Electrical Power Flashcards
AC system is ___V at ___Hz
115V at 400Hz
The AC system is supplied power from what sources?
2 engine driven Integrated Drive Generators (IDGs)
1 APU Generator
1 RAT Generator
1 AC external power input
DC system is __V
24V
The DC system is supplied power from what sources?
2 Nickel cadmium batteries
1 DC external power input
3 Transformer Rectifier Units (TRUs) convert AC to DC
1 Inverter converts DC to AC
What converts variable engine speed into constant generator supply?
Constant Speed Drive (CSD). One per engine
Each IDG generates constant frequency __ power at __kVA, ___V, ___Hz, _-phase
AC power at 40kVA, 115V, 400Hz, 3-phase
(T/F) The IDG oil system is liquid-cooled
False. Air cooled
If the amber light next to the IDG switch illuminates what does this mean?
The IDG OIL message is on EICAS and a manual disconnection of the IDG is required
(T/F) The APU generator needs to be manually turned on when the APU is to be used for AC power.
False. Pushing the APU GEN button disconnects the APU GEN
BATT DISCHARGING means what on EICAS?
The batteries are discharging, the generators aren’t working and the RAT should be deployed once all other options are checked
The only inverter on the aircraft is located where?
The FWD E-bay
BATT __ provides power for APU start
BATT 2
BATT 1 is located ____
BATT 2 is located ____
BATT 1 is located in the FWD E-bay
BATT 2 is located in the AFT E-bay
(T/F) During an APU start the battery contactor for battery 2 will automatically open, stopping supply to the other systems.
True
There are __ Integrated control centers (ICCs) installed on the aircraft. The L & R are located ____. The Emergency ICC is located ___. The Auxiliary ICC is located ____.
There are 4 Integrated control centers (ICCs) installed on the aircraft. The L & R are located Middle E-bay. The Emergency ICC is located FWD E-bay. The Auxiliary ICC is located AFT E-bay.