# SDR 98ZZZX1524

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 26, 1998
- Submitted: March 26, 2000
- Operation: General aviation
- Engine: Lyc LTS101650B1
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Axial Rotor
- Part number: 410100641
- Condition: Separation
- Location: Blade Root
- Part time: 787 hours
- Component: 410102050
- Stage of operation: IN
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/98ZZZX1524

## Discrepancy

AXIAL BLADE SEPARATION AT BLADE ROOT AREA - ENGINE FAILURE.  INVESTIGATION ONGOING.  CORRECTIVE ACTION IN PROGRESS.

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