# STC SA01444WI-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Diamond Aircraft Industries, Inc, Canada - Description: Upgrade of G1000 and GFC 700 AFCS software and installation of optional hardware upgrades including WAAS capability, optional Envelope Stability & Protection (ESP), and optional Synthetic Vision System (SVS). - Applied: September 28, 2006 - Status date: January 12, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A47CE](https://openairdocs.org/tcds/A47CE) - Certificate PDF: https://openairdocs.org/files/sha256/45/30/45308cfbbee0dd1a6470b0cf189bb5e5bceb2065b2ca6a036f65e0c03537d1cf - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9C219E57B7E9F87F862582190047E91F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01444WI-D ## 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. FAA FORM 8110-2(10-68) PAGE 1 of 4 PAGES IMPORT SA01444WI-D Diamond Aircraft Industries, Inc 1560 Crumlin Side Road London, Ontario N5V 1S2 23* Federal Aviation A47CE Diamond DA 40, DA 40F Upgrade of G1000 and GFC 700 AFCS software and installation of optional hardware upgrades including WAAS capability, optional Envelope Stability & Protection (ESP), and optional Synthetic Vision System (SVS). Data Required: (1) Garmin Master Drawing List (MDL) 005-00400-01, Revision 1, dated July 26, 2007 or later TCAA approved revision. (2) Garmin G1000/GFC700 Airplane Flight Manual Supplement (AFMS), 190-00492-10, Revision 1, dated July 26, 2007, or Garmin G1000 AFMS, 190-00492-11, Revision 1, dated July 26, 2007, or G1000/KAP140 AFMS, 190-00492-12, Revision 1, dated February 28, 2008 or later TCAA approved revisions, as required by the MDL. (3) If the optional SVS is enabled, the following are required: a. Garmin MDL 005-00400-01, Revision 10, or later TCAA approved revision. b. Garmin G1000 Synthetic Vision and Pathways Option AFMS, 190-0492-08, Revision 1, or later FAA-approved revision. (4) If the optional ESP is enabled, the following are required: a. Garmin MDL 005-00400-01, Revision 10, or later TCAA approved revision. b. Garmin G1000 Electronic Stability and Protection (ESP) Option AFMS, 190-00492-09, Revision 1, or later TCAA approved revision. Sept. 28, 2006 July 26, 2007 April 30, 2014, September 2, 2016 February 28, 2008; May 16, 2013, January 12, 2018 __Original signed by Ben Tyson (Signature) Ben Tyson Program Manager Wichita ACO Branch (Title) Transfer the ownership of Supplement Type Certificate Number To From Signature of grantor FAA FORM 8110-2(10-68) PAGE 3 of 4 PAGES IMPORT SA01444WI-D Date Amended: February 28, 2008, May 16, 2013 Date Reissued: April 30, 2014, September 2, 2016, January 12, 2018 1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. The modified aircraft must be operated in accordance with the applicable AFMS identified on the MDL, appropriate to the configuration installed on the aircraft. 3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other p erson written evidence of that permission. 4. Installation of STC #SA01254WI-D is a prior or concurrent requirement for all MDL Configurations. 5. Installation of STC #SA01389WI is a prior or concurrent requirement for the -1 and -2 MDL Configurations. 6. Aircraft equipped with the Honeywell KAP 140 autopilot are only eligible for the -5 and -6 MDL Configurations. 7. Installation of the -3 and -4 MDL Configurations is permitted only on aircraft with no autopilot installed. 8. Aircraft modified by this STC shall be maintained in accordance with the Instructions for Continued Airworthiness defined by the MDL. FAA FORM 8110-2-1(10-69) PAGE 4 of 4 PAGES IMPORT SA01444WI-D Date Amended: February 28, 2008; May 16, 2013 Date Reissued: April 30, 2014, September 2, 2016, January 12, 2018 *Certification Basis Based on 14 CFR ยงยง 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 is shown on the TCDS A47CE. b. The certification basis for parts changed or affected by this change since the date of application is determined to be: Section Amdt. Section Amdt. 23.21(a)(b) Orig. 23.23(b)(3) 23-45 23.29 23-21 23.1321(a)(c)(d)(e) 23-49 23.143(a)(b)(c) 23-50 23.1322 23-43 23.301(a)(b)(c) 23-48 23.1323(a) 23-49 23.303 Orig. 23.1327(a) 23-20 23.305 23-45 23.1329(a)(b)(d)(e)(f)(g) 23-49 23.307 Orig. 23.1335 23-20 23.397(a)(b) 23-45 23.1337(b)(1) 23-51 23.561(e) 23-48 23.1351(a)(g) 23-49 23.601 Orig. 23.1353(h) 23-49 23.603 23-23 23.1357(a)(1)(2)(b) (c)(1)(2)(d) 23-43 23.605(a) 23-23 23.1359(a)(b)(c) 23-49 23.607(a)(b)(c) 23-48 23.1365(a)(b)(d)(e) 23-49 23.609(a) Orig. 23.1367(c)(d) Orig. 23.611 23-48 23.1381(a)(b) Orig. 23.613(a)(b)(2)(d) 23-45 23.1431(a)(b)(e) 23-49 23.671(a)(b) Orig. 23.1501(a)(b) 23-21 23.677(a)(d) 23-49 23.1525 23-45 23.685(a)(d) 23-17 23.1529 23-26 23.689(b)(e) 23-7 23.1541(a)(1)(2)(b)(1)(2)(c)(2) 23-21 23.771(a) 23-14 23.1543(b)(c) 23-50 23.777(a)(b) 23-51 23.1545(a)(b)(1)(2)(3)(4) 23-50 23.867(a)(b)(c) 23-49 23.1549(a)(b)(c) 23-45 23.1301 23-20 23.1553 23-50 23.1303(a)(b) 23-49 23.1555(a)(b) 23-50 23.1305(a)(1)(2)(3)(b)(2)(3)(4)(i)(5) 23-52 23.1581(a)(b)(2)(3)(c)(d)(f) 23-50 23.1309(a)(1)(2)(b)(c)(d)(e) 23-49 23.1583(h)(m)(n) 23-50 23.1311(a)(1)(2)(3)(4)(7)(b) 23-49 23.1585(a)(1)(j) 23-50 23-139-SC Orig. Regulations at an intermediate amendment: None Regulations at the amendment level shown on TCDS: None ---------- END ---------- ## Every issue (5) - January 12, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/45/30/45308cfbbee0dd1a6470b0cf189bb5e5bceb2065b2ca6a036f65e0c03537d1cf) - April 30, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/18/86/1886087385fc61b1f9ba598d1c14030314988520ba3d0c988489cbf7601c9e77) - May 16, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/03/11/03112ffb9e72008a17eb45e4f1615735163c32e1c27dfef7c216819d94d1c6a5) - February 28, 2008: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/09/64/096468ce481d580f30a5dad19f3d090393f3abf9f890875b5582405dac7029dc) - July 26, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/9d/8f/9d8fa75f9f7b813efbed1398c486ab2f4778f4f1b0d73e8eb502fd9df4cb302f) --- 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.