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Bus 1
connects to avionics bus 1
Bus 2
connects to avionics bus 2
avionics bus 1
PFD, ADC, AHRS, GEA
avionics bus 2
MFD, GTX, avionics cooling fan, audio panel and autopilot system
cross feed bus
connects #1 and #2, alternate master switch and also to all warning systems
Essentials
only standby is connected to it
PECANS
PFD
engine airframe unit
COM 1
ADC and AHRS
NAV 1
standby indicator lights
batteries
both 24 volt and connected to a 28 volt system
only there to start engine and then in case of alternator failure
volt vs amps
volts = electrical potential
amps = the current/ flow of electricity
alternator
60 amps
belt connects to the crankshaft
re charges system