# STC SR02080SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Garmin International Inc, United States
- Description: Installation of Garmin Model 400W/500W Series Navigators including Helicopter Terrain Awareness and Warning System (HTAWS) functionality.
- Applied: March 31, 2010
- Status date: June 19, 2015
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/84/10/8410b6d0bed1e498a97d040f2adfe58a9dac757176b70555dcbb243bdf52aabc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33546579EB5DF57486257E700053734A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02080SE

## ADs that name it (0)

None.

## Approved models (6)

- Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

This certificate issued to Garmin International, Inc.

1200 East 151st Street Olathe, KS 66062

Part 27 of the Federal Aviation Regulations.

Original Product--Type Certificate Number: H2SW Make: Bell Model: 206B, 206L, 206L-1, 206L-3, 206L-4, 407

Description of Type Design Change: Installation of Garmin Model 400W/500W Series Navigators including Helicopter Terrain Awareness and Warning System (HTAWS) functionality in accordance with Garmin Master Drawing List (MDL), 005-00610-02, Rev. 2, dated June 18, 2015, or later FAA approved revision. The Master Drawing List establishes the approved configuration for each model listed above. The applicable FAA approved Rotorcraft Flight Manual Supplements and Instructions for Continued Airworthiness are identified in the Master Drawing List by model.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only.

This approval should not be extended to other rotorcraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft.

A copy of: 1) this certificate; 2) the applicable RFMS as listed in the FAA approved MDL; 3) the applicable Instructions for Airworthiness as listed in the FAA approved MDL, must be maintained as part of the permanent records for the modified rotorcraft.

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.

(See Continuation Sheet on Page 3)

Date of application: March 31, 2010 Date reissued:

Date of issuance: August 30, 2010 Date amended: June 19, 2015

(Signature) Michael Warren, ODA STC Unit Administrator ODA-240087-CE, Garmin International, Inc.

(Title)

Transfer the ownership of Supplement Type Certificate Number

To (Name of Transferee)

(Address of Transferee) (Number and street)

(City, State and Zip code)

From (Name of Grantor) (Print or type)

(Address of Grantor) (Number and street)

(City, State and Zip code)

Signature of Grantor (In Ink):

Number SR02080SE Issued: August 30, 2010 Reissued:

Amended: June 19, 2015

Rotorcraft modified in accordance of this STC must be operated in accordance with the applicable RFMS; and must be maintained in accordance with the applicable Instructions for Continued Airworthiness, as listed in FAA approved MDL for this STC.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change are shown on Type Certificate Data Sheet H2SW for each model.

b. The certification basis for parts changed or affected by this change is:

Regulations at the latest amendment: Original through 27-43 Section Amdt Section Amdt

27.251 Original 27.1316 (a) 27-46

27.301 All Original 27.1317 (c) 27-42

27.303 Original 27.1321 (a)(c)(d) 27-13

27.305 All Original 27.1322 All 27-11

27.307 (a) 27-26 27.1351 (a) 27-13

27.337 All 27-26 27.1357 (a)(b)(d) 27-13

27.561 (a)(b)(3) 27-32 27.1365 All 27-35

27.601 All Original 27.1367 All Original

27.603 All 27-16 27.1381 All Original

27.605 (a) 27-16 27.1501 All 27-14

27.609 All Original 27.1523 All Original

27.610 All 27-37 27.1525 27-21

27.611 (a)(b) Original 27.1529 27-18

27.613 All 27-26 27.1541 All Original

27.771 (a) Original 27.1555 (a) 27-21

27.773 All Original 27.1559 27-21

27.777 All Original 27.1581 (a)(b)(d) 27-14

27.1301 All Original 27.1583 (e) 27-16

27.1307 (e) Original 27.1585 (a) 27-21

27.1309 (a)(c) 27-46 ------ ------

Note (1) Amendment 27-46 was used for regulations 14 CFR 27.1309 and 27.1316.

------------------------------------------------END------------------------------------------------

## Every issue (2)

- June 19, 2015: Amended, Current. [certificate](https://openairdocs.org/files/sha256/84/10/8410b6d0bed1e498a97d040f2adfe58a9dac757176b70555dcbb243bdf52aabc)
- September 23, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e5/4b/e54bbcb076e29104092b654aa0338076e6a2c6b1bb0c36077a1f8a4667a28f4f)

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