# STC SA00834DE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: MAG Aerospace, United States - Description: Installation of a cargo floor - Applied: October 11, 2016 - Status date: September 6, 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/d0/e2/d0e2a7326f38fb4b0f6d9373c3a3717c3e8bea35cb5c5c91eb89e2f88b3073a2 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/578FA88D6CA4969786258305004AB715.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00834DE ## 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 The STC’s supporting documentation (drawing s, instructions, specifications, flight manual supplements, etc.) is the property of the ST C holder. FAA Form 8110-2 (5/14) Page 1 of 2 Number: SA00834DE 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 a cargo floor in accordance with document number 2016012-101, Master Drawing List, Cessna 208B Cargo Floor Installation, Revision IR dated 12/5/2016, FAA Approved 12/8/2016 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. 2016012-ICA, Revision IR dated 11/29/2016, FAA Accepted 12/8/2016, or later FAA accepted revision are required to be made available at installation. 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. 3. Installation of this STC is limited to airplanes configured with no passenger seats in the areas where the floor is installed. (Certification Basis on page 3 of 3) Date of Application: October 11, 2016 Date Reissued: September 06, 2018 Date of Issuance: December 9, 2016 Date Amended: Signature Title (for) Christina M. Underwood Manager, Atlanta ACO Branch 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 2 of 2 Transfer the ownership of Supplemental Type Certificate Number: SA00834DE To (Name and address of transferee) From (Name and address of grantor) 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 3 of 2 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. 208B Cargo Floor Installation: a. The type certification basis for Textron Aviation, Inc. 208B is shown on the TCDS A37CE 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, October 11, 2016, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-28, as defined per the TCDS. 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 TCDS Certification Basis (Part 23, Amendments 23-1 through 23-28): 14 CFR Sections: 23.1 Amdt. 23-10; 23.17 Amdt. 23-17; 23.25(b) Amdt. 23-21; 23.29 Amdt 23-21; 23.301(a) Amdt. 23-28; 23.303 Amdt.-; 23.305(a) Amdt.-; 23.307(a) Amdt.-; 23.337 Amdt. 23-7; 23.561 Amdt. 23-7; 23.601 Amdt.-; 23.603 Amdt. 23-23; 23.605(a) Amdt, 23-23; 23.609 Amdt.-; 23.613 Amdt. 23-23; 23.623(a) Amdt. 23-7; 23.625(a) Amdt. 23-7; 23.853(a) Amdt. 23-25; 23.1519 Amdt.-; 23.1529 Amdt. 23-26 ------------------------------------------------------------END----------------------------------------------------------------- ## Every issue (2) - September 6, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d0/e2/d0e2a7326f38fb4b0f6d9373c3a3717c3e8bea35cb5c5c91eb89e2f88b3073a2) - December 9, 2016: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d1/b0/d1b0b543ec5396d0174cf894582c014b9382e56cf639e8ccfd53ed5ac097c9d1) --- 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.