# STC SA10737SC - Type: Supplemental type certificate - Status: Current, Issued - Holder: Blackhawk Modifications Inc. - Description: Installation of Pratt & Whitney Canada PT6A-61Engines and Hartzell (Raisbeck) HC-D4N3A/D9383K-1 Propellers - Status date: September 21, 2007 - Data sheets: A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE - Certificate PDF: https://openairdocs.org/files/sha256/80/4b/804b01dce42b105184b0537ece2d65c4d56629b6edc69bf0453304cad67b7c52 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7E90C426BAFE7A8486257B87004991CD.0001 - Page: https://openairdocs.org/stc/SA10737SC ## ADs that name it None. ## Approved models (12) - Hawker Beechcraft Corporation 200 (TCDS A24CE) - Hawker Beechcraft Corporation 200C (TCDS A24CE) - Hawker Beechcraft Corporation 200CT (TCDS A24CE) - Hawker Beechcraft Corporation 200T (TCDS A24CE) - Hawker Beechcraft Corporation B200 (TCDS A24CE) - Hawker Beechcraft Corporation B200C (TCDS A24CE) - Hawker Beechcraft Corporation B200C (C-12F) (TCDS A24CE) - Hawker Beechcraft Corporation B200C (C-12R) (TCDS A24CE) - Hawker Beechcraft Corporation B200C (UC-12F) (TCDS A24CE) - Hawker Beechcraft Corporation B200C (UC-12M) (TCDS A24CE) - Hawker Beechcraft Corporation B200CT (TCDS A24CE) - Hawker Beechcraft Corporation B200T (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 Project Number ST8563SC-A TB Part 23 of the Federal Aviation Regulations. Description of Type Design Change: Installation of Pratt & Whitney Canada PT6A-61Engines and Hartzell (Raisbeck) HC-D4N3A/D9383K-1 Propellers in accordance with Blackhawk Modifications, Inc. Master Drawing List Document Number 06010050, Rev. IR dated June 05, 2007, or later FAA approved revision. FAA approved Blackhawk Modification Inc. Flight Manual Supplement No. AFMS 06010102, Rev. IR dated September 18, 2007, or later FAA approved revision is required. Instructions for Continued Airworthiness are contained in Blackhawk Modifications Inc. Document Number 06010105, Rev. A dated June 5, 2007. Limitations and Conditions : The installer must determine whether the design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certification to alter a product, the holder must give the other person written evidence of that permission. Blackhawk Modifications, Inc. 7601 Karl May Drive Waco, TX 76708 A24CE Make : Hawker Beechcraft Model : 200; 200C; 200T; 200CT; B200; B200C; B200CT; and B200T Date of application: September 11, 2006 Date of issuance: September 21, 2007 ( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region ( Title) ## Every issue (1) - September 21, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/80/4b/804b01dce42b105184b0537ece2d65c4d56629b6edc69bf0453304cad67b7c52) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.