As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ASH 9432 CLT TO CLT, RETURNED TO THE FIELD FOR THE NR 2 HYDRAULIC SYSTEM LOW PRESSURE AND QUANTITY. MX FOUND EVIDENCE OF HYD FLUID IN THE LT WING FUEL SYSTEM. MX TOOK FLUID SAMPLES FROM E1 AND E2 FUEL FILTER. FOUND DAMAGED LINE IN RT TANK. MX COULD NOT REPAIR REC'D TUBE ASSY FROM BOMBA. FUEL SAMPLE RESULTS WERE BEYOND ALLOWABLE LIMITS. NR 2 ENGINE FUEL CONTROL AND FUEL PUMP WERE CHANGED. FUEL PUMP P/N 6078T39P04 S/N REMOVED CGWT0595 (TT-21042 TC-17580 TSO-5546 CSO-2351 MFGR- GE).