# SDR 2008UALA06405

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 6, 2008
- Submitted: November 13, 2008
- Operation: Air carrier
- Aircraft: [N426UA](https://openairdocs.org/aircraft/N426UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 510
- Aircraft time: 48,145 hours, 17,338 cycles
- Engine: Iae V2527A5
- System (JASC): [5313 · Fuselage Main, Longeron/Stringer](https://openairdocs.org/jasc/5313)
- Part: Stringer
- Condition: Damaged
- 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/2008UALA06405

## Discrepancy

DAMAGE FOUND AT FRAME 69 STRINGER 20 DIMENSION ARE D=.030 A=.500 B=.311 OF STRINGER 20.  CREASE IS ON STRINGER.  SIZE OF DENT IS 2 INCH BY 2 INCH BY .030 DEEP.  THIS IS AFT OF DOOR 2LT.  *S/D*  MAJOR REPAIR ACCOMPLISHED.  REPLACED STRINGER 20 NEAR FRAME 69.  ACP HFEC INSP OF SKIN AND FASTENER HOLES AFTER OLD STRINGER WAS REMOVED.  NO CRACKS FOUND.

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