generally )the downstream system , Ext Pwr supplies AC bus 2.
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The flight attendants have all the coffee makers and ovens on at once .
The Main Galley has shed.
The load on any generator is above 100% of it´s rated output.
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VHF 1 ,RMP 1 VOR 1
ACP 1 ,& ACP 2 ,VHF 1 ,HF1 , RMP 1 ,VOR 1 and ILS 1.
RMP 1&2 ,VHF 1 , HF , ACP 1 ,VOR ,ILS 1
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Exit sign , emergency lights and scape path lighting .
Exit signs, emergemcy lights , main panel flood lights and escape path lights .
Exit signs , emergency lights , dome lights , main panel flood lights and the standby compass light .
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BATT HOT busses Will be power ESS DC , ESS DC SHED ,ESS AC ,and ESS AC SHED
The BATTERIES busses would power Booth HOT BATT busses , ESS DC and ESS AC through the STATIC INVERTER
The STATIC INVERTER would power Both HOT BATT busses ESS DC and ESS AC through the ESS AC SHED busses.
AC bus 1 unpowered.
AC shed bus unpowered .
DECESS SHED bus unpowered .
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DME , and Transponder 1.
DME 1, DDRMI and Transponder.
DME 1 and Transponder 1.
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ELAC 1 , SEC 1 and FAC 1
ELAC 1 and 2 SEC 1 and 2 , FAC 1
ELAC 1 , and SEC 1.
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Check to see that FMGC has auto tuned the appropiate NAV facility for the approach to be accomplish.
Depress the guarded RMP NAV puso button and tune the aprópiate NAV facility and Course for the aproach to be acomplish.
A & B
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Yes , transfer is automatic .
Yes, only if AUTO was selected on the AC ESS FEED push button.
No this must be done by the crew .
DC ESS SHED bus not powered.
AC ESS SHED bus not powered.
Loss of power to the AC bus 1.
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