As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON TAKEOFF ROLL THE #2 ENGINE DID NOT PRODUCE TAKEOFF RATED THRUST. THE TAKEOFF WAS REJECTED. MAINTENANCE FOUND THE PROBLEM TO BE AN AIR LEAK. CORR UJOINT AND 3 GASKETS WERE REPLACED ON THE #2 ENGINE FUEL FLOW REGULATOR AT THE P3 CONNECTION. ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.