# SDR 04FDEA02657

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 6, 2004
- Submitted: September 8, 2004
- Operation: Air carrier
- Aircraft: [N609FE](https://openairdocs.org/aircraft/N609FE), registered now
- Make and model: Doug MD-11F
- Registry model: [Doug MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (OpenAirDocs)
- Aircraft serial: 48549
- Aircraft time: 40,254 hours, 9,190 cycles
- Engine: Ge CF680
- Engine time: 38,344 hours, 8,755 cycles
- System (JASC): [7261 · Turbine Engine Oil System](https://openairdocs.org/jasc/7261)
- Part: Engine
- Condition: Leaking
- Location: Nr 2
- Part time: 36,034 hours, 8,356 cycles
- Stage of operation: CR
- How discovered: O
- Nature of condition: K, J
- Precautionary procedure: E, A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/04FDEA02657

## Discrepancy

AFTER START NR 2 ENG OIL WAS APPROX 15 QTYS. AFTER 1 37 OIL QTY DECREASED TO 10 QTYS.  MONITORED AND SLOW LEAK OVER THE NEXT 45 MIN DOWN TO 4 QTYS. NR 2 ENG SHUT DOWN AT 6 QTYS. OIL TEMP AND PRESS NORMAL DURING THE LEAK.  FND OIL TUBE ASSY P/N 1800M14G01 BROKEN. ALSO, OIL PRES S/W MOUNT BROKEN.   R/R'D LOW OIL PRESS SW S1-8121 PER 79-33-02-4-1 DUE ITS MOUNTING FLANGE BROKEN.   R/R'D OIL PRESS TXMTR PER 79-33-01-4-1 DUE POSSIBLE INTERNAL LEAK.  R/R`D GASKET SEAL AT CONNECTION OF OIL SUPPLY LINE REF GE IPC79-00-00 FIG25 ITEM75 FOR PRECAUTIONARY MEASURE DUE ONLY LOWER PORTION OF FAN COWL GETTING OIL ON IT.  INSTALLED TUBE, NR 2 ENG PER MD11JRH CHPT-5, NO LEAKAGE NOTED AND ALL PARAMETERS ARE NORMAL.

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