# SDR ASAA2020032532557

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 17, 2020
- Submitted: March 25, 2020
- Operation: Air carrier
- Aircraft: [N624VA](https://openairdocs.org/aircraft/N624VA), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 02778
- Aircraft time: 45,558 hours, 14,314 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Beam
- Part number: D5347219320200
- 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/ASAA2020032532557

## Discrepancy

AFT MAIN CABIN LONGITUDINAL BEAM AT FR 70 RBL 30 HAD CORROSION AT LAVATORY ATTACH POINT HOLE GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 66-70 AT RBL 30. REF AIRBUS DWG D53472836, D53472458, D53472093

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