What was found
ON APP RECEIVED LEADING EDGE LIGHT, AIRPLANE WAS FULLY CONFIGURED WITH FLAPS 25. RAN THE QRH FOR LE SLAT DISAGREE AND FOLLOWED THE CHECK LIST TO THE LEADING EDGE SLAT ASYMMETRY CHECK LIST. THE AIRPLANE FLEW NORMALLY WITH NO ASYMMETRIC INPUTS. NO ASSOCIATED EICAS MESSAGE, PERFORMED OPERATIONAL TEST OF LEADING EDGE SLAT SENSOR SWITCH REF AMM 27_88_00_5_0 NO FAULTS FOUND, PERFORMED LEADING EDGE SLAT SYSTEM TEST REF B767 AMM 27_81_00_5_0 NO FAULTS NOTED, AFTER PUSHING LEADING EDGE CONFIG LIGHT SWITCH IN, LIGHT WENT OUT, REPLACED BULBS PER SPM ALL CHECKS PASSED, NO PREVIOUS HISTORY ACFT OK FOR SERVICE