# SDR EE4Y2024122321462

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 23, 2024
- Submitted: December 23, 2024
- 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: [N271NV](https://openairdocs.org/aircraft/N271NV), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 2932
- Aircraft time: 38,234 hours, 26,384 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Zone 200
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/EE4Y2024122321462

## Discrepancy

DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-002 UPPER FUSELAGE FR66 LH SIDE DOOR STOP FITTING # 1 AT UPPER AND LOWER I/B HOLES WITH CRACK INDICATION  WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR66 LH STOP FITTING # 1 DUE TO WEB WITH CORROSION AND CRACKED HOLE IAW COOPESA EO # COO-EO-2024-21364-R00 DATED 12-12-2024 AND AIRBUS TD 81502943/032/2024#A. DOCUMENTED APPROVED AND SUBMITTED ON AIRBUS REPAIR AND DESIGN APPROVAL FORM RDAF REF ISSUE 81502943/004/2024#A APPROVED BY ALLEGIANT UNDER ERO A32X-STR-53ERO-00127-R00. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P229 ITEM 2-51.

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