What was found
97-223 - CONTROL WHEEL TRIM SWITCHES INOP BOTH SIDES. REPLACED R-29 PHASE SEQUENCE RELAY. SYSTEM G/CS NORMAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
97-223 - CONTROL WHEEL TRIM SWITCHES INOP BOTH SIDES. REPLACED R-29 PHASE SEQUENCE RELAY. SYSTEM G/CS NORMAL.