What was found
ENG 1 OVHT LOOP A CREW REPORTS WARNING ON CLIMB OUT. WHEN THROTTLES PLACED TO IDLE ENG1 OVERHEAT LIGHT ILLUMINATED WITH ENGINES OFF. ACP ENG APU REF FIM 26-10 TASK 811 REPLACED P8-1 PEDESTAL FIRE DET ENG APU MODULE REF AMM CONDUCTED AMM SUBTASK 26-00-01-720-001 STEP (2). PASSED. WARNING WENT OUT. ADVANCED THROTTLE FOR LANDING WITH NO CONTROL MODULE BITE PER FIM 26-10 801. NO FAULTS 26-00-01-400-801. ALL INSTALLATION TESTS NEED TO BE ACCOMPLISHED WARNINGS. ALL ENGINE INDICATIONS NORMAL AND MATCHED NR 2 ENG. REF AMM 26-00-01-400-801 PARA 3.G REQUESTING INSPECTION FOR INSTALLATION OF PERFORMED TEST (9) WHEEL WELL, WING AND LOWER AFT BODY OVERHEAT SQUIB CONNECTORS. DETECTION SYSTEM - OPERATIONAL TEST, TASK 26-18-00-710-801, OPS TEST OK. AIRPLANE HAS BEEN RETURNED BACK TO USUAL CONDITION REF AMM 26-00-01-400-801. IN COMPLIANCE WITH AMM: 26-21-00-730-801 AND IDT CONDUCTED AMM SUBTASK 26-00-01-720-002 STEP (3). PASSED PERFORMED TEST (4): ENGINE FIRE EXTINGUISHING BOTTLE SQUIB PERFOREMED TEST (6) APU FIRE SWITCH SYSTEM SHUTDOWN TEST. OPS REF AMM 26-00-01-400-801. PERFORMED TEST (7) APU FIRE PER TOMC FULL POWER ENGINE RUN MUST BE PERFORMED TO CONFIRM THAT ADD EMP:U224567 CIRCUIT TEST, AND TEST (5): ENGINE FIRE EXTINGUISHING BOTTLE CHECK GOOD. REF AMM: 26-22-00-720-801 EXTINGUISHING BOTTLE SQUIB CIRCUIT TEST