# SDR AU000381

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 15, 2000
- Submitted: June 23, 2000
- Operation: Air carrier
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Engine: Cfmint CFM565A1
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Corroded
- 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/AU000381

## Discrepancy

(AUS) FUSELAGE FRAME 20 LOCATED IN R1 DOOR CUTOUT SEVERELY CORRODED.AREA OF CORROSION 152.4MM BY 101.6MM (6IN BY 4IN) WITH A MAXIMUMDEPTH OF 2.8MM (0.112IN). EVIDENCE OF PREVIOUS CORROSION REMOVALIN THE SAME AREA.

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