# SDR YENA2026021100187

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 8, 2026
- Submitted: February 11, 2026
- Operation: Air carrier
- Aircraft: [N613JB](https://openairdocs.org/aircraft/N613JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02449
- Aircraft time: 76,940 hours, 27,768 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/YENA2026021100187

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00032) REF AE NR 2025-717375, WO 2025-414/1 - **FUR-A320-53-02840 CREATED ***, PERFORMED PERMANENT REPAIR ON HOLE A AT FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA IAW A320 SRM      53-11-12-300-012 THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED THRESHOLD FROM TIME OF ADL/ REPAIR  EMBODIMENT 6800FC/FH NOT RELEVANT SUBSEQUENT INSPECTION AT 6800FC/FH NOT RELEVANT INTERVALS UNTIL 60000 FC/ FH NOT RELEVANT INSPECTION METHOD FOR LEADER AND ASSOCIATED HOLE ROTOTEST INSPECTION IAW   A320 SRM 53-11-12-205-008 TABLE 1.

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