# SDR EE4Y2022020515086

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 5, 2022
- Submitted: February 5, 2022
- Operation: General aviation
- Filed by: [Cooperativa Autogestionaria de Servicios Aeroindus, repair station EE4Y151M](https://openairdocs.org/faa-repair-station/EE4Y151M/cooperativa-autogestionaria-de-servicios-aeroindus.md) (OpenAirDocs)
- Aircraft: [N311NV](https://openairdocs.org/aircraft/N311NV), registered now
- Make and model: Airbus A319-111
- Registry model: [Airbus A319-111](https://openairdocs.org/model/airbus-a319-111) (OpenAirDocs)
- Aircraft serial: 02702
- Aircraft time: 42,792 hours, 27,765 cycles
- System (JASC): [5300 · Fuselage Structure (General)](https://openairdocs.org/jasc/5300)
- Part: Skin Panel
- Part number: UNK
- Part serial: UNK
- Condition: Corroded
- Location: Zone 100
- Stage of operation: IN
- How discovered: V
- Nature of condition: Z
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/EE4Y2022020515086

## Discrepancy

DURING THE STRUCTURE INSPECTION, IT WAS FOUND REAR FUSELAGE PASSENGER/CREW DOOR LH CUT OUT AREA FROM FR68 TO FR69+150MM SILL WITH CORROSION. 
ACTION: 
PERFORMED PERMANENT REPAIR AT PAX/CREW DOOR LH LOWER SILL WEB FROM FR68 AND FR68+160MM, +Y 1260 IAW A319 SRM TASK 53-41-14-300-001  FIG 001, DETAIL M, SHEET 5 AND 9 REPAIR PRINCIPLE 8.

---
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.
