# SDR DALA2026053103303

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 30, 2026
- Submitted: May 31, 2026
- Operation: Air carrier
- Aircraft: [N341NW](https://openairdocs.org/aircraft/N341NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 380
- Aircraft time: 96,420 hours, 43,802 cycles
- System (JASC): [5315 · Fuselage Main, Floor Beam](https://openairdocs.org/jasc/5315)
- Part: Floorbeam
- Condition: Cracked
- Location: Zone 200
- Stage of operation: IN
- How discovered: O
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA2026053103303

## Discrepancy

AD RELATED AA 5711-01036-CENTER WING FRONT SPAR VERTICAL STRINGERS, CRACKS FOUND ON FLOORBEAM SIDE VERTICAL RADIUS AT-Y765 ZONE 1 CRACK L= 0.250 INCHES APPROX AT ZONE 2 CRACK L= 0.400 INCH APPROX, REPAIR IS R EQUIRED PRIOR TO FUTHER FLIGHT.  COMPLIED WITH ER/A 587692-14AD REV.B MATCHES WITH ALL STEPS ON ER/A 587692-14AD REV.B PRI REV.0 AND ER/A 587692-14AD REV.B PRIREV.1 IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON CENTER WING FRONT SPAR FR36 AT VERTICAL STIFFENER AND FLOOR BEAMAS PER ER/A 587692-14AD REV.B SECTION III HAS BEEN COMPLIED WITH. APPROVED DATE: 29-MAY-26. SEE LOG PAGE 1619499 FOR TIMECONTROLLED ITEMS SECTION IV: REPETITIVE INSPECTION WITHIN EVERY 11500FC/23000FH (WHICHEVER COMES FIRST) AFTER SECTION III. SEEINDIVIDUAL SIGN-OFF ON ORNRC 280/200. RII INSPECTION COMPLETE. (LP: 1621767, AIRCRAFT WAS GROUNDED)

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