I amconfused by table 2-Skyview System Power Requirements. It shows the SV-XPNDR, ADSB-470 drawing current (.4A and .2A respectively) from the display, yet both of the devices have power directly from the aircraft master power like the autopilot servos which per the text above the table use only aircraft master power. So I guess the question is why do the transponder and ADS draw noticable current from the display?
Russ
Russ