# STC SA02017SE-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Garmin International Inc, United States - Description: Installation of a Garmin G600 Flight Display System, GNS430W GPS/NAV/COM, and GMA 347 Audio Panel - Applied: May 19, 2009 - Status date: June 9, 2014 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) - Certificate PDF: https://openairdocs.org/files/sha256/45/a5/45a5d606f17dc589ac297a9ca5fa7125cd26c3325f6539747ca80c58fddeb8b1 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/798DCA8C5C0ABE2F86257CF2006B6674.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02017SE-D ## ADs that name it (0) None. ## Approved models (2) - Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - Cessna Aircraft Company 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) ## 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 SA02017SE-D This certificate, issued to Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: TCDS A37CE Make: Cessna Aircraft Company Model: 208, 208B Description of the Type Design Change: Installation of a Garmin G600 Flight Display System, GNS 430W GPS/NAV/COM, and GMA 347 Audio Panel in accordance with Garmin Master Drawing List, G600 GNS 430W GMA 347 Cessna 208/208B, 005-00559-00, Rev. 10, dated 6-June-2014, or later Federal Aviation Administration (FAA) approved revision. Maintenance instructions are provided in the Instructions for Continued Airworthiness G600, GNS 530W, GNS 430W, GMA 347, GTX 330D, GMX 200, WSI AV-200 Cessna 208/208B, 190-01080-05, Rev. 2, signed 6-June-2014, or later FAA approved revision. Operating information is provided in the Garmin Airplane Flight Manual Supplement Garmin G600, GNS 530W, GNS 430W, GMA 347, GTX 330D Cessna 208/208B, 190-01080-06, Rev. D, signed 6-June-2014, or later FAA approved revision. 1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. Installation of the following STCs: STC SA01712SE, SA01512WI-D, and SA00171BO are prior requirements. 3. Aircraft equipped with Garmin G1000 Integrated Cockpit System are not eligible for this STC. (See Continuation Sheet on Page 3) Date of application: May 19, 2009 Date reissued: January 5, 2011 Date of issuance: January 26, 2010 Date amended: June 9, 2014 (Signature) Michael Warren, ODA STC Unit Administrator ODA-240087-CE, Garmin International, Inc. (Title) Transfer the ownership of Supplemental 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): PAGE 2 OF 3 PAGES U.S. GPO: 1987-763-289 Number SA02017SE-D Company Name Here Issued: January 26, 2010 Reissued: January 5, 2011 Amended: June 9, 2014 4. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. 5. 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 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: The certification basis for parts changed or affected by this change is: Section Amdt Section Amdt Section Amdt 23.251 23-45 23.1301 23-20 23.1359(a)(c) 23-49 23.301(a) 23-48 23.1303(a)(b)(c)(d) 23-49 23.1365(a)(b)(d)(e) 23-49 23.303 Orig 23.1309(a)(1)(2) 23-49 23.1367 Orig 23.305(a)(b) 23-45 23.1309(b) 23-49 23.1381(a)(b) Orig 23.307(a) Orig 23.1309(c)(d) 23-49 23.1431(a)(b)(d)(e) 23-49 23.337(a)(b) 23-48 23.1309(e) 23-49 23.1501 23-21 23.561(e) 23-48 23.1311 23-49 23.1523 23-34 23.601 Orig 23.1321(a)(c)(d)(e) 23-49 23.1525 23-45 23.603(a)(b) 23-23 23.1322 23-43 23.1529 23-26 23.605(a) 23-23 23.1323(a) 23-49 23.1541(a)(b) 23-21 23.607(a)(b) 23-48 23.1325(b)(1)(2)(i) 23-50 23.1543(b)(c) 23-50 23.609 Orig 23.1327(a) 23-20 23.1545(a)(b) 23-50 23.611 23-48 23.1329(h) 23-49 23.1555(a) 23-50 23.613(a)(b)(c) 23-45 23.1331(a)(b)(1) 23-43 23.1581(a)(b)(c)(f) 23-50 23.771(a) 23-14 23.1335 23-20 23.1583(h)(m) 23-50 23.773(a)(2) 23-45 23.1351(a)(1)(2)(i) 23-49 23.1585(j) 23-50 23.777(a)(b) 23-51 23.1353(h) 23-49 23.867(a)(b)(c) 23-49 23.1357(a)(b)(c)(d) 23-43 - END - **FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES** ## Every issue (2) - June 9, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/45/a5/45a5d606f17dc589ac297a9ca5fa7125cd26c3325f6539747ca80c58fddeb8b1) - January 5, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/5a/1e/5a1e9bfe6c200743320e84a40f230ffbe5be3e1db2591701dde0a7c7c4257dad) --- 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.