# STC SR02206AK

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Garmin AT Inc., United States
- Description: Installation of Garmin AT, MX20 Multi-Function Display (MFD).
- Applied: May 8, 2003
- Status date: January 9, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW), [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/98/63/986368f0d415dae4f91480b49f02816deedf256c7b9d9f489c7edf3a9853e8e6
- Approved model list and other attachments: [SR02206AK certificate amend 1.pdf](https://openairdocs.org/files/sha256/86/75/8675e4011d3b3b96f6fabd76d724bf578245de9540251163ce3c28f48ac8e783)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BD95012E6C905F27862573D8006AE220.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02206AK

## ADs that name it (0)

None.

## Approved models (15)

- Bell Helicopter Textron (Canada) 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France EC 130 B4 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))

## 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.

United States Of America Department of Transportation - Federal Aviation Administration Garmin AT, Inc. Approved Model List (AML) 2345 Turner Road SE Number SR02206AK Salem, Oregon 97302 Date of Issuance: 26 May 2005 Date Amended: 08 February 2005 09 January 2008

Approved Model List For: Garmin AT MX20 MFD

Original Product Make Original Product Model Original Product Type Certificate No.

Certification basis of Supplemental Type Certificate Bell Helicopter Textron 206A; 206A-1; 206B; 206L;

206L-1; 206L-3; 206L-4 H2SW 14 CFR Part 27 Amendments 27-1 thru 27-40 1 Eurocopter France AS350C, AS350D, AS350D1, AS350B, AS350B1, AS350B2, AS350BA, AS350B3, EC130B4 H9EU 14 CFR Part 27 Amendments 27-1 thru 27-40

NOTES:

1. Except 27.561 at amendment 27-24

FAA APPROVED:

Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska Page 1 of 1

### SR02206AK certificate amend 1.pdf

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 3 This certificate may be transferred in accordance with FAR 21.47.

Number SR02206AK This Certificate issued to Garmin AT, Inc.

2345 Turner Road SE Salem, Oregon 97302

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Regulations.

Original Product Type Certificate Number:

Make:

Model:

* See attached FAA Approved Model List (AML) No. SR02206AK, dated 09 January 2008, for a list of approved aircraft models and applicable airworthiness regulations.

Description of Type Design Change:

Installation of Garmin AT, MX20 Multi-Function Display (MFD) in accordance with Garmin AT MX20 Helicopter STC Master Data List, P/N 560-1051-01, Revision B, dated 14 August 2006, or later FAA approved revision.

Limitations and Conditions:

1. Installer must determine compatibility of this design change with previously approved modifications.

2. 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.

3. Rotorcraft Flight Manual Supplement, P/N 560-1052-01, Revision D, FAA approved on 28 December 2007, or later FAA approved revision is a required part of this installation.

4. Rotorcraft Instructions for Continued Airworthiness, Document No. 560-1053-01, Revision B, dated 19 July 2006, or later FAA accepted revision is a required part of this installation.

5. On Bell Helicopter Textron Models 206A; 206A-1; 206B; 206L; 206L-1; 206L-3; 206L-4 only. NG Tachometer, Insco P/N 6501-3008, Bell P/N 206-0070-266-9, or FAA approved equivalent is required. Refer to Garmin AT MX20 Helicopter Installation Supplement 560-1054-00 for equivalency criteria.

6. On Bell Helicopter Textron Models 206A; 206A-1; 206B; 206L; 206L-1; 206L-3; 206L-4 only. Engine torque, temperature and NG tachometer must be rotated 90 degrees counter-clockwise as defined in Garmin AT MX20 Helicopter Installation Supplement 560-1054-00.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: 8 May 2003

Date of issuance: 26 May 2005 Date reissued:

Date amended: 09 January 2008

By direction of the Administrator

______________________________________________ ( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office ______________________________________________ ( Title)

## Every issue (1)

- January 9, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/98/63/986368f0d415dae4f91480b49f02816deedf256c7b9d9f489c7edf3a9853e8e6), [SR02206AK certificate amend 1.pdf](https://openairdocs.org/files/sha256/86/75/8675e4011d3b3b96f6fabd76d724bf578245de9540251163ce3c28f48ac8e783)

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