What was found
EVIDENCE OF HYDRAULIC FLUID ON TAIL SECTION OF AIRCRAFT. AFT FUSELAGE TAIL CONE HAS FLUID SPRAYED (APPEARS TO BE OIL NOT HYD) PREDOMINANTLY ON RIGHT. ACCMP'D CLEANED RESIDUAL OIL. RAN APU, NO ACTIVE LEAKS NOTED. LEAKING LINE ID BY MIDS. P/N BACH8C06EE0274B. LINE FROM BULKED FITTING TO RATIO CHARGER REMOVED LEFT SYS CENTER LINE. ITEM 300 SEAL, ON SHELF WHERE LINE ATTACHES. HELD ON BY TY WRAP AROUND BOOT. PANEL 324CL HAS ONE FASTENER THAT SPINS (NUTPLATE BROKEN). ALL OTHER FASTENERS ON PANEL ARE REMOVED. SECURED FASTNER REINSTALLED PANEL. REPLACED LINE PER IPC. ACCOMPLISHED RUDDER RATIO TEST PER MM AND RUDDER DEFLECTION. LEAK CHECK GOOD. ALL PANELS SECURED. L-C-R HYD RESEVOIRS WERE DEPRESSURIZED & VLV PINNED OPEN FOR RUDDER RATIO CHGR HYD HOSE RPLCMNT. REMOVED PINS. RESV PRESSURIZED.