# SDR DALA2026080704568

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 6, 2026
- Submitted: August 7, 2026
- Operation: Air carrier
- Aircraft: [N352NW](https://openairdocs.org/aircraft/N352NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 778
- Aircraft time: 81,941 hours, 39,111 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Window 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/DALA2026080704568

## Discrepancy

AD 2020-17-03 / A.A WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, L/H R/H CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION.  PERFORMED NOSE FWD FUSELAGE I FRONT WINDSHIELD FRAME AND L/H R/H CONTINUITY FITTINGS REPLACEMENT I/A/W DELTA ER/A NO 635072-14AD SECTION I REV: ORIGINAL DATED 24-JUL-26. NOTE: REPAIR APPROVAL IS LIMITED TO 60.000 TOTAL FLIGHT CYCLES (ESG). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. SECTION DTE AND LOG PAGE #1717978 ARE ESTABLISHED TO ENSURE THAT AIRBUS IS CONTACTED PRIOR TO THIS THRESHOLD FOR INSPECTION METHOD AND REPETITEVE INSPECTION LIMITS. CLOSING ACCESS AND TESTING WAS PERFORMED AS PER ER/A #635408-14 SECTION I REVISION ORIGINAL DATED 05-AUG-26. ASSOCIATED ER/A 00-635072 ADDED FOR AC 3252. (LP: 1741900, AIRCRAFT WAS GROUNDED)

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