# SDR 2A6R2026031675201

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 16, 2026
- Submitted: April 6, 2026
- Operation: Air carrier
- Filed by: [Air Methods, LLC, repair station 2A6R933B](https://openairdocs.org/faa-repair-station/2A6R933B/air-methods-llc.md) (OpenAirDocs)
- Aircraft: [N813AM](https://openairdocs.org/aircraft/N813AM), registered now
- Make and model: Urocop EC 130 T2
- Registry model: [Urocop EC 130 T2](https://openairdocs.org/model/eurocopter-ec-130-t2) (OpenAirDocs)
- Aircraft serial: 7735
- Aircraft time: 2,944 hours, 10,587 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Support Frame
- Part number: 350A21491322
- Condition: Damaged
- Location: Zone 100
- Part time: 2,944 hours, 10,587 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/2A6R2026031675201

## Discrepancy

DAMAGE TO THE LEFT EDGE FRAME  AND RT EDGE FRAME, IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. A DETAILED DESCRIPTION OF THE APPROVED REPAIR/INSTALLATION PROCEDURES IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2024-0040, ISSUE A DATED 09 JAN 2024, AND AC 43.13-1B CHAPTER 4, SECTION 4, PARAGRAPH 4-57 CHANGE 1 DATED 9/8/98.

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