# STC SA01670SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Garmin AT Inc., United States
- Description: Installation of a GWX 68 Weather Radar
- Applied: March 3, 2005
- Status date: May 10, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20)
- Certificate PDF: https://openairdocs.org/files/sha256/71/01/7101e7706540d19c06d38b00567d373294480fabe55073ad161301c1ada04b25
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A12B578572A56FE86257178005179A0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01670SE

## ADs that name it (0)

None.

## Approved models (8)

- Raytheon Aircraft Company 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company 65-B80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company A65 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Raytheon Aircraft Company E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SA01670SE

This certificate, issued to: Garmin AT, Inc.

2345 Turner Road SE Salem, OR 97302

Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: TCDS 3A20 Make: Raytheon Aircraft Company Mo del: 65-B80, A65, 70, 65-90, 65-A90, B90, C90, C90A, C90GT, E90

Description of the Type Design Change: Installation of a GWX 68 Weather Radar in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0171-00, Revision B, dated March 17, 2006, or later FAA approved revision.

Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: March 3, 2005 Date reissued:

Date of issuance: May 10, 2006 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- May 10, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/71/01/7101e7706540d19c06d38b00567d373294480fabe55073ad161301c1ada04b25)

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