What was found
(CAN) AIRCRAFT ABORTED TAKEOFF DUE TO #2 ENGINE OIL PRESSURE FLUCTUATING 45-60 POUNDS. INSPECTION FOUND THE HYDRO MECHANICAL UNIT FUEL PUMP GARLOC SEAL LEAKING. THE GARLOC SEAL WAS REPLACED AND THE AIRCRAFTRETURNED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) AIRCRAFT ABORTED TAKEOFF DUE TO #2 ENGINE OIL PRESSURE FLUCTUATING 45-60 POUNDS. INSPECTION FOUND THE HYDRO MECHANICAL UNIT FUEL PUMP GARLOC SEAL LEAKING. THE GARLOC SEAL WAS REPLACED AND THE AIRCRAFTRETURNED TO SERVICE.