Finishing the planning of my dual HDX panel and trying to understand system redundancy and failure modes. If wiring a SV-GPS-2020 per the installation manual, the unit is powered via spliced voltage and spliced serial data from both HDX displays. I am sure the thinking is that a a failure of one display would not cause the GPS to lose power, but wondering about a dead short in one display or junk serial data from one HDX display corrupting the other.
Any thoughts on this? My installer recommends dual GPS units, but I am honestly not sure how necessary another $600 receiver is for a plane that also has a G5 and GTN650 for backups.
I am installing dual ADAHRS and a backup battery for the avionics power bus for IFR flight. Any other recommendations? Thanks in advance for any thoughts,
Dan
Any thoughts on this? My installer recommends dual GPS units, but I am honestly not sure how necessary another $600 receiver is for a plane that also has a G5 and GTN650 for backups.
I am installing dual ADAHRS and a backup battery for the avionics power bus for IFR flight. Any other recommendations? Thanks in advance for any thoughts,
Dan