# STC SA04007NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: MAG Aerospace, United States - Description: Installation of Retractable Mount, Turret as Inert Load Only (Not Including Turret Systems Functionality), and Wiring Provisions - Applied: August 31, 2017 - Status date: August 1, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) - Certificate PDF: https://openairdocs.org/files/sha256/d9/ad/d9ad4bcf6f39d270cca65b69601ae8e525aeced25bfdd02d1da49d14a2533445 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3C85296BB94B6F90862582E10055CBEB.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA04007NY ## ADs that name it (0) None. ## Approved models (1) - Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) ## 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 Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA04007NY This certificate issued to: MAG Aerospace 7065 Challenger Avenue Titusville, FL 32780 Part 23 of the Federal Aviation Regulations. Original Product – Type Certificate Number: A37CE Make: Textron Aviation Inc. Model: 208B Description of Type Design Change: Installation of Retractable Mount, Turret as Inert Load Only (Not Including Turret Systems Functionality), and Wiring Provisions in accordance with FAA Approved Aerospace Design & Compliance (1) Master Data List, C208B-MDL-0010, Revision B, dated November 9, 2017, or later FAA approved revision. (2) Instructions for Continued Airworthiness (ICA) C208B-ICA-0010. Revision IR, dated November 9, 2017, or later FAA accepted revision. The ICA and its contents must be incorporated into the operator’s maintenance program. (3) Airplane Flight Manual Supplement C208B-AFMS-0010, Revision IR, dated November 9, 2017 or later approved revision. 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. Date of Application: August 31, 2017 Date Reissued: March 28, 2018, August 01, 2018 Date of Issuance: November 9, 2017 Date Amended: March 28, 2018 By Direction of the Administrator Signature Title (for) Christina M. Underwood Manager, Atlanta ACO Branch Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an ai rcraft, aircraft engine, or propeller. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: SA04007NY To (Name and address of transferee) From (Name and address of grantor) Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an ai rcraft, aircraft engine, or propeller. FAA Form 8110-2 (5/14) Page 3 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA04007NY Reissued: August 01, 2018 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, Model 208B airplane is as follows: (1) The type certification basis for Textron, Model 208B airplane is shown on the TCDS A37CE for parts not changed or not affected by the change. (2) The certification basis for parts changed or affected by the change since the reference date of application April 12, 2017, is based upon part 23 as amended by Amendment 23-28 with the exception of those above amendment 23-28, listed below. Regulations at later amendment than 23-28: 14 CFR Part Amendment 23.777(a)(b) 23-33 23.1359(c) 23-49 23.1431(b) 23-43 23.1581(a)(2)(f) 23-50 ------------------------------------------------------------END----------------------------------------------------------------- ## Every issue (2) - August 1, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d9/ad/d9ad4bcf6f39d270cca65b69601ae8e525aeced25bfdd02d1da49d14a2533445) - March 28, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3b/75/3b75affee526fedc69b308404351c08dcf8793421ed686b032b6569f535fcbf4) --- 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.