# SDR AU000733

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 1, 2000
- Submitted: September 1, 2000
- Operation: General aviation
- 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): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- 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/AU000733

## Discrepancy

(AUS) FUSELAGE SKIN CRACKED IN RIVET HOLES (16OFF). FOUND DURINGINSPECTION IAW SB A320-53-1031.

## Service documents this report cites (1) (OpenAirDocs)

Manufacturers' service documents named in its text, read by OpenAirDocs, so check each against the text.

- [Airbus SB A320-53-1031](https://openairdocs.org/service-documents/airbus/a320-53-1031.md). Cited as "SB A320-53-1031". OpenAirDocs has a copy of revision 02

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