# STC SA03749NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Aerocorp Avionic Solutions Inc., Canada - Description: Installation of Garmin G950 Integrated Flight Deck System - Applied: October 14, 2015 - Status date: March 24, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Foreign approvals: TCCA SA15-76 @ Issue 4 - Data sheets: [TCDS A9EA](https://openairdocs.org/tcds/A9EA) - Certificate PDF: https://openairdocs.org/files/sha256/e1/19/e119089329569f25b1f16d12da1e5bc189e63068e4ae3f0735d5094ec25d4c1f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115277952320260325153813.0001 - DRS record last changed: March 25, 2026 - Page: https://openairdocs.org/stc/SA03749NY ## ADs that name it (0) None. ## Approved models (4) - De Havilland Aircraft of Canada Limited DHC-6-100 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - De Havilland Aircraft of Canada Limited DHC-6-200 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - De Havilland Aircraft of Canada Limited DHC-6-300 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - De Havilland Aircraft of Canada Limited DHC-6-400 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) ## 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. IMPORT SA03749NY Aerocorp Avionic Solutions Inc. 125 – 4950 McCall Way NE Calgary, Alberta Canada T2E 2B9 Part 23 Federal Aviation Regulations A9EA De Havilland Aircraft of Canada Limited DHC-6-100, DHC-6-200, DHC-6-300, DHC-6-400 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission. (See Continuation Sheet 3) 10/14/2015 05/03/2017 04/24/2018 09/24/2018 04/07/2025 ✔ John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4 Installation of Garmin G950/1000 (NXi) Integrated Flight Deck System Configuration 1: G950 Legacy System (Series 100/200/300) Installation of the Garmin G950 Legacy Integrated Flight Deck System must be done in accordance with Transport Canada Civil Aviation (TCCA) approved Genesys Engineering Order A029430 Issue L, dated 19 January 2024, or later TCCA approved revision. 03/24/2026 Description of Type Design Change (continued): Configuration 2: G950 NXi System (Series 100/200/300) Installation of the Garmin G950 NXi Integrated Flight Deck System must be done in accordance with TCCA approved Genesys Engineering Order A029431 Issue I, dated 19 January 2024, or later TCCA approved revision. Configuration 3: G950/1000 NXi System (Series 400) Installation of the Garmin G950/1000 NXi Integrated Flight Deck System must be done in accordance with TCCA approved Genesys Engineering Order A179430 Issue B, dated 6 June 2024, or later TCCA approved revision. All Configurations: 3. Operation of the Garmin G950 Legacy or G950/1000 Legacy or NXi Integrated Flight Deck System must be in accordance with: Series 100/200: TCCA approved Genesys Airplane Flight Manual Supplement A029602, Issue H, dated 22 January 2019, or later TCCA approved revision. Series 300: TCCA approved Genesys Airplane Flight Manual Supplement A029601, Issue H, dated 22 January 2019, or later TCCA approved revision. Series 400: TCCA approved Genesys Airplane Flight Manual Supplement A179601, Issue B, dated 6 June 2024, or later TCCA approved revision. 4. Maintenance of the Garmin G950 Legacy or G950/1000 NXi Integrated Flight Deck System must be in accordance with: Series 100/200/300: TCCA accepted Genesys Instructions for Continued Airworthiness A029600 Issue J, dated 19 January 2024, or later TCCA accepted revision. Series 400: TCCA accepted Genesys Instructions for Continued Airworthiness A179600 Issue B, dated 6 June 2024, or later TCCA accepted revision. 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 modification to the Viking Air Limited DHC-6-100, DHC-6-200, DHC-6-300, and DHC-6-400 is as follows: a. The type certification basis for the DeHavilland DHC-6-100, DHC-6-200, DHC-6-300, and DHC-6-400 as shown on the TCDS A9EA for parts not changed or not affected by the change. b. The type certification basis for the DeHavilland DHC-6-100, DHC-6-200, DHC-6-300, and DHC-6-400 as shown on the TCDS A9EA for parts changed or affected by the change with the following requirements: • 14 CFR Part 23 including amendments 23-1 through 23-62 with the follow exceptions: 23.1457 at Amendment 23-35 23.2000, 23.2005, 23.2010, 23.2325(g), 23.2510, 23.2525, 23.2540(b) at Amendment 23-64. Equivalent Level of Safety Finding 14 CFR Part 23.1549(a), (b), and (c) ----------END---------- 4 4 Add Page ## Every issue (5) - March 24, 2026: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e1/19/e119089329569f25b1f16d12da1e5bc189e63068e4ae3f0735d5094ec25d4c1f) - April 7, 2025: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/1d/0e/1d0ebc5102066f26afda489eb51681fe7bf62b0e637ed88bbf5db97761b311ae) - September 24, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/11/3f/113f3b4fbff390de3a74116b995278714dce674fc0d27c6e65c42cdb8c6d3d45) - April 24, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b7/7d/b77da769828c2f4f9c728e8502d397930edf8c0fa992cee81e2367e5ac4a5a6f) - May 3, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/57/c3/57c38d285ceadc4f1509b0d7ddff8c6a1fd99b890ab81633b14b025d12403bca) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.