# SDR DALA2025113008733

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 26, 2025
- Submitted: November 30, 2025
- Operation: Air carrier
- Aircraft: [N340NW](https://openairdocs.org/aircraft/N340NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 372
- Aircraft time: 96,330 hours, 43,943 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- 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/DALA2025113008733

## Discrepancy

CRACK INDICATION FOUND ON INNER CAP FR 68 RH SIDE AREA, CRACK LENGHT: 1.5 INCH, REQUESTING REPAIR DISPOSITION ADITIONAL EGINEERING DOCUMENTA TION IS REQUIRED AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIG HT REFER TO EM 5311-01244 AND SB A320-531491.  COMPLIED WITH ER/A 630590-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 630590-14AD REV 0, PRI 630590-14AD REV 1, PRI630590 -14AD REV 2. IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FUSELAGE FRAME 68RH AT LEVEL OF STR 22R AS PER ER/A630590-14AD REV. ORIGINAL SECTION I HAS BEEN COMPLIED WITH. APPROVED DATE: 24-NOV-25. FOR TIME CONTROLLED ITEMS SEE LOG PAGE #1320268.

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