Originally Posted by
TiredSoul
Separate power sources, separate standby Air Data Computer, standby extra everything.
Interesting and nice looking consolidation. I've seen it before but always wondered about the following:
Separate Power Source
Does that mean a separate Bus, or a different path off the same Bus?
ADC Standby
Would the standby ADC drive input to Conventional Instruments? The all-in -one Glass backup shows Attitude, Airspeed and Altitude. What happens if/when ADC is lost to that single unit and/or if electrical is lost to that single unit? Assumes a double failure of the primary GDU and All-In-One backup.
In that scenario, would having stand-alone Conventional units still provide coverage?