As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SUSPECT RIGHT LEADING EDGE FLAP DRIVE MECHANISM. NR 1 SFCC RPL ON DIFFERENT LOG GRIPE. REPLACED FIXED PROBLEM. PERF COMPLETE OPS CHECK OF SLATS REF AMM 27-84-00-710. NO FAULTS DETECTED. PERF ALL CFDS TESTS ON SLAT SYSTEM NO FAULTS DETECTED. REPLACE OF SFCC FIXED PROBLEM.