# STC SA01254WI - Type: Supplemental type certificate - Status: Historical, Amended - Holder: Garmin International Inc - Description: Installation of the Garmin G1000 Integrated Avionics System in the Diamond Aircraft DA 40. Data Required: (1) Garmin Master Drawing List (MDL) 005-C0004-00, Revision F, dated June 22, 2004; and (2) FAA Approved Airplane Flight Manual Supplement (AFMS), Dwg. Number 190-00303-02, Revision 4, dated June 25, 2004; or later FAA Approved Revisions to (1) or (2). - Status date: June 18, 2005 - Data sheets: A47CE - Certificate PDF: https://openairdocs.org/files/sha256/ca/7f/ca7f44501b973aa28014de599a489886ac3667cfd6c06f0abe88c7ec5769c1f9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5CFC4130680A7C57862570820052E68C.0001 - Page: https://openairdocs.org/stc/SA01254WI ## ADs that name it - [AD 2006-23-04](https://openairdocs.org/ad/2006-23-04): Fuel system indicating system · Diamond Aircraft Industries DA 40 and DA 40F with STC SA01254WI or SA01254WI-D. Effective Nov 28, 2006. Named in the applicability ## Approved models (1) - Diamond Aircraft Industries GmbH DA 40 (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. 1200 East 151st Street Olathe, KS 66062 Part 25 of the Federal Aviation Regulations. Original Product--Type Certificate Number : A47CE Make : Diamond Aircraft Industries GmbH Model : DA 40, DA 40F Installation of the Garmin G1000 Integrated Avionics System in the Diamond DA 40, DA 40F aircraft. Data Required: DA 40 (1) Garmin Master Drawing List (MDL) 005-C0004-00, Revision F, dated June 22, 2004; and (2) FAA Approved Flight Manual Supplement (AFMS), Dwg. Number 190-00303-02, Revision 4, dated June 25, 2004 or later FAA approved revisions to (1) or (2). The modified aircraft must be operated in accordance with the applicable Airplane Flight Manual Supplement (AFMS) identified on the Master Drawing List. Compatibility of this design change with previously approved modifications must be determined by the installer. Date of application : March 06, 2003 Date of issuance : June 25, 2004 Date reissued : Date amended : July 18, 2005 Original signed by HEN ( Signature) Harvey E. Nero FAA Program Manager Wichita Aircraft Certification Office (Title) FAA FORM 8110-2-1(10-69) PAGE 4 of 4 PAGES Number SA01254WI Date of Issuance: June 25, 2004 Date Amended: July 18, 2005 Description Of Type Design Change (Continued): DA 40F (1) Garmin Master Drawing List (MDL) 005-C0004-00, Revision P, dated June 01, 2005; and (2) FAA Approved Flight Manual Supplement, (AFMS), Drawing 190-00303-02, Revision 7 dated June 27, 2005 or later FAA approved revisions to (1) or (2). 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. Previous design changes that are necessary to enable the newly altered product to be airworthy or to complete the installation are: DA 40 STC SA01850CH, Installation of a Hartzell HC-C2YR-1BF/F7495S propeller and A-2295(P) spinner. Diamond OAM modification in accordance with Garmin Installation drawing 005-00149-01, Revision 8 dated June 17, 2004, or later FAA approved revision (for the standard range fuel tank). Diamond OAM modifications in accordance with Garmin Installation drawing 005-00304-00, Revision 3 dated March 14, 2005, or later FAA approved revision (for the long range fuel tank). DA 40F Diamond OAM modifications in accordance with Garmin Installation drawing 005-00304-00, Revision 4 dated June 01, 2005, or later FAA approved revision (for the long range fuel tank). FAA FORM 8110-2-1(10-69) PAGE 4 of 4 PAGES Number SA01254WI Date of Issuance: June 25, 2004 Date Amended: July 18, 2005 • Certification Basis: With respect to the modifications of this STC, the applicant has complied with the existing Certification Basis of the DA 40, which is equivalent to 14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through Amendments 23-51, and as amended by the Amendments stated as follows: 14 CFR Part Amendment 14 CFR Part Amendment §23.301(a)(b)(c) 23-48 §23.1301 23-20 §23.303 - §23.1303(a)(b)(c)(f) 23-49 §23.305 23-45 §23.1305 23-52 §23.307(a) - §23.1307 23-49 § 23.561(a)(b)(3) 23-48 §23.1309 23-49 § 23.562(c)(5) 23-50 §23.1311 23-49 §23.1525 23-45 §23.1321(a)(c)(d)(e) 23-49 §23.601 - §23.1322 23-43 §23.603 23-23 §23.1323 23-49 §23.605(a) 23-23 §23.1325 23-50 §23.607(a)(b) 23-48 §23.1326 23-49 §23.609(a) - §23.1327 23-20 §23.611 23-48 §23.1329(h) 23-49 §23.613(a)(b)(2)(d) 23-45 §23.1331 23-43 §23.619 23-7 §23.1337 23-51 §23.625(a)(b)(c) 23-7 §23.1351 23-51 §23.771(a) 23-14 §23.1353 23-49 §23.773(a)(2) 23-45 §23.1357(a-d) 23-43 §23.777(a)(b) 23-51 §23.1359(c) 23-49 §23.853(a) 23-49 §23.1183 23-51 §23.867 23-49 §23.1365(a)(b)(d)(e) 23-49 §23.901(b)(2)(e)(1) 23-51 §23.1381(a)(b) - §23.954 23-51 §23.1431(a)(b)(e) 23-49 §23.963(e) 23-51 §23.1547 23-20 §23.993(a)(d) 23-43 §23.1549 23-45 §23.1529 23-26 §23.1553,55 23-50 §23.1541(a)(b) 23-21 §23.1557 23-43 §23.1543,45 23-50 §23.1559-67 23-50 An Equivalent Level Of Safety (ELOS) has been found for 14 CFR 23.1337(b); Reference ACE-03-01 --END-- ## Every issue (2) - June 18, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ca/7f/ca7f44501b973aa28014de599a489886ac3667cfd6c06f0abe88c7ec5769c1f9) - June 25, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/af/34/af34927a4d5c40b8a2d72daab1a958719af5895c6a88c7bcaf42f56d7c062d1b) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.