As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE HAS FUEL LEAKING FROM LEFT VSV. ACFT GROUNDED. R & R NR 2 ENG LT VSV ACTUATOR IAW AMM 75-31-01. ACCOMPLISHED VSV ACTUATOR LEAK TEST IAW AMM 75-31-01-790-801-F00 TO STEP 7E2D. NOTE HMU ACT HEAD AND ROD LEAK TEST REQUIREMENT ACCOMPLISHED. VSV ACTUATOR LEAK TEST IAW AMM 75-31-01-790-801-F00 7F-7G. ACCOMPLISHED IDLE LEAK CHECK AND VSV ACTUATOR TEST. NO LEAKS OR FAULTS FOUND IAW AMM 71-00-00.