# STC SA01389WI - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Diamond Aircraft Industries Inc., Canada - Description: Installation of Garmin GFC 700 Automatic Flight Control System. - Applied: June 8, 2006 - Status date: December 18, 2017 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A47CE](https://openairdocs.org/tcds/A47CE) - Certificate PDF: https://openairdocs.org/files/sha256/f7/ea/f7eadb5024a14891eae663216d66abfa10b4cfa7017d387f0f9233427f28b051 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B9B7B623EF709EF3862582110062A1EF.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01389WI ## ADs that name it (0) None. ## Approved models (2) - Diamond Aircraft Industries GmbH DA 40 ([TCDS A47CE](https://openairdocs.org/tcds/A47CE)) - Diamond Aircraft Industries GmbH DA 40F ([TCDS A47CE](https://openairdocs.org/tcds/A47CE)) ## 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. 1560 Crumlin Sideroad London, Ontario N5V 1S2 23* Federal Aviation A47CE Diamond DA40, DA40F Installation of the Garmin GFC 700 Automatic Flight Control System in the Diamond DA 40, DA40F aircraft. Data required: (1) Garmin Master Drawing List (MDL) 005-00336-01, Revision B, dated June 8, 2006, and (2) FAA Approved Flight Manual Supplement (AFMS), Document No. 190-00492-00, Revision 2, dated June 8, 2006 or later Transport Canada approved revisions to (1) or (2) 1. DA 40 and DA 40F aircraft equipped with a G1000 Integrated Avionics system per STC #SA01254WI and Diamond Aircraft Optional Aircraft Modification (OAM) 40-226 are eligible for this STC. 2. The modified aircraft must be operated in accordance with the applicable AFMS identified on the MDL. 3. The modified aircraft must be operated in accordance with the applicable Instructions for Continued Airworthiness (ICA) identified on the MDL. 4. Compatibility of this design change with previously approved modifications must be determined by the installer. 5. If the holder agrees to permit another person to use this certificate to alter the p roduct, the holder shall give the other person written evidence of that permission. September 28, 2005 June 8, 2006 December 18, 2017 _Original signed by Ben Tyson (Signature) Ben Tyson Program Manager Wichita ACO Branch (Title) FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES Transfer the ownership of Supplement Type Certificate Number To From Signature of grantor Date Issued: June 8, 2006 Date Reissued: December 18, 2017 *Certification Basis: With respect to the modifications of this STC, the applicant has complied with th e following Certification Basis: a. The type certification basis for Diamond DA 40 and DA 40F airplanes is shown on the TCDS A47CE parts not changed or not affected by this change. b. The certification basis for parts changed or affected by this change since the reference date of application, September 28, 2005 , is based upon Part 23 as amended by Amendment 23-55. The certification basis for this modification was determined to be: 14 CFR Part Amendment 14 CFR Part Amendment 23.1 23-34 23.867(a)(b) 23-49 23.29(a)(b) 23-21 23.1301(a)(b)(c)(d) 23-20 23.143(a)(b)(c) 23-50 23.1309(a)(b)(c)(d)(e)(f) 23-49 23.301(a) 23-48 23.1311(a)(b)(c) 23-49 23.303 - 23.1321(a)(c)(e) 23-49 23.305(a)(b) 23-45 23.1322(a)(b)(c)(d)(e) 23-43 23.307(a) - 23.1327(a)(b) 23-20 23.395(a)(1) 23-7 23.1329(a)(b)(c)(d) (e)(f)(g)(h) 23-49 23.397(a)(b) 23-45 23.1335 23-20 23.561(a)(b) 23-48 23.1351(a)(g) 23-49 23.601 - 23.1353(h) 23-49 23.603(a)(b) 23-23 23.1357(a)(b)(c)(d) 23-43 23.605 23-23 23.1359(a)(b)(c) 23-49 23.607 - 23.1365(a)(b)(d)(e) 23-49 23.609(a)(b) - 23.1367(a)(b)(c)(d) - 23.611 - 23.1381(a)(b) - 23.613(a)(b)(c) 23-45 23.1431(a)(b)(e) 23-49 23.625(a) 23-7 23.1525 23-45 23.671(a) - 23.1529 23-26 23.677(a)(d) 23-49 23.1541(b)(1) 23-21 23.685(a)(b)(c)(d) 23-17 23.1555(a)(b) 23-50 23.689(a)(1)(2)(2) (b)(c)(d)(e)(f) 23-7 23.1581(a) (b)(2)(c)(d)(f) 23-50 23.771(a) 23-14 23.1583(h)(m) 23-50 23.777(a)(b) 23-51 23.1585(j) 23-50 23.779(a) 23-51 - - An Equivalent Level of Safety (ELOS) has been found for 14 CFR 23.1337(b); Reference ACE-03-01 ------------------------------------------------END------------------------------------------------ ## Every issue (2) - December 18, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f7/ea/f7eadb5024a14891eae663216d66abfa10b4cfa7017d387f0f9233427f28b051) - June 8, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ab/46/ab4614f3a87dfc3df5f1d56736199713c49f41938a46567643414cff21ae5176) --- 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.