# STC ST04412CH - Type: Supplemental type certificate - Status: Current, Issued - Holder: MAG Aerospace, United States - Description: Installation of FANS 1/A+ compliant datalink and voice recorder system; installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out functionality in accordance with MAG Aerospace Master Data List, Doc. No. E19024-2300L001, Revision A, dated November 20, 2019, or later FAA approved revision. - Applied: July 9, 2019 - Status date: November 22, 2019 - Product: Aircraft - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/54/c7/54c7a6ffef61ce735bcca240f93e6cc5601572948fbc5a43e19afe2e7805a23f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/790FEEE3BA93E2D5862584CB00685C1F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST04412CH ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 737-700 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) ## 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. Part 25 of the Federal Aviation Regulations. (See Page 3 of 3 for complete certification basis) Installation of FANS 1/A+ compliant datalink and voice recorder system; installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out functionality in accordance with MAG Aerospace Master Data List, Doc. No. E19024-2300L001, Revision A, dated November 20, 2019, or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. FAA Approved Flight Manual Supplements, MAG Aerospace Doc. No’s. E19024-2300-B005, Revision IR, dated November 22, 2019, and E19024-2300-B006, Revision IR, dated November 22, 2019, and E19024-2300B010, revision IR, dated November 22, 2019 or later FAA approved revisions are required onboard the modified aircraft. 3. FAA Approved Instructions for Continued Airworthiness – Airworthiness Limitations, Section 5 of MAG Aerospace Document No. E19024-2300-B001, Revision – , approved November 22, 2019, or later FAA approved revision is a required part of this STC. 4. 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. MAG Aerospace 7065 Challenger Avenue Titusville, FL 32780 A16WE Make: The Boeing Company Model: 737-700 Series Date of application : July 9, 2019 Date of issuance : November 22, 2019 (Signature) Brenda L. Litchfield ODA Administrator Envoy Aerospace, LLC ODA-831240-CE (Title) FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number ST04412CH Date of issuance: November 22, 2019 Certification Basis:(continued) The certification basis for the Boeing 737-700 Series aircraft as described in this certificate is as follows: a. The type certification basis for the Boeing 737-700 Series is shown on TCDS A16WE for parts not changed or not affected by this change. b. The type certification basis for the parts changed or affected by this change since the reference date of application, July 9, 2019, is shown on TCDS A16WE. The applicant has complied with 14 CFR Part 25, as amended by Amendments 25-77 or later as specified by the sections listed below, and by Special Conditions listed below, and 14 CFR 26 as amended by Amendment 26-1 as listed below. 14 CFR Part 25 Regulations at amendment level 25-77 or later as specified on TCDS A16WE 25.29(a), (b); 25.301(a), (b); 25.303; 25.305(a), (b); 25.307(a); 25.341(a) ; 25.365(a), (b), (c), (d); 25.561(c); 25.571(a), (b); 25.581(a), (b), (c); 25.601; 25.603(a), (b), (c); 25.605(a); 25.609(a), (b); 25.611; 25.613(a), (b), (c), (d); 25.619(a), (b), (c); 25.625(a); 25.771(a); 25.777(a), (c); 25.789(a); 25.863(a), (b), (c), (d); 25.1301(a), (b), (c), (d); 25.1307(c); 25.1309(a), (b), (c), (d), (e), (f), (g); 25.1316(b), (c); 25.1321(e); 25.1322(a), (b), (c), (d); 25.1333(a), (b), (c); 25.1351(a); 25.1353(a), (b); 25.1355(c); 25.1357(a), (c); 25.1381(a), (b) 25.1431(a), (b), (c); 25.1457(a), (b), (c), (d)(1)(i), (d)(2), (d)(3), (d)(6), (e) , (f), (g); 25.1501(a), (b); 25.1523(a), (b); 2 5.1529; 25.1581(a), (b), (d); 25.1583( h); 25.1585(a), (b). 14 CFR Part 25 Regulations at other amendment levels 25.869(a)(4) [Amdt 25-113]; 25.981(a)(3) [Amdt 25-102] . 14 CFR Part 26 Regulations Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the latest amendment date of this STC, compliance has been found for the following regulations: 14 CFR §§ 26.11(c) [Amdt. No. 26-0]; 26.47(c) [Amdt. No. 26-1]. Special Conditions 25-632-SC, Special Conditions, Boeing Model 737-8 Airplane; Non-Rechargeable Lithium Battery Systems, dated August 19, 2016. -----END---- ## Every issue (1) - November 22, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/54/c7/54c7a6ffef61ce735bcca240f93e6cc5601572948fbc5a43e19afe2e7805a23f) --- 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.