# SDR DALA12016233210

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 13, 2012
- Submitted: December 17, 2012
- Operation: Air carrier
- Aircraft: [N310NW](https://openairdocs.org/aircraft/N310NW), registered now
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Aircraft serial: 121
- Aircraft time: 68,007 hours, 30,286 cycles
- System (JASC): [5340 · Fuselage Main, Attach Fittings](https://openairdocs.org/jasc/5340)
- Part: Attach Fitting
- Condition: Chafed
- Location: Fuselage
- 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/DALA12016233210

## Discrepancy

DURING INSPECTION, FOUND CHAFED MARK ON LT AFT PAX DOOR ASSIST CYLINDER ATTACHMENT FITTING.  BLENDED OUT DAMAGE IAW SRM 51-73-00.  DIM OF REWORK L=.4", W=.2", D=.008", NO ALLOWABLE LIMITS PROVIDED.  HFEC ACCOMPLISHED IAW NTM 51-10-08, NO CRACKS OR OTHER DISCREPANCIES REPORTED.  NO ADDITIONAL DAMAGE TO ADJACENT STRUCTURE DETECTED AND CAUSE WAS UNABLE TO BE DETERMINED.  COMPLY WITH FINAL ER/A 509270-14 REV ORIGINAL SECTION I PERMANENT REPAIR.

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