Tecnam P2012 Captain reported loss of electrical power during cruise. Captain returned to departure airport and landed safely.
Synopsis
Tecnam P2012 Captain reported loss of electrical power during cruise. Captain returned to departure airport and landed safely.
Narrative
This incident began on the previous day when I wrote up the aircraft due to what appeared to be an inoperative right alternator. I consulted with Maintenance regarding my concerns and the abnormal indications observed. Under an electrical load with the tie bus turned off there was a draw/discharge observed from: the Main amps; main bus; Ess. Bus.; refer to AML (Aircraft Maintenance Logbook) log sheet. Maintenance reviewed the write-up and said 'Performed ground run with load as stated by pilot. R/H alternator functions properly. Inspected Act. R/H belt + wiring. No defects noted.'The following morning I conducted a preflight of the plane in accordance to the Normal Procedure outlined in the QRH; reviewed the AML and corrective actions regarding the write-up. The rest of the morning proceeded normally: GPS update day; start-up; run-up; takeoff. Made contact with Approach and continued the IFR flight as planned; Cruise flight 6;000 direct to ZZZZZ intersection. Current weather at 6;000 hard IMC.During the cruise flight; I decided; since I had some time to check to see if the repair worked as intended. I turned off the Tie bus with an electrical load and the draw/discharge was still present. I noted the electrical loads under different tie bus settings; I then left the Tie bus on. Shortly thereafter; I lost all electrical power from: PFD1 (Primary Flight Display); PFD2; MFD (Multi-function Flight Display); Radios; Autopilot; and heaters and etc with no accompanying CAS (Crew Alerting System) messages. In response; I immediately; began hand flying the plane with the compass and standby instruments. I then switched on the Emergency Back up Path Essential Bus". I understand that the emergency essential bus switch bypasses the main bus and connects the main battery and essential bus. I was hoping to regain some functionality of PFD 1 and its associated systems before turning to the QRH.My understanding is that flipping the emergency Essential Bus switch provides an immediate response of electrical power. This was not the case; but I left the switch on nevertheless.With the Emergency Essential Bus switched on I decided to discontinue the flight and returned back to ZZZ airport on a reverse heading knowing that the weather and traffic flow at my destination would have increased variables and associated risk. Once established on a heading back to ZZZ I consulted the QRH and conducted the "Dual Alternator Failure Checklist". It provided no adequate troubleshooting solution; so I continued with my decision and flew back to ZZZ. I then turned the Emergency Essential Bus Switch off and turned on the Main Battery switch; referencing the "Main Battery Failure checklist" in the QRH. The Emergency battery switch connects all three batteries in parallel onto the main bus and is mainly during a dual alternator failure.This also provided no positive feedback as well.At this point; I determined to stop troubleshooting knowing full well that ZZZ airport would be my best option given the following conditions: single pilot hand flying referencing only the standby instrument and compass; while in IMC with a complete electrical failure. I left both emergency switches on at this point with the hopes that maybe one of them would provide power if any. On my descent back towards ZZZ; I exited IMC and was VMC at approximately 2;500' at some unknown distance from ZZZ. Shortly after entering VMC; I regained power to PFD1 and PFD2 and its corresponding equipment (MFD still out). With ZZZ airport was well within sight; I communicated with ZZZ Ops and informed them that I was coming back to land. I committed to the landing and once on the ground I contacted ZZZ Clearance; canceled IFR; stated the reason for the air return was due to a dual alternator failure. Returned to the gate; parked the plane performed all After Landing; securing checklists. Cause: Potential dual alternator failure."
Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.