# SDR CALA2020010600073

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 2, 2020
- Submitted: January 6, 2020
- Operation: Air carrier
- Aircraft: [N801UA](https://openairdocs.org/aircraft/N801UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 686
- Aircraft time: 71,720 hours, 30,389 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Pressure Panel
- Part number: D53370901210
- Condition: Cracked
- Location: Fuselage
- 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/CALA2020010600073

## Discrepancy

RH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLES 2,3,4,14,16,18 ,19,20,21,22,24,25,26,27,28 ARE CRACKED IN THE PRESSURE PANEL. H OLE 2 IS ALSO CRACKED IN THE CORNER FITTING SUPPORT TASK AD 2018 -06-04 PER HAECO LCQ NR 9290282 GENERATED ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02550 PART 1.ALL WORK ACCOMPLISHED ON HAECO NR 9290282.INSPECTIONS REQUIREMENTS FOR EC RA 5331-02550 ACCOMPLISHED ON LP 4162286 AND LP 4163200 RII INSP ACP

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