# SDR AU980954

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 8, 1998
- Submitted: March 26, 2000
- Operation: General aviation
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Bs 43
- Stage of operation: IN
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AU980954

## Discrepancy

(AUS) FUSELAGE FRAME 43 AT STN 1023 CONTAINED CRACKS IN THE FASTENER HOLES OF THE FLOORBEAM FLANGES Y-765RH AND Y-1292RH.  FOUND DURING EDDY CURRENT INSPECTION IAW SB A320-53-10-08.

## 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 A320-53-10-08](https://openairdocs.org/service-documents/airbus/a320-53-10-08.md). Cited as "SB A320-53-10-08"

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