by Tom Straughan » Mon Oct 22, 2012 3:12 am
Since 01/27/12, I have had electrical problems with my twin comanche. Initially, the problem manifested itself through the illumination of the "discharge light" on my Electronic International V/A and the shutdown of both alternators. The 2 A&P's who annualed my plane in April were convinced that I needed a new main voltage regulator. The original voltage regulator was replaced by a Zeftronics unit. When this didn't solve the problem, an electronics specialist told me that my new voltage regulator was bad and after it was replaced, I still had the problem. Next, I replaced the original aux. voltage regulator with a new Zeftronics unit. When I still had the problem, the electronics specialist tested numerous electronic parts and we checked and filed down the battery grounding lug and both engine grounding lugs and all connectors on the attached wires. He became convinced that the main/aux regulator switch needed to be replaced along with both over-voltage relays and each 90-Amp circuit breaker/alternator switches. After purchasing and installing all these components, the problem became somewhat abated, but it seemed that the problem was confined to the right side and another A&P told me to replace the R. E. alternator. Until the new alternator was delivered, I flew 6 flights using only the left alternator and when the "discharge light" did illuminate, I was able to bring the alternators back on-line by switching to the aux voltage regulator. After the new Hartzell Technologies ALX8521 alternator was installed on the R.E., a different problem arose; during engine run-up and during flight with a significant electrical load, the R.E. alternator was supplying 4/5 of the total amp load. Then the new A&P recommended that we replace the L.E. alternator. Another new Hartzell Technologies ALX8521 alternator was installed on the L.E. on 10/19/12 and the problem reversed; that is that the L.E. alternator was supplying 3/5 of the total amp load during engine run-up. In summary, except for the two filters, every electrical/electronic component shown in the non-paralleling alternator wiring diagram has been replaced with new components in my twinco, and numerous old cracked alternator field wires have been replaced and 3 main grounds have been thoroughly cleaned and new Bogert battery cable systems installed and after all this, I now am unable to get the two alternators to equally share the amp load. I really need some help to make this electrical system perform properly!