# STC SA2105SW-AC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Federal Aviation Administration, United States
- Description: Installation of Total Temperature Sensor, Static Defect Corrector, and Omega Nav System with interface into Pilot Flight Director System.
- Applied: August 26, 1982
- Status date: October 4, 1982
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 6A6](https://openairdocs.org/tcds/6A6)
- Certificate PDF: https://openairdocs.org/files/sha256/73/db/73dbfbcc8101f178bffbed34f11f17867a26cc90c2402e80380ac433ed5c8144
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/04188E0A873F15FA862576870056FBFB.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2105SW-AC

## ADs that name it (0)

None.

## Approved models (1)

- Kelowna Flightcraft R & D Ltd. 440 ([TCDS 6A6](https://openairdocs.org/tcds/6A6))

## What the certificate says

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

## Every issue (1)

- October 4, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/73/db/73dbfbcc8101f178bffbed34f11f17867a26cc90c2402e80380ac433ed5c8144)

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