As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHEEL WELL LIGHT CAME ON INTERMITTENT ON TAKEOFF FOR ABOUT 1 SEC & AGAIN MOMENTARILY ABOUT 2 MINUTES LATER. INSPECTED WW LOWER BODY OVERHEAT SENSOR M270 & PERFORMED FAULT ISOLATION RESISTANCE CHECK. IAW FIM 26-18-00-810-802 STEP H 8 & I FOR OPEN LOOP CHECK OF SENSOR. SENSOR CHECKED GOOD. R & R OVERHEAT DETECTOR CONTROL UNIT IAW AMM 26-18-01-400-801 & OPERATIONAL TEST IAW AMM 26-18-00-710-801.