# SDR CALA2019051700785

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 17, 2019
- Submitted: May 17, 2019
- Operation: Air carrier
- Aircraft: [N808UA](https://openairdocs.org/aircraft/N808UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 804
- Aircraft time: 68,297 hours, 28,755 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Pressure Panel
- 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/CALA2019051700785

## Discrepancy

AD 2018-06-04 EA 5330-05216 DOT NO.A3- NO DOT RT SIDE PRESSURE PANEL BETWEEN FRAME 35 AND 36 ADDITIONAL FASTENERS OUTSIDE THE CUT OUT AREA CRACKED AT 2,5,15,18,20,21,23,24,28,29.  CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT N/R S/N 9618703. ACCOMPLSIHED INTERIM REPAIR ON RT SIDE PRES SURE PANEL BETWEEN FRAME 35 AND 36 CRACKED REF ECRA NO.5331-0238 7. ACCOMPLISH A PERMANANT REPAIR PER PART 3 OF ECRA 5331-02387 ON OR BEFORE 15 OCT 19 FOR PERMANANT REPAIR.

---
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.
