# SDR CALA2020010600074

- 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/CALA2020010600074

## Discrepancy

LH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLE 2,3,4,14,15,16, 17,19,20,22,23,24,25,26,27 AND 28 ARE CRACKED TO THE PRESSURE PA NEL. HOLE 28 IS ALSO CRACKED IN THE TITANIUM ANGLE SUPPORT TASK AD 2018-06-04 PER HAECO LCQ NR 9290281 GENERATED ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02552 PART 1.1 ALL WOR K ACCOMPLISHED ON HAECO NR 9290281.DIP INSPECTIONS ACCOMPLISHED ON LP 4170731,4170926,4171282 AND 4171103. RII INSP ACP

---
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.