# SDR HALA2019030600090

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 5, 2019
- Submitted: March 6, 2019
- Operation: Air carrier
- Aircraft: [N360HA](https://openairdocs.org/aircraft/N360HA), registered now
- Make and model: Airbus A330-243
- Registry model: [Airbus A330-243](https://openairdocs.org/model/airbus-a330-243) (OpenAirDocs)
- Aircraft serial: 1732
- Aircraft time: 12,402 hours, 1,898 cycles
- Engine: Rroyce RB211TRENT77
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Blade
- Part number: 43723190003
- Part serial: 64996
- Condition: Damaged
- Location: Nr 2 Engine
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/HALA2019030600090

## Discrepancy

ETOPS SIGNIFICANT SYSTEM - FOUND DAMAGE ON NR 15 COMPRESSOR BLADE ON NR 2 ENG. 5 INCHES FROM BLADE TIP DENT DIMENSION X AT .162 INCH DIMENSION Y .094 DIMENSION Z 1.04 INCH. FOUND DIM X=.162 DIM Y=.094 DIM Z= 1.04. FOUND TO BE OUT OF LIMITS PER AMM 72-31-41-000-801-A. REMOVED AND REPLACED LP COMPRESSOR BLADE NR 15. INSTALLED SHIP SET LP COMPRESSOR BLADES PER AMM 72-31-41-400-801-A, TO FACILITATE LP COMPRESSOR BLADE RESHUFFLE. ACCOMPLISHED TEST 11 ENGINE VIBRATION SURVEY OF NR 2 ENGINE PER AMM 71-00-00-700-838-A. OK FOR SERVICE.

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