Wiring Ignition for 912iS
1. Is it possible to isolate the Battery and use a dedicated charger powered into the VPX in flight and switch to 110V AC on the ground?
2. How is Generator B integrated into the VPX? – Is it useful or should I reserve that VPX circuit for an external Alternator?
3. How is the connection between Buss A and Buss B accomplished? – All internally by the engine wiring?
4. How is the engine shut down under normal circumstances? – Turning off Line A and Line B?
5. Is it correct that if generator A fails, generator B would take over
6. Also if generator A and B fail, the Battery would take over. How are the two busses connected in those situations?