# SDR SOKF20041118

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 18, 2004
- Submitted: November 23, 2004
- Operation: Air carrier
- Aircraft: [N465TA](https://openairdocs.org/aircraft/N465TA), registered now
- Make and model: Airbus A320-233
- Registry model: [Airbus A320-233](https://openairdocs.org/model/airbus-a320-233) (OpenAirDocs)
- Aircraft serial: 1374
- Engine: Iae V2527EA5
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Engine
- Condition: Fod
- Location: Nr 2
- Stage of operation: LD
- How discovered: O
- Nature of condition: C
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/SOKF20041118

## Discrepancy

DURING LANDING, CAPTAIN REPORTED (FOD ON ENGINE NR 2, NO ABNORMAL INDICATION DURING TAXI).  MAINT PERFORMED INSPECTION OF ENGINE NR 2 IAW MM AND FOUND SOME DAMAGES LOCATED ON ATTRITION LININGS AT 5 OCLOCK, ACOUSTIC PANEL AT 4:30, (ENGINE, FROM THE FRONT), SOME SCORES ON INNER BARREL OF INTAKE COWL:  ALL OF THEM ACCEPTABLE IAW MM.  ALSO FOUND DAMAGES OUT OF LIMITS ON FAN BLADES, POSITIONS: 9,13,14,15,16,17,18,20, WHICH WERE REMOVED AND REPLACED IAW AMM.  A FRONT LINER PANEL AT 4 OCLOCK IAW AMM, ADDITIONALLY WAS REPLACED THE RUBBER SEAL AT 5 OCLOCK DUE TO DAMAGES, PERFORMED TEST NR 8 VIBRATION SURVEY IAW AMM AND TEST NR 9.  FAN TRIM BALANCE IAW AMM WITH SATISFACTORY RESULTS AND THE AIRCRAFT RETURNED TO SERVICE.

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