What was found
AIRCRAFT RETURNED TO PLATFORM DURING TAXING, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO WHEEL WELL FIRE, WING AND BODY OVERHEAT DETECTION CONTROL MODULE IAW FIM 26-18 TASKS 801 AND 802, SHOWING FAILURE CODE 64 “RIGHT WING LE AND AC PACK BY ALARM”. AIRCRAFT WAS SENT TO THE HANGAR AND BOTH ENGINES WERE RUN AT 70% OF N1 IAW AMM 73-21-00, NO CONFIRMING THE FAILURE. AS A PRECAUTIONARY ACTION, THE COMPARTMENT DETECTION CONTROL MODULE WAS REPLACED IAW AMM 26-18-00, TESTED CORRECT.