# STC SH7406SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: American Eurocopter Corporation, United States
- Description: To move the height-velocity diagram from the limitation section of the RFM to the Performance Section.
- Applied: April 1, 1987
- Status date: June 30, 2003
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H10EU](https://openairdocs.org/tcds/H10EU)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E4A68CA03D5CB23286256DF3005C9A42.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH7406SW-D

## ADs that name it (0)

None.

## Approved models (3)

- Eurocopter France AS-365N2 ([TCDS H10EU](https://openairdocs.org/tcds/H10EU))
- Eurocopter France SA-365N ([TCDS H10EU](https://openairdocs.org/tcds/H10EU))
- Eurocopter France SA-365N1 ([TCDS H10EU](https://openairdocs.org/tcds/H10EU))

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.