# SDR DALA2025110608079

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 5, 2025
- Submitted: November 6, 2025
- Operation: Air carrier
- Aircraft: [N349NW](https://openairdocs.org/aircraft/N349NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 417
- Aircraft time: 95,083 hours, 43,979 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Condition: Damaged
- 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/DALA2025110608079

## Discrepancy

OVERSIZE DIAMETER HOLES JOGGLE AREA FR16 RT, AT DOOR STOP FITTING 7. HOLES H1: 0.2641 H2: 0.3305 H3: 0.2663 H4: 0.3263 H5: 0.2662 H 6: 0.3339 H7: 0.2039 H8: 0.2634 HOLE A: 0.2073 HOLE B: 0.2634 HOLE C: 0.2264 HOLE D:0.2636.  COMPLIED WITH ER/A 558682-14AD REV. A,  MATCHES WITH ALL STEPS ON PRI 558682-14AD REV 0, PRI 558682-14AD REV 1, PERFORMED REPAIR INSTRUCTIONS ON FRAME 16R DOOR STOP 7 FUSELAGE SKIN AS PER ER/A 558682-14AD REV.

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