# STC SH218NW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: American Eurocopter Corporation, United States
- Description: Installation and maintenance of Allison 250-C20 engine equipped with Bendix fuel control system.
- Applied: July 2, 1975
- Status date: June 30, 2003
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H3EU](https://openairdocs.org/tcds/H3EU)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C6B2DE808EBD623C86256DF100702430.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH218NW-D

## ADs that name it (1)

- [AD 2005-10-13](https://openairdocs.org/ad/2005-10-13): Turbine energy absorbing ring · Rolls-Royce 250-B17B, 250-B17C, 250-B17D and 7 more. Effective Jun 22, 2005. Named in the applicability

## Approved models (1)

- Eurocopter Deutschland GmbH BO-105C ([TCDS H3EU](https://openairdocs.org/tcds/H3EU))

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