# SDR MU12008F00004

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 22, 2008
- Submitted: November 20, 2008
- Operation: Air carrier
- Filed by: [Aerovias del Continente Americano, S.A., repair station MU1Z335K](https://openairdocs.org/faa-repair-station/MU1Z335K/aerovias-del-continente-americano-s-a.md) (OpenAirDocs)
- Aircraft: [N948AC](https://openairdocs.org/aircraft/N948AC), registered now
- Make and model: Airbus A330-243
- Registry model: [Airbus A330-243](https://openairdocs.org/model/airbus-a330-243) (OpenAirDocs)
- Aircraft serial: 0948
- Engine: Rroyce RB211TRENT77
- System (JASC): [7220 · Turbine Engine Air Inlet Section](https://openairdocs.org/jasc/7220)
- Part: Acoustic Panel
- Condition: Damaged
- Location: Engine
- Stage of operation: IN
- How discovered: B
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/MU12008F00004

## Discrepancy

ENGINE FOREING OBJECT DAMAGE.  MX REPORT DURING TRANSIT CHECK IN BOG ENG N1 WAS FOUND FOD EVIDENCE.  BOROSCOPIC INSPECTION ON HP AND HI COMPRESSOR IAW TASK 72-00-00-200-812 AND PENETRANT LIQUID INSPECTION ON LEADING EDGE OGV IAW TASK 70-20-02-230-804.  NO DAMAGES WERE FOUND.  IAW AMM TASK 72-21-41-000-803 2 ICE IMPACT/REAR ACOUSTIC PANELS WERE REPLACED.  IAW AMM TASK 72-21-41-400-802.  5 OGV ANNULUS FORMER PANELS WERE REPLACED.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.