# SDR 2A6D20230427001

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 27, 2023
- Submitted: April 27, 2023
- Operation: General aviation
- Filed by: [Air Methods LLC, repair station 2A6D933B](https://openairdocs.org/faa-repair-station/2A6D933B/air-methods-llc.md) (OpenAirDocs)
- Aircraft: [N259AM](https://openairdocs.org/aircraft/N259AM), registered now
- Make and model: Urocop EC 130 B4
- Registry model: [Urocop EC 130 B4](https://openairdocs.org/model/eurocopter-ec-130-b4) (OpenAirDocs)
- Aircraft serial: 7050
- Aircraft time: 4,577 hours, 15,247 cycles
- System (JASC): [5300 · Fuselage Structure (General)](https://openairdocs.org/jasc/5300)
- Part: Mount
- Part number: 350A21467420
- Part serial: 15247
- Condition: Unknown
- Location: Zone 100
- Part time: 4,577 hours, 15,247 cycles
- 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/2A6D20230427001

## Discrepancy

DAMAGE TO THE AFT LANDING GEAR FITTING (P/N: 350A21-4674.20) IN THE FORM OF A GOUGE /
CHAFE. THE DAMAGE IS AT THE TWO HOLES OF THE TWIN CLEVIS, AND WAS MEASURED TO BE APPROXIMATELY 10.381MM
(0.409”). THE BOLT HOLE IS ORIGINALLY 10JS13 MM (10.0MM (+/- 0.11)) DIAMETER (0.394” (+/-0.004”)).

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