As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON TAKE-OFF, THE AMMETER BEGAN FLUCTUATING BETWEEN 15 AND 30 AMPS CAUSING THE AP 1 TO FAIL. TEST FLIGHT EVALUATION REVEALED AMMETER DIFFERED BY AS MUCH AS 25 AMPS BETWEEN #1 AND #2 SIDES IN FLIGHT, AND THEN CONTINUED TO DIFFER BY 10-20 AMPS ONCE ON GROUND. #2 FLUCTUATED FREQUENTLY AND WAS CONSISTENTLY LOWER THAN #1. REPLACED #2 CURRENT TRANSFORMER IAW AMM 24-30-00, 4-6; A/C OPERATED IAW RFM. MOC OK.