# SDR YENA2025032000291

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 19, 2025
- Submitted: March 20, 2025
- Operation: Air carrier
- Aircraft: [N766JB](https://openairdocs.org/aircraft/N766JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 03724
- Aircraft time: 61,218 hours, 21,880 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/YENA2025032000291

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA. CRACK DEPTH 0.100 INCH. CRACK DIRECTION 9 OCLOCK; (RESOLVED ON W/O: 1353243 TASKCARD: NR-00021) FUR-A320-53-02090, REF AEROMAN N/R 2025-125700, MESURE OF DIAMETER ON OPEN HOLE D FR16LH DOUBLE JOGGLE AREA.IS 0.248IN. PERFORMED PERMANENT REPAIR ON HOLE D FR16LH JOGGLE AREA I.A.W A320 SRM 53-11-12-300-012 FIGURE 004 AND FIGURE 008, HOLE #D FRAME 16 LH DIAMETER MEASURED: 10.150 MM. (0.3996 INCH)THIS REPAIR IS CAT B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 6800FC /FH NOT RELEVANT, SUBSEQUENT INSPECTIONS AT INTERVALS OF 6200FC / FH NOT RELEVANT I.A.W A320 SRM 53-11-12-205-008 TABLE 1.

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