# STC SA01002DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Alaska Central Express Inc, United States - Description: Installation of Garmin G700 TXi display and sensor system - Applied: March 22, 2019 - Status date: July 31, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/f9/eb/f9eb7504ed5cfb144d27d90940883e889b9ba29970c1647d1c03a614abd66c09 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F495D7F72D534609862585A1005BC852.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01002DE ## ADs that name it (0) None. ## Approved models (1) - Textron Aviation Inc. 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder. FAA Form 8110-2 (5/14) Page 1 of This certificate issued to: Part of the Signature Title 3 SA01002DE Alaska Central Express Inc. 5901 Lockheed Ave. Anchorage, AK 99502 Federal Aviation Regulations23 Installation of Garmin G700 TXi display and sensor system in accordance with ACE Document No. CW0602-1032, Master Drawing List (MDL) Beech 1900C Garmin G700 Txi Installation, Revision IR, dated 7/9/2019 FAA Approved 7/30/2019 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. CW0725-1075, Revision A dated 7/28/2019, FAA Accepted 7/29/2019, or later FAA accepted revision are required to be made available at installation. FAA Approved Airplane Flight Manual Supplement, Document No. CW0715-1126, Revision IR dated 4/11/2019, FAA Approved 7/30/2019, or later FAA approved revision is required for this modification. 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 this certificate to alter a product, the holder must give the other person written evidence of that permission. (Certification Basis on page 3 of 3) Kreg R. Voorhies ODA Administrator, Cert Works ODA(AIR)-833887-NM Textron Aviation Inc 1900C March 22, 2019 July 31, 2019 A24CE United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder. FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): 3 SA01002DE The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder. FAA Form 8110-2 (5/14) Page 3 of 3 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 the Textron Aviation Inc 1900C installation of the Garmin G700 TXi display and sensor system is as follows: a. The type certification basis for Textron Aviation Inc 1900C series airplane is shown on TCDS A24CE for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, March 22, 2019, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-63. 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 was determined to be: Regulations at the latest amendment 23-0 through 23-63 14 CFR Sections: 23.301(a) Amdt. 23-48; 23.303 Amdt. - ; 23.305(a) Amdt. 23-45; 23.307(a) Amdt. - ; 23.337(a)(1),(b)(1) Amdt. 23-48; 23.341(c) Amdt. 23-48; 23.561(e) Amdt. 23-62; 23.571(a-c) Amdt. 23-62; 23.601 Amdt. - ; 23.603 Amdt. 23-23; 23.605 Amdt. 23-23; 23.607 Amdt. 23-48; 23.609 Amdt. - ; 23.611 Amdt. 23-48; 23.613 Amdt. 23-45; 23.619 Amdt. 23-7; 23.625(a-c) Amdt. 23-7; 23.771(a) Amdt. 23-14; 23.773(a)(1,2) Amdt. 23-63; 23.777(a,b) Amdt. 23-62; 23.785(i) Amdt. 23-49; 23.853(a) Amdt. 23-62; 23.867 Amdt. 23-49; 23.1301 Amdt. 23-62; 23.1303(a-d,f) Amdt. 23-62; 23.1306 Amdt. 23-61; 23.1307 Amdt. 23-49; 23.1308(a-c) Amdt. 23-57; 23.1309(a,b,c,d) Amdt. 23-62; 23.1310 Amdt. 23-62; 23.1311(a,b) Amdt. 23-62; 23.1321(a,c,d,e) Amdt. 23-49; 23.1322 Amdt. 23-43; 23.1323(c) Amdt. 23-62; 23.1323(a,b) Amdt. 23-62; 23.1325(b) Amdt. 23-50; 23.1327 Amdt. 23-20; 23.1329(h) Amdt. 23-49; 23.1331 Amdt. 23-62; 23.1351(a)(1)(2)(i),(b)(1)(i, ii, iii) Amdt. 23-49; 23.1357(a-d) Amdt. 23-43; 23.1359 Amdt. 23-49; 23.1365(a,b,d, e) Amdt. 23-49; 23.1431(a,b,e) Amdt. 23-62; 23.1501 Amdt. 23-21; 23.1523 Amdt. 23-34; 23.1525 Amdt. 23-45; 23.1529(a,c,d,h) Amdt. 23-26; 23.1541(a,b) Amdt. 23-21; 23.1543 Amdt. 23-50; 23.1545(a)(b)(1-4),(c-d) Amdt. 23-62; 23.1555(a,b) Amdt. 23-62; 23.1581(a-d),(f) Amdt. 23-50; 23.1583(h,m) Amdt. 23-62; 23.1585(j) Amdt. 23-62; 25.1419 Amdt. 25-42 Regulations at an intermediate amendment Regulations at the amendment level in TCDS A24CE ---------------------------------- END- --------------------------------- SA01002DE ## Every issue (1) - July 31, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f9/eb/f9eb7504ed5cfb144d27d90940883e889b9ba29970c1647d1c03a614abd66c09) --- 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.