As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 2 ENG FUEL SOV ACTUATOR FUNCTION FAIL. IAW AMM 28-22-01-404-057 REV 85, REMOVED NR 2 ENG SOV ACTUATOR. IAW AMM 28-22-01-404-056 REV 85 STEP 3A TO E, INSTALLED NR 2 ENG SOV ACTUATOR & IAW AMM 28-22-00-705-108 REV 85, PERFORM NR 2 ENG SOV OPERATION TEST. RESULT WAS SATISFACTORY. CONDITION CHECKED NORMAL.