What was found
AFTER ACFT ROTATION EICAS DISPLAYED L/E SLAT DISAGREE WITH THE FLAP LEVER IN 5. OVERWEIGHT LANDING, 1000KG LW 1293 KG NO HARD LANDING. HARD LANDING INSPECTION WAS PERFORMED IAW AAM 05-51-35 PAGE 201 TO 203 PHASE I OPTION A. NO DAMAGE FOUND. DURING BITE TEST TO PSEU, IT SHOWS FAULT CODE 010 CARD. PROXIMITY SW ELECTRONIC UNIT WAS R & R IAW AMM 32-09-4, PAGE 401-406. TEST OK IAW AMM32-09-04, PAGE 406. FLAP/SLAT ELECTRONIC UNIT WAS R & R AS TROUBLESHOOTING IAW AMM 27-51-01, PAGE 401 TO 406. BITE TEST OF THE FSEU IAW AMM 27-51-0, PAGE 550 TO 551 TEST OK. A VERIFICATION FLIGHT WAS PERFOMED TO CONFIRM C/A. NO DISCREPANCIES WERE NOTED.