# SDR WX0A2026100232969

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 1, 2026
- Submitted: October 5, 2026
- Operation: Air carrier
- Aircraft: [N261NV](https://openairdocs.org/aircraft/N261NV), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 4115
- Aircraft time: 41,465 hours, 25,859 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Beam
- Condition: Corroded
- Location: Zone 100
- 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/WX0A2026100232969

## Discrepancy

(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0049: BULK CARGO COMPARTMENT, SILL BEAM BTW FR60 - FR62 FOUND CORRODED. TO BE INVESTIGATED. / BULK CARGO COMPARTMENT, AFTER REMOVAL OF CORROSION ON 4X ANCHOR NUT AREA OF SILL BEAM BTW FR60 - FR62 FOUND OUT OF LIMITS AS PER SRM 53-41-49-283-001 REV. 159. SILL BEAM WAS REPAIRED AS PER SRM 53-41-49-300-003 REV. 159. REPAIR IS CATEGORY B WITH FUTURE INSPECTION AS PER SRI 53-41-49-205-001 REV. 159.  INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT: 60000 FC/ 120000FH (WHICHEVER FC/FH IS ACHIEVED FIRST), SUBSEQUENT INSPECTION AT INTERVALS OF: TBD, METHOD OF INSPECTION: TBD (TO BE DEFINED IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60000FC/120000FH, WHICHEVER IS ACHIEVED FIRST)."

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