My "B" alternator voltage, measured by voltmeter at the battery terminals and also reported by my DyYnon Skyview is 13.9 volts (Voltmeter 13 .94, Skyview 13.9). This is with a nominal 2A charging current and a system load of maybe 5A. The "A" Alternator output, as reported by the CAN bus is 14.1V
13.93 volts is at the very low end for charging and balancing the cells of a Lithium battery, which is causing problems in flight. The rotax manual specifies a nominal voltage of 14.2V. This problem is a PITA. Is there an adjustment anywhere for the B alternator voltage or some other fix? The aircraft and charging system is wired as per Rotax installation manual.