# SDR 03FDEA02044

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 4, 2003
- Submitted: December 4, 2003
- Operation: Air carrier
- Aircraft: [N430FE](https://openairdocs.org/aircraft/N430FE), registered now
- Make and model: Airbus A310
- Registry model: [Airbus A310](https://openairdocs.org/model/airbus-a310) (OpenAirDocs)
- Aircraft serial: 394
- Aircraft time: 38,474 hours, 18,035 cycles
- System (JASC): [5753 · Trailing Edge Flaps](https://openairdocs.org/jasc/5753)
- Part: Flap Track
- Condition: Cracked
- Location: Zone 500
- 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/03FDEA02044

## Discrepancy

LT WING TE,  MIDPOINT BETWEEN NR 1 O/B PYLON AND I/B NR 3 FLAP TRACK EVIDENCE OF CRACK AT RIVET HEAD TO EDGE LWR SKIN.  REQUEST NDT TO CONFIRM.  REMOVED FASTENER IAW A310 SRM 51-40-21, ROTO TESTED HOLE IAW NTM 51-10-00-01 NO CRACKS FOUND, FABRICATED REPAIR PARTS IAW EA6-5710-73485A DWG R57249152.  INSTALLED REPAIR PARTS IAW EA6-5710-73485A  DWGR 57249152.  DOME SEALED FASTENER IAW A310 SRM 51-76-20, LEAK CHECK IAW AMM A310-28-11-00-5.

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