Alternator B Failure Diagnosis
I’m working on a 912iS aircraft that is not charging the battery. I have the problem diagnosed to the alternator B stator, but I’m hoping to get a couple of you to shoot holes in (or confirm) the diagnosis before I order a stator assembly. Originally I missed diagnosed this as the Voltage Regulator B, so that has been replaced and did not solve the problem.
These are the test results:
1. Stator B ohm readings are between .5 and .7 ohms measuring between any two of the three yellow leads with the connector unplugged from the regulator. This is similar to Stator A (and misleading).
2. Stator B open circuit output voltage is 3-6 volts between any two of the stator poles (yellow wires). Stator A open circuit voltage is 35 volts.
3. Stator B leads all show grounded with readings between 1 and 2 Ohms from any yellow lead to engine case. Stator A leads show infinite ohms to ground.
My diagnosis is that Stator B has gone to ground, even though the windings are not open. So, voltage is being shunted to ground inside the stator. Is there any reason to take the alternator apart before ordering the Stator? Is there a possible ground failure that might be repaired? I would not think so.