# SDR YENA2025123001297

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 27, 2025
- Submitted: December 30, 2025
- Operation: Air carrier
- Aircraft: [N583JB](https://openairdocs.org/aircraft/N583JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 01250
- Aircraft time: 82,933 hours, 29,648 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: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/YENA2025123001297

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ4 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.115 INCH . CRACK DIRECTION 11 AND 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623135 WO 2025 278/1 CCOMPLISHED REPAIR ON HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS #4 IN CENTER FUSELAGE ON FRAME 36 IN ACCORDANCE WITH AEROMAN #EA 57-0108-25 REV. 0 (COVER- PARTS 1-3) AND AIRBUS RDAF 81679714/004/2025 ISSUE A I.A.W EC NO. A25-1124-01. THIS REPAIR IS CATEGORY A NO REQUIRED FURTHER INSPECTION REQUIRED.

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