# STC SA09923AC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Fieldtech Avionics and Instruments Inc., United States - Description: Installation of an L-3 Digital Flight Data Recorder, impact switch, and associated accelerometer - Applied: August 14, 2018 - Status date: November 29, 2021 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/a4/06/a40627b54652c484f719d66c48d6f8f8758a5142acc5f2d76c2a134548aefa45 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159148062020250729182150.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA09923AC ## ADs that name it (0) None. ## Approved models (10) - Textron Aviation Inc. 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300C ([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. SA09923AC Fieldtech Avionics and Instruments, Inc. 4151 North Main Street Fort Worth, TX 76106 Part 23 the Federal Aviation Regulations A24CE Textron Aviation, Inc. 200, 200C, B200, B200C, B200GT, B200CGT, 300, 300LW, B300, B300C Installation of an L-3 Digital Flight Data Recorder, impact switch, and associated accelerometer in accordane with Master Data List 1001-MDL-1400, Revision IR, dated March 17, 2021, or later FAA approved revision. (See continuation sheet 3 of 4) August 14, 2018 November 29, 2021 April 14, 2021 Jim Grigg Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service 4 SA09923AC 4 SA09923AC Date of Issuance: April 14, 2021 Date of Reissuance: November 29, 2021 The installer must determine whether this design change is compatible with previously approved modifications. 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. Garmin Avionics STC SA01535WI-D for the Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP) is a prerequisite for the installation of the Digital Flight Data Recorder modification described on the Master Data List identified above. Airplane Flight Manual Supplement (AFMS) 1001-FMS-1000, Revision IR, dated October 16, 2020, or later FAA approved revision, is required. Aircraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) 1001-ICA-1000, Revision C, dated February 6, 2021, or later accepted FAA revision. Certification Basis: Based on 14 CFR ยงยง 21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Textron Aviation King Air Models: 200, 200C, B200, B200C, B200GT, B200CGT, 300, 300LW, B200, B200C is as follows: a. The type certification basis for Textron Aviation King Air Models: 200, 200C, B200, B200C, B200GT, B200CGT, 300, 300LW, B300, B300C airplanes is shown on TCDS A24CE for parts not changed or not affected by this installation. SA09923AC Date of Issuance: April 14, 2021 Date of Reissuance: November 29, 2021 Certification Basis (continued): b. The certification basis for parts changed or affected by this installation is as follows: Regulation Amdt Regulation Amdt Regulation Amdt 23.29 23-21 23.611 23-48 23.1321 e 23-49 23.301 a,b 23-48 23.613 a,b,c 23-45 23.1322 b,e 23-43 23.303 Original 23.619 23-7 23.1351 a 23-49 23.305 a,b 23-45 23.625 a,b 23-7 23.1353 a,b,c,d 23-49 23.307 a Original 23.6 Original 23.1357 a,c 23-43 23.321 a,b Original 23.671 a Original 23.1359 a,c 23-49 23.341 23-34 23.685 a,c,d 23-7 23.1365 a,b,d,e 23-49 23.561 a,b,e 23-34 23.689 a 23-7 23.1367 a,b Original 23.601 Original 23.867 a,b 23-49 23.1431 a,b 23-49 23.603 a,b 23-23 23.1301 a,b,c,d 23-20 23.1459 23-35 23.605 a 23-23 23.1306 23-61 23.1529 23-26 23.607 23-48 23.1308 23-57 23.1581 a(2) 23-50 23.609 a,b Original 23.1309 a(1)(3),b,e,f 23-49 -END- 4 4 ## Every issue (2) - November 29, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/06/a40627b54652c484f719d66c48d6f8f8758a5142acc5f2d76c2a134548aefa45) - August 14, 2021: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/b5/4f/b54ff9ca06bd0f593247d954fc7a692c6c96b8047c53a7e5abbfabdf70df9b0f) --- 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.