What was found
DURING CLIMB OUT AFTER TAKEOFF, NR 1 ENGINE COULD ONLY PRODUCE 85 PERCENT N1. WHILE RETURNING TO BASE , ENGINE SHUT ITSELF DOWN ON 2 MILE FINAL. TROUBLESHOOTING FOUND THAT FUEL FLOW DIVIDER HAD MALFUNCTIONED. FUEL FLOW DIVIDER WAS REMOVED FROM SERVICE, AND REPLACED WITH AN OVERHAULED UNIT. AIRCRAFT WAS RETURNED TO SERVICE. (K)