POWER DISTRIBUTION Flashcards
Two buses for servicing AC
Ground handling and ground servicing bus
No switches for ground handling bus
External power has priority over APU for powering the ground handling bus
Ground handling bus powers
Cargo doors
Cargo compartment lights
Maintenance access dooors
Ground service bus
For cabin service personnel
Cabin lights and outlets
Battery chargers for main and APU battery chargers
Left forward fuel pump (APU fuel)
Ground service switch at attendants panel
Can be used to power the ground service bus when buses are not powered by any other source of power
Right main AC bus powered
Ground service bus powered
If right AC bus not powered and APU running
Ground service bus is powered by APU gen through the same ground service switch
In cabin with IFE/PASS SEATS and CABIN/UTILITY switches on
The ground service bus, utility bus and galleys are powered normally
Cabin utility switch off
Removes power form cabin lighting and outlets portion of ground service bus
The main and APU battery chargers and left fwd fuel pump remain powered
Powered removed fro cabin lighting
The following turned on Night lights Supp night lights Reading lights Attendant work lights
DC POWER SYSTEM
PDFs
ND
GPS
ADIRU
Fully automatic/no controls
Sources of DC POWER
2 batteries
APU
Main battery
Monitored by ELMS
Main soursce of DC POWER
By 4 TRU Transformer rectifier units AC to DC power Powered by two transfer buses They power 4 DC buses
TRU L
LMAIN DC BUS
TRU C1
CAPT FLT INST BUS
TRU C2
FO FLT INST BUS
TRU R
R MAIN DC BUS
If TRU Fails
Tie relays connect the left and right DC buses
And CAPT and FO FLT instrument buses this allows all buses to remain powered
Flight controls DC system
Fly by wire
PMGs
Permanent magnet generators
Housed within each backup gen
Power source for the flight controls