# SDR 06FDEA03800

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 27, 2006
- Submitted: October 30, 2006
- Operation: Air carrier
- Aircraft: [N680FE](https://openairdocs.org/aircraft/N680FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 794
- Aircraft time: 12,164 hours, 6,586 cycles
- Engine: Ge CF680
- Engine time: 12,202 hours, 6,583 cycles
- System (JASC): [7261 · Turbine Engine Oil System](https://openairdocs.org/jasc/7261)
- Part: Magnetic Seal
- Condition: Leaking
- Location: Engine
- Stage of operation: CR
- How discovered: O
- Nature of condition: K, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/06FDEA03800

## Discrepancy

APPROX 1 HOUR OF FLIGHT NR 1 OIL QUANTITY STARTED TO DECREASE.  ALL OTHER INDICATIONS NORMAL.  AFTER  APPROX 2 HOURS OF FLIGHT THE OIL PRESSURE STARTED TO FLUCTUATE PLUS OR MINUS 15 PSI.  PER QRH THIS COULD BE ABNORMAL, DIVERTED TO KDEN.  ENGINE NR 1 LEFT AT IDLE, NO SHUTDOWN.  NO EMERGENCY DECLARED.  OIL LEAKING FROM NR 1 STARTER DRIVE PAD AS PER AMM 71-70-00-6-05 CAPPED STARTER DRIVE PAD DRAIN AND STOWED CLOSED AND SECURED COWLING AS PER AMM 71-13-00.  A/C LIMITED TO 10 CYCLES.  REMOVED AND REPLACED STARTER DRIVE PAD CARBON AND MAGNETIC SEAL REF A300-600 MM 72-65-00-8-05.  REINSTALLED STARTER REF A300 MM 80-13-01-4-05.

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