# SDR AWXA200400182

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 14, 2004
- Submitted: February 17, 2004
- Operation: Air carrier
- Aircraft: [N626AW](https://openairdocs.org/aircraft/N626AW), registered now
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 65
- Aircraft time: 46,499 hours, 20,891 cycles
- System (JASC): [5321 · Fuselage Floor Panel](https://openairdocs.org/jasc/5321)
- Part: Floor Panel
- Part number: D5367004100000
- Condition: Delaminated
- 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/AWXA200400182

## Discrepancy

DURING C-04 CHECK RT OB CABIN FLOOR PANEL (252VF) WAS FOUND DELAMINATED BETWEEN FR 60 AND FR 64, RBL 46 TO RBL 65.  MAINTENANCE REMOVED DELAMINATED FLOOR PANEL (252VF); FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG D53670041; INSTALLED NEW PANEL IAW A320 SRM 53-02-00, FIG. 209, PG. 233-236.

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