Question re: Gen 1 failure
In the Sling TSi POH, 3.8.3, for Generator 1 failure, it says, "in this event Generator 2 output is (or only partially) available to the aircraft systems / charge the main battery.”
However, in the Rotax 915is Operator's Manual, 4.1.1, for Failure of Generator 1, it says, "If Generator 2 is used for supplying the EMS, the airframe will not be supplied with electrical power by an internal generator."
So, which is correct? In the event of Gen 1 failure, can Gen 2 still provide partial power to the airframe, or none at all?