Electric Panel - Rev 01 Flashcards
When performing the PRELIMINARY FLIGHT DECK PREPARATION, what is the minimum Battery Voltage?
(FCOM-PRO-NOR-SOP-04)
25.5 Volts
What do you do if battery voltage is below 25.5V when performing the PRELIMINARY FLIGHT DECK PREPARATION?
(FCOM-PRO-NOR-SOP-04)
Select BATT push buttons to ON with EXT PWR on aircraft. This starts the charging cycle (approximately 20min required)
When performing the FLIGHT DECK PREPARATION, what are we looking for on the ELEC panel BAT check?
(FCOM-PRO-NOR-SOP-06)
a. ECAM ELEC page – select
b. BAT 1 & 2 – OFF then ON
c. Check BATT current is < 60 amps after 10 seconds and continues to decrease
Will the batteries completely drain if you leave the BAT switches in AUTO after AC power is removed?
(FCOM-DSC-24-20)
No. Battery cut-off logic prevents complete discharge when the aircraft is on the ground and unpowered – 22VDC
How is the BATTERY BUS normally powered?
(FCOM-DSC-24-10-30-20)
DC BUS 1 through a DC tie contactor
What does the amber FAULT light in the GALLEY push button indicate?
(FCOM-DSC-24-20)
At least 1 generator load is above 100% rated output
How does the GALLEY pushbutton work in AUTO?
(FCOM-DSC-24-20)
a. Sheds main galley and in-seat power supply if:
b. Only 1 generator (APU or Engine) is available in FLIGHT, or
c. Only 1 ENGINE generator is available on the GROUND
What does a FAULT on the ENG GEN pushbutton indicate?
(FCOM-DSC-24-20)
TODO
The generator line contactor is open because of a fault detected by the Generator Control Unit (GCU) which could include:
a. The generator line contactor is open
b. Over/under voltage
c. Differential fault (short), and/or;
d. Overload
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
When is the APU GEN FAULT light inhibited?
(FCOM-DSC-24-20)
a. APU speed too low
b. Line contactor OPEN after EXT PWR or ENG GEN takes over
What is the function of the BUS TIE in the AUTO position?
(FCOM-DSC-24-20)
a. Allows the BUS TIE CONTACTORS to open and close automatically to maintain power to both AC BUS 1 & 2:
b. Allows a single source to power the entire system
c. Allows connection of the APU GEN or EXT PWR to the system
d. Inhibits multiple sources to connect simultaneously
What does an IDG FAULT light indicate?
(FCOM-DSC-24-20)
a. Oil pressure low (inhibited when N2 < 14%)
b. Oil outlet temperature overheat
c. Light is inhibited when IDG is disconnected
What precautions must you take when disconnecting an IDG?
(FCOM-DSC-24-20)
a. Do not disconnect when the engine is not operating or windmilling
b. Do not hold button longer than 3 seconds
How can an IDG be reset?
(FCOM-DSC-24-20)
On the ground by maintenance
How is AC ESS FEED transferred from AC BUS 1 to AC BUS 2?
(FCOM-DSC-24-20)
Manually by selecting ALTN on the AC ESS FEED pushbutton or automatically if AC BUS 1 is lost and the switch is in the normal position.
What does the AC ESS FEED pushbutton white ALTN light indicate?
(FCOM-DSC-24-20)
AC BUS 2 is powering the AC ESS BUS
What is the purpose of the static inverter?
(FCOM-DSC-24-10-20)
To provide AC power to the AC ESS bus from the battery when the EMER GEN is not online when in the Emergency Electrical Configuration
What is the significance of the green and red collared circuit breakers on the flight deck?
(FCOM-DSC-24-10-20)
Green – Monitored by ECAM system
Red – Wing tip brake C/B
