Electrical Flashcards
What HYD systems are Electric in 787
Stabilizer Trim
Spoilers
Main Wheel Brakes
What is the Location of the 3 electric power supply
FWD E/E Bay - 115 Vac and 28VDC
AFT E/E Bay - 235 Vac
What power supply is Ext
115 Vac usually both FWD
What power supplies are used for a normal start
Both FWD Vac and APU
or
Both FWD Vac and AFT Vac if APU is inop
(Supplementary procedure)
Only the Right eng can be started if Ext Pwr is the only source
What Converters are on board
235 Vac –> 28 VDC
115 Vac –> 235 Vac to operate Hyd pumps Eng starters NGS
What AC buses do we have
L1 Main
L2 Main
R1 Main
R2 Main
When APU or Eng gen online they supply 235 Vac which converts to 115 Vac and 28 VDC pwr
What generators does the APU have
2 - 235 Vac starter/generators
How can APU start be powered
APU bat
Ext Pwr
Eng Gen
(one started is used for APU start but both generators available after for pwr delivery)
Describe the Eng Starter/Generators
2 - 235 Vac on each eng L1, L2
unlike the APU both starters assist in eng starting
Where does the 235 Vac power from the eng go
to the AFT E/E bay
In normal operation which gen supplies which bus
L1 - L1
L2 - L2
R1 - R1
R2 - R2
After the Buses where does the 235 Vac power go
Large Motor Power system
In AFT E/E Bay, and cooled by the PECS
What are RPDU’s
Remote Power Distribution
used for lower amp loads through 17 units throughout the aircraft
Where can you see the systems Load Shed?
Synoptic
SYS - ELEC page, bottom middle
Where does the power for starting eng 2 come from
assisted by Large Motor Power System
indicated on the Synoptic page