Electrical Flashcards
Q1 | EMERGENCY ELECTRICAL PANEL
What buses are powered by the emergency generator?
- AC ESS and AC ESS SHED
- DC ESS and DC ESS SHED
[ FCOM-DSC-24-10-30-30 ]
Q2 | EMERGENCY ELECTRICAL PANEL
What is the function of the RAT & EMER GEN pushbutton?
- AUTO – RAT will automatically extend if AC BUS 1 & 2 are not powered and airspeed > 100 knots
- MAN – extend the RAT at any time
[ FCOM-DSC-24-20 ]
Q3 | EMERGENCY ELECTRICAL PANEL
How long does it take the RAT to extend and provide power?
- 8 seconds
- (3 seconds for RAT extension, 5 seconds to pressurize the Blue hydraulic system and power the EMER GEN)
[ FCOM-DSC-24-10-30-30 ]
Q4 | EMERGENCY ELECTRICAL PANEL
What does the red FAULT light on the RAT & EMER GEN pushbutton indicate?
Loss of power to AC Bus 1 + AC Bus 2 and the emergency generator is not supplying power
[ FCOM-DSC-24-20 ]
Q5 | EMERGENCY ELECTRICAL PANEL
What powers the emergency generator?
Blue hydraulic power from the RAT
[ FCOM-DSC-24-10-20 ]
Q6 | EMERGENCY ELECTRICAL PANEL
Is there another way to deploy the RAT?
Yes, RAT MAN ON from the HYD panel
[ FCOM-DSC-24-10-30-30, FCOM-DSC-29-20 ]
Q7 | EMERGENCY ELECTRICAL PANEL
What is different about deploying the RAT via the HYD Panel?
Blue HYD pressure only – No Emergency Generator
[ FCOM-DSC-24-10-30-40 ]
Q8 | EMERGENCY ELECTRICAL PANEL
What happens when you push the GEN 1 LINE pushbutton?
- GEN 1 Line Contactor opens and the white OFF light illuminates
- AC BUS 1 is powered by GEN 2 through the BUS TIE CONTACTOR
- GEN 1 continues to power 1 fuel pump in each wing tank
- During smoke procedures
[ FCOM-DSC-24-20 ]
Q9 | EMERGENCY ELECTRICAL PANEL
When is the GEN1 Line pushbutton used?
During smoke procedures
[ FCOM-DSC-24-20 ]
Q10 | ELECTRIC PANEL
When performing the PRELIMINARY COCKPIT PREPARATION, what is the minimum Battery Voltage?
25.5 Volts
[ FCOM-PRO-NOR-SOP-04 ]
Q11 | ELECTRIC PANEL
What do you do if it is below 25.5V?
- Select BATT pushbuttons to ON with EXT PWR on aircraft
- This starts the charging cycle (approximately
20min required)
[ FCOM-PRO-NOR-SOP-04 ]
Q12 | ELECTRIC PANEL
When performing the COCKPIT PREPARATION, what are we looking for on the ELEC panel BAT check?
- ECAM ELEC page – select
- BAT 1 & 2 – OFF then ON
- Check BATT current is < 60 amps after 10 seconds and continues to decrease
[ FCOM-PRO-NOR-SOP-06 ]
Q13 | ELECTRIC PANEL
Will the batteries completely drain if you leave the BAT switches in AUTO after AC power is removed on the ground?
No
Battery cut-off logic prevents complete discharge when the aircraft is on the ground and unpowered – 22VDC
[ FCOM-DSC-24-20 ]
Q14 | ELECTRIC PANEL
How is the BATTERY BUS normally powered?
DC BUS 1 through a DC bus tie contactor
[ FCOM-DSC-24-10-30-20 ]
Q15 | ELECTRIC PANEL
What does the amber FAULT light in the GALLEY pushbutton indicate?
At least 1 generator load is above 100% rated output
[ FCOM-DSC-24-20 ]
Q16 | ELECTRIC PANEL
How does the GALLEY pushbutton work in AUTO?
[ FCOM-DSC-24-20 ]
Sheds main galley and in-seat power supply if:
* Only 1 generator (APU or Engine) is available in FLIGHT, or
* Only 1 ENGINE generator is available on the GROUND (All galleys are available when APU GEN or EXT PWR is supplying power)
[ FCOM-DSC-24-20 ]
Q17 | ELECTRIC PANEL
What does a FAULT on the ENG GEN pushbutton indicate?
[ FCOM-DSC-24-20 ]
The generator line contactor is open because of a fault detected by the Generator Control Unit (GCU) which could include:
* Overload
* Over/under voltage
* Differential fault (short), and/or;
* The generator line contactor is open
[ FCOM-DSC-24-20 ]
Q18 | ELECTRIC PANEL
What does the APU GEN FAULT light indicate?
[ FCOM-DSC-24-20 ]
The generator line contactor is open because of a fault detected by the GCU
[ FCOM-DSC-24-20 ]
Q19 | ELECTRIC PANEL
When is the APU GEN FAULT light inhibited?
[ FCOM-DSC-24-20 ]
- APU speed too low
- Line contactor OPEN after EXT PWR or ENG GEN takes over
[ FCOM-DSC-24-20 ]
Q20 | ELECTRIC PANEL
What is the function of the BUS TIE in the AUTO position?
- Allows the BUS TIE CONTACTORS to open and close automatically to maintain power to both AC BUS 1 & 2:
- Allows a single source to power the entire system
- Allows connection of the APU GEN or EXT PWR to the system
- Inhibits multiple sources to connect simultaneously
[ FCOM-DSC-24-20 ]
Q21 | ELECTRIC PANEL
What does an IDG FAULT light indicate?
[ FCOM-DSC-24-20 ]
- Oil pressure low (inhibited when N2 < 14%)
- Oil outlet temperature overheat
- Light is inhibited when IDG is disconnected
[ FCOM-DSC-24-20 ]
Q22 | ELECTRIC PANEL
What precautions must you take when disconnecting an IDG?
- Do not disconnect when the engine is not operating or windmilling
- Do not hold button longer than 3 seconds
[ FCOM-DSC-24-20 ]
Q23 | ELECTRIC PANEL
How can an IDG be reset?
On the ground by maintenance
[ FCOM-DSC-24-20 ]
Q24 | ELECTRIC PANEL
What is the function of the AC ESS FEED pushbutton in the normal position?
Allows AC BUS 1 to power the AC ESS BUS
[ FCOM-DSC-24-20 ]
Q25 | ELECTRIC PANEL
How is AC ESS FEED transferred from AC BUS 1 to AC BUS 2?
- Manually by selecting ALTN on the AC ESS FEED pushbutton
- Automatically if AC BUS 1 is lost and the switch is in the normal position
[ FCOM-DSC-24-20 ]
Q26 | ELECTRIC PANEL
What does the AC ESS FEED pushbutton white ALTN light indicate?
AC BUS 2 is powering the AC ESS BUS
[ FCOM-DSC-24-20 ]
Q27 | ELECTRIC PANEL
What is the purpose of the static inverter?
To provide AC power to the AC ESS bus from the battery when the EMG GEN is not online in the Emergency Electrical Configuration
[ FCOM-DSC-24-10-20 ]
Q28 | ELECTRIC PANEL
What are the 3 times the batteries are connected to the BATTERY BUS?
- APU start
- Battery charging
- AC BUS 1 & 2 not powered and airspeed below 100 knots
[ FCOM-DSC-24-10-30-20, FCOM-DSC-24-10-30-30, FCOM-DSC-49-10-40 ]
Q29 | ELECTRIC PANEL
What is the priority sequence for electrical power (OOIO! Sewers & Caves)?
O - Onside - Engine Generator
O - Outside - EXT PWR (manually selected)
I - Inside - APU Generator
O - Offside - Engine Generator
Sewers (Rats) - RAT Emergency Generator
Caves (Bats) - Batteries
[ FCOM-DSC-24-20-10-30-10, FCOM DSC-24-10-30-30 ]
Q30 | ELECTRIC PANEL
With the APU green AVAIL light ON and the EXT PWR blue ON light illuminated, which system is powering the aircraft?
EXT PWR
[ FCOM-DSC-24-20 ]
Q31 | ELECTRIC PANEL
What is the significance of the green and red collared circuit breakers on the flight deck?
- Green – Monitored by ECAM
- Red – Wing tip brake C/B
- Black – Not monitored by ECAM
[ FCOM-DSC 24-10-20 ]