As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON FINAL, THE CREW HAD AN INDICATION OF L/E SLAT ASYMMETRY. ACTUAL L/E SLATS WERE IN THE CORRECT POSITION ON BOTH SIDES RESOLUTION: CARRIED OUT FMR STEPS 2 TO 4 AND NO FAULTS NOTED. STEP 5 ALSO CARRIED OUT. THE RESISTANCE WAS MEASURED AT 19.7 OHMS. SENSOR S278 ADJUSTED TO 0.105" IAW AMM 27-88-01. OPS TEST OF THE SLAT SYSTEM CARRIED OUT.