# STC SA00095BO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Pratt & Whitney Engine Services Inc., United States - Description: Installation of Pratt & Whitney Engine Services, Inc. Twin Engine Aircraft Data Acquisition System ADAS/ADAS+ Upgrade, P/N TWIN-K-010, - Applied: December 8, 1997 - Status date: October 22, 2007 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/93/04/9304cb197156d9416160ecf9f32792a57bd08676ac148ea3aeb4870c2eb2cf70 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E36480AFD8D21F968625738E00553F94.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00095BO ## ADs that name it (0) None. ## Approved models (19) - Raytheon Aircraft Company 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company A200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company A200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company A200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 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. 249 Vanderbilt Ave. Norwood, MA 02062 Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number : A24CE Make : Raytheon Aircraft Company 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, 300, B300, 300LW, B300C, 1900, 1900C, 1900D Installation of Pratt & Whitney Engine Services, Inc. Twin Engine Aircraft Data Acquisition System ADAS/ADAS+ Upgrade, P/N TWIN-K-010, in accordance with Pratt & Whitney Engine Services, Inc. Installation Manual, Document No. TWIN-I-010-1, Revision J, dated November 8, 2002, or later FAA-approved revision. 1. Pratt & Whitney Engine Services, Inc., Aircraft Flight Manual Supplement for Raytheon Aircraft Company Models 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, 300, B300, 300LW, B300C, 1900, 1900C, 1900D, Document No. TWIN-T-250-1, Revision C, approved on May 21, 2003, or later FA-approved revision, is required and must be carried in the aircraft during all flights. 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 : December 8, 1997 Date of issuance : December 18, 1998 Date reissued : October 22, 2007 Date amended : March 12, 2003; May 21, 2003 ( Signature) Robert G. Mann Manager, Boston Aircraft Certification Office ( Title) FAA Form 8110-2-1(10-69) Page 2 of 2 Number SA00095BO Date Amended: March 12, 2003, May 21, 2003 Limitations and Conditions (Cont’d): 2. Instructions for Continued Airworthiness (ICA), Pratt & Whitney Engine Services, Inc. Document No. TWIN-T-260-1, Revision D, dated November 26, 2002, or later FAA accepted revision shall be made available to the operator at the time of installation. 3. Compatibility of this design change with previously approved modifications must be determined by the installer. 4. Required maintenance, as prescribed in the applicable airframe or engine Instructions for Continued Airworthiness, shall not be predicated on the data obtained from the Pratt & Whitney Engine Services, Inc. monitoring/recording system. 5. This system shall not be used to supersede or replace the pilot’s responsibility to monitor and record engine exceedance information. ….END…. ## Every issue (1) - October 22, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/93/04/9304cb197156d9416160ecf9f32792a57bd08676ac148ea3aeb4870c2eb2cf70) --- 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.