# STC SA1783NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Raisbeck Engineering Inc., United States - Description: Install Mark VI system. - Applied: December 11, 1980 - Status date: September 1, 2023 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/36/41/364107d16768e51b7d6eb552ca91670b15687cfce20f7d4358fae4a3ff177d10 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195965669920230926134705.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA1783NM ## ADs that name it (0) None. ## Approved models (26) - Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200T ([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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: Page 1 of 2 SA1783NM Raisbeck Engineering Inc. 2811 South 102nd Street , Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviatin Regulations. A24CE Beech 200 Series Installation of the Mark VI system in accordance with the drawings listed on FAA sealed Raisbeck Engineering Drawing List 81-1007. The Mark VI system consists of modification to nose vane, windshield wiper arm and installation of Ram Air recovery system. reduced frontal area exhaust stacks, aft body strakes, aileron seals, and recontoured leading edge between nacelle and fuselage. December 11, 1980 February 24, 1983; March 22, 1989; September 1, 2023 December 30, 1982 for Manager, West Certification Branch A copy of this Certificate shall be maintained as part of the permanent record of each airplane so modified. This approval should not be extended to other specific airplanes of these same models on which other previously approved modifications are incorporated unless it is determined that the interrelationship; between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: Page 2 of 2 SA1783NM ## Every issue (2) - September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/36/41/364107d16768e51b7d6eb552ca91670b15687cfce20f7d4358fae4a3ff177d10) - March 22, 1989: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a6/10/a610c3afb8da06276d2b4531970aed4f148661cef454156d7f1a5f0b72549848) --- 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.