System Electrical Flashcards
DC sources (4)
Batteries 2
External DC power
DC starter/generator 2
TRU 2
AC sources 4
APU
AC generators 2
Inverters 9
External AC
Batteries
2x24 volt DC
Engine/APU start
Backup power source
DC starter/Generator
One per engine
Starters to crank engine
Revert to generator when engine reaches idle speed
Produce 28V DC limited to 300 amps
TRU
Convert AC to DC
Ensure DC available even if both generators fail
Both can run off one generator through cross-feed bus
In the nose
APU
115 volt 400hz variable frequency
Cannot start engine
Provides AC power for ATS via AC generator, charging battery and hydraulic system
Supplies air conditioning via bleed air
Fuel from left main
Extinguisher automatic, Temperatures above 182-227°, APU is shut down. 15 seconds later, the extinguisher is discharged. Red doll eye
AC generators
Do not work until prop unfeathered
Produce 3 phase 115V variable freq AC power
Each phase output powers different bus
Variable freq AC used to power: TRU, Anti-icing, Sby aux fuel pumps
Inverters 9
DC to AC
ATS: fixed frequency power to the NIM, Doppler and cooling (in the floor)
Radar (nose)
Avionics
Electrical anti-icing
Kind of power
Areas
Powered by Freq AC prop blade (not on ground and below 900RPM) pitot tubes static ports Stall warning transducers (DC on ground and AC in air after PSEU) Engine intakes Windshields Pilot side window (42°) elevator horn
Can all DC and AC services be operated from the AC generators or from external AC
Yes
What is the ESU with regard to the APU?
Electronic Sequence unit provides automatically-controlled APU start sequencing and malfunction indication
Also has built-in fault monitoring which automatically shuts down APU if detection of faults occurs
Fixed frequency
Provided by 3 Inverters
- 2 for NAV interface Module, Doppler and computer rack cooling fans
- 1 to maintain the AC power synchronization