What was found
DURING SLAT EXTENSION, DUAL SLAT FAULT SYS 1 AND 2. CYCLED AND SLATS STILL STUCK AT 0 DEGREES. REMOVED AND REPLACED THE NR 1 SFCC IAW AMM 27-51-18-04. OPS CHECKED GOOD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SLAT EXTENSION, DUAL SLAT FAULT SYS 1 AND 2. CYCLED AND SLATS STILL STUCK AT 0 DEGREES. REMOVED AND REPLACED THE NR 1 SFCC IAW AMM 27-51-18-04. OPS CHECKED GOOD.