# SDR 2024F00114

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 9, 2024
- Submitted: April 9, 2024
- Operation: General aviation
- Aircraft: [N212HA](https://openairdocs.org/aircraft/N212HA), registered now
- Make and model: Airbus A321-271N
- Registry model: [Airbus A321-271N](https://openairdocs.org/model/airbus-a321-271n) (OpenAirDocs)
- Aircraft serial: 8129
- Engine: Iae PW1133GJM
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Rotor
- Part number: 30G5908
- Part serial: LENCAU9946
- Condition: Cracked
- Location: Eng Compressor
- Part time: 838,152 hours, 4,938 cycles
- 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/2024F00114

## Discrepancy

DURING THE INSPECTION PHASE, A CRACK IS DETECTED IN A BLADE WITHOUT REPAIR IAW SP1100G-B-72-35-30-00A-310A-B.  DO A VISUAL INSPECTION OF THE HIGH PRESSURE COMPRESSOR (HPC) ROTOR ASSEMBLY FOR SERVICEABILITY TABLE 10. HPC 8TH STAGE (IBR) ROTOR - VISUAL INSPECTION PWA REFERENCE: CAS 21138-R9K8P0 NON REPAIRABLE LIFE LIMITED PART TO BE RETIRED BEFORE END OF LIFE

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