# STC SA00166BO

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Avidyne Corporation, United States
- Description: Installation of Avidyne Corporation primary flight display, p/n 700-00006-000, and Magnetometer/OAT sensor, p/n 700-00011-000.
- Applied: April 18, 2001
- Status date: February 21, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)
- Certificate PDF: https://openairdocs.org/files/sha256/40/e3/40e3de09629540e4da3620133bff53c1843cb87e3f39fdbaba1c67479b9f3d05
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EA3E98C38DB728AB86256CE2005125D5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00166BO

## ADs that name it (0)

None.

## Approved models (1)

- Cirrus Design Corporation SR22 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- February 21, 2003: Issued, Current. [certificate](https://openairdocs.org/files/sha256/40/e3/40e3de09629540e4da3620133bff53c1843cb87e3f39fdbaba1c67479b9f3d05)

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