# STC SA00295BO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Pratt & Whitney Engine Services Inc., United States - Description: Installation of the Pratt & Whitney Engine Services ADASd - Applied: July 31, 2008 - Status date: May 14, 2010 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/16/1a/161a380f8379baf93a0d7fd30580c82e8af367958f5bcce465eeb6d3e3e86674 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7C412048ED1F8A58625772F007B1342.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00295BO ## ADs that name it (0) None. ## Approved models (5) - Hawker Beechcraft Corporation 300 ([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 B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300C (C-12W) ([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. Number SA00295BO This Certificate issued to Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number: A24CE Make: Hawker Beechcraft Corporation Model: B200, B200C, 300, B300, B300C Description of Type Design Change: Installation of the Pratt & Whitney Engine Services ADASd in accordance with Pratt & Whitney Engine Services’ Master Document List No. DAAS-T-100-3, Revision D, dated May 13, 2010, or later FAA-approved revision. 1. Pratt & Whitney Engine Services , Fli ght Manual Supplement No. DAAS-T-250-5 for Hawker Beechcraft Corporation Models B200, B200C, 300, B300, and B300C Part 23 aircraft, Revision D, approved May 14, 2010 , or later FAA approved revision, is required with this modification. 2. Instructions for Continued Airworthiness (ICA), Pratt & Whitn ey Document No. DAAS-G-260-5 , Revision D, dated May 4, 2010 or later FAA accepted revision shall be made available to the operator at the time of installation. 3. Compatibility of this design with previously approved modifications must be determined by the installer. 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. Date of application: July 31, 2008 Date reissued: Date of issuance: January 05, 2010 Date amended: May 14, 2010 (Signature) Robert G. Mann Manager Boston Aircraft Certification Office (Title) Pratt & Whitney Engine Services, Inc. 249 Vanderbilt Avenue Norwood, MA 02062 United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA00295BO Effective Date: May 14, 2010 Certification Basis Model B200, B200C, 300, B300, B300C Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for signifi cant changes in FAA Order 8110.48, the certification basis for the Hawker Beechcraft B200, B200C, 300, B300, and B300C aircraft models is as follows: a. The type certification basis for Hawker Beechcraft B200, B 200C, 300, B300, B300C model aircraft is shown on the TCDS A24CE for parts not changed or not affected by the change. b. The type certification basis for parts chan ged or affected by the change since the reference date of application, July 31, 2008, is based upon Part 23 as amended by Amendment 23-58. 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 latest amendment 23-0 through 23-58 §23.301(a), §23.303, §23.305(a), §23.307(a), §23.561(b), §23.601, §23.603(b), §23.605(a), §23.609, §23.613(a), §23.1301, §23.1309, §23.1322, §23.1357, §23.1365, §23.1431, §23.1529, §23.1367 Regulations at an intermediate amendment None. Regulations at the amendment level in the TCDS A24CE None. -END- ## Every issue (2) - May 14, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/16/1a/161a380f8379baf93a0d7fd30580c82e8af367958f5bcce465eeb6d3e3e86674) - January 5, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/af/53/af530c64cfba6664aec0ca0361a8bbf2fe9c8102857f275eaa6e9989af8076e9) --- 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.