As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENG HAS FUEL LEAK POSSIBLE FUEL CONTROL OR TVBC ACTUATOR ENGINE WILL HAVE TO BE RERUN TO VERIFY. FOUND 2.5 BLEED ACTUATOR LEAKING FROM MATING SURFACE. CONTINUE INSTALLATION OF NEW ACTUATOR FROM MM. PARA 3G(4) HYD ADJ TEST TO COMPLETION.