# SDR YENA2026020400137

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 2, 2026
- Submitted: February 4, 2026
- Operation: Air carrier
- Aircraft: [N587JB](https://openairdocs.org/aircraft/N587JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02177
- Aircraft time: 80,243 hours, 29,180 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/YENA2026020400137

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN OPEN FASTENER LHOLE LOC Y1292 MORE 8 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CNETER WING BOX.  CRACK AT 1 O'CLOCK CRACK DEPTH 0,140 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2025-682715 WO 2025 413/1 ACCOMPLISH REPAIR ON THE CENTER FUSELAGE PRESSURE DECK Y1292 PANEL FR36 LHS ON HOLE #100 I.A.W EC#  A18-465-04, AEROMAN EA 53-0105-25 REV. 0 (COVER), AEROMAN EA 53-0085-25 REV. 0 (PARTS 1-8) AND AIRBUS RDAF 80467398/041/2025 ISSUE A. THIS REPAIR FOR THE LHS PRESSURE PANEL PERFORMED UNDER THIS EA WAS DETERMINATED TO BE MINOR REPAIR CATEGORY B. INSPECTION THRESHOLD 64 400FC/ 121 300FH FROM FIRST FLIGHT, INSPECTION INTERVAL TBD AND METHOD OF INSPECTION TBD. I.A.W AIRBUS RDAF 80467398/041 /2025 ISSUE A. TOOLS USED: P/N NORTEC 600D, S/N: 210138003 DUE DATE AUG-22-2026, MANDREL GAGE P/N: CBMG-10-1-N, S/N:AE-24088, DUE DATE: SEP-25-2026, COMBINATION GAGE P/N: CBG-10-1-N-1, S/N: AE-420240, DUE DATE: SEP-25-2026, SMALL HOLE GAUGES PN: 154-901; SN: AE-411354; DUE DATE: FEB-27-2026, DONE BY L. TORRES 8636723.

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