# STC SA00752SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Raisbeck Engineering, United States - Description: Installation of Raisbeck Enhanced Performance Leading Edge (SA3831NM), Dual Aft Body Strakes (SA3591NM), Ram Air recovery Systems (SA3366NM), High Flotation Gear Doors (SA4175NM) and Hartzel/Beechcraft Turbofan Propeller System - Applied: April 16, 1999 - Status date: March 20, 2014 - Product: Aircraft, Small/Large Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/40/19/40192f2e9caf817228784b6297e4bc91e7c6f2be1167843933a73b4e8c5a8a1c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F6B8D7DE0B401ECA86257CA70069A66C.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00752SE ## ADs that name it (0) None. ## Approved models (10) - Beechcraft Corporation B200T ([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)) ## 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 Number SA00752SE This certificate, issued to Raisbeck Engineering 4411 South Ryan Way Seattle, WA 98178 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: A24CE Make: Beechcraft Model: See Eligible Model List, Sheet 3 Description of the Type Design Change: Installation of Raisbeck Enhanced Performance Leading Edge (SA3831NM), Dual Aft Body Strakes (SA3591NM), Ram Air recovery Systems (SA3366NM), High Flotation Gear Doors (SA4175NM) and Hartzel/Beechcraft Turbofan Propeller System. Installed in accordance with Raisbeck Engineering Master Drawing List 99-1500, Revision H, dated February 14, 2014, or later Federal Aviation Administration (FAA)-approved revision, and requires the incorporation of Supplemental Type Certificates SA4175NM (when equipped with High Flotation Gear), SA3366NM, SA3831NM, and SA3591NM. Limitations and Conditions: Approval of this change in type design applies to the models shown on the approval model list only. This approval should not be extended to these models on which other previously-approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and the appropriate FAA-approved airplane flight manual supplement shall be maintained as part of the permanent records for the modified aircraft. Aircraft must be operated in accordance with an FAA-approved copy of the applicable Airplane Flight Manual Supplement (AFMS) listed in Raisbeck Engineering Document 11-200EPIC-ORL, Revision IR, dated February 14, 2014, or later FAA-approved revision. Date of application: April 16, 1999 Date reissued: May 23, 2012 Date of issuance: November 4, 1999 Date amended: 3/14/00; 11/16/07; 6/20/08, 4/29/09; 7/15/09; 3/20/14 (Signature) Manager, Seattle Aircraft Certification Office (Title) Number SA00752SE Raisbeck Engineering Date of issuance: November 4, 1999 Date reissued: May 23, 2012 Date amended: 3/14/00; 11/16/07; 6/20/08, 4/29/09; 7/15/09; 3/20/14 Limitations and Conditions (cont’d): 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. Eligible Models: B200 S/N BB-1439, BB-1444 and after except BB-1463 B200C S/N BL-139 and after, BW-1 and after B200T S/N BT-35 and after B200CT S/N BN-5 and after B200GT S/N BY-1 and after B200CGT S/N BZ-1 and after 200/200C/B200/B200C equipped with PT6A-52 engine upgrade Per STC SA10824SC, or SA10842SC With two Hartzell HC-E4N-3G/D9390SK-1R propellers installed - END - ## Every issue (5) - March 20, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/40/19/40192f2e9caf817228784b6297e4bc91e7c6f2be1167843933a73b4e8c5a8a1c) - May 23, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/99/f1/99f18700c5301bda763217b7a53223ce8e0287ab444a11eb44317f3a6d4cd845) - July 15, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3c/39/3c392eb67523ed5cdd0eb823d99e2d0fbd0ed0925c68bd30a1a90434e216df31) - June 25, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/cd/46/cd46fb0a804d6339ec042f4c03f4b9397a1476dfd7939672a9686af63b9e0fc5) - November 16, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c7/f7/c7f77b6a0626592ffd9d00b49698c7b8995fec16251659b86f80fa23cf62f10e) --- 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.