What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft departed gpz for IFR flight to wdg. While enroute aircraft encountered total electrical failure after pilot turned on prop de-ice. The pilot made a VFR approach to FAR and landed with the gear partially extended as he had not fully extended the gear manually. Both propellers, nose gear bellcrank, all antennas on the fuselage belly and skins were damaged. Post incident investigation revealed the right alternator field wire to be separated from the connector on the stude. Review of the pilot statement revealed the aircraft battery was dead prior to the flight due to the door light being left on after the last flight. The pilot had the aircraft jump started with external power and proceeded with the IFR flight with a completely discharged battery. When IFR, the pilot lost all electrical when prop deice was selected. This likely happened due to the battery not having any reserve and the likely loss of right alternator leaving the left alternator to carry all load which it could not do.
As the FAA filed it
(-23) AIRCRAFT DEPARTED GPZ FOR IFR FLIGHT TO WDG. WHILE ENROUTE AIRCRAFT ENCOUNTERED TOTAL ELECTRICAL FAILURE AFTER PILOT TURNED ON PROP DE-ICE. THE PILOT MADE A VFR APPROACH TO FAR AND LANDED WITH THE GEAR PARTIALLY EXTENDED AS HE HAD NOT FULLY EXTENDED THE GEAR MANUALLY. BOTH PROPELLERS, NOSE GEAR BELLCRANK, ALL ANTENNAS ON THE FUSELAGE BELLY AND SKINS WERE DAMAGED. POST INCIDENT INVESTIGATION REVEALED THE RIGHT ALTERNATOR FIELD WIRE TO BE SEPARATED FROM THE CONNECTOR ON THE STUDE. REVIEW OF THE PILOT STATEMENT REVEALED THE AIRCRAFT BATTERY WAS DEAD PRIOR TO THE FLIGHT DUE TO THE DOOR LIGHT BEING LEFT ON AFTER THE LAST FLIGHT. THE PILOT HAD THE AIRCRAFT JUMP STARTED WITH EXTERNAL POWER AND PROCEEDED WITH THE IFR FLIGHT WITH A COMPLETELY DISCHARGED BATTERY. WHEN IFR, THE PILOT LOST ALL ELECTRICAL WHEN PROP DEICE WAS SELECTED. THIS LIKELY HAPPENED DUE TO THE BATTERY NOT HAVING ANY RESERVE AND THE LIKELY LOSS OF RIGHT ALTERNATOR LEAVING THE LEFT ALTERNATOR TO CARRY ALL LOAD WHICH IT COULD NOT DO.