# SDR YENA2025022500204

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 23, 2025
- Submitted: February 25, 2025
- Operation: Air carrier
- Aircraft: [N586JB](https://openairdocs.org/aircraft/N586JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02160
- Aircraft time: 79,271 hours, 28,961 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- 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/YENA2025022500204

## Discrepancy

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16 RH SIDE AT HOLE A. CRACK DIRECTION 9 OCLOCK (VIEW FROM OUTSIDE) AND CRACK LENGTH 0.100 INCHES (1EA); PERFORMED PERMANENT REPAIR LOC. ON DOUBLE JOGGLE AREA HOLE A ON FR16 RH SIDE IAW A320 SRM  53-11-12-300-012. THIS REPAIR IS CATEGORY B AND INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR  EMBODIMENT 6800 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT OF 5900 FC (FH NOT RELEVANT), INSPECTION METHOD FOR LEADER HOLE REFER TO TASK 53-11-12-300-12 FIGURE 014:  FUR-A320-53-02031

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
