# STC SA00171BO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Pratt & Whitney Engine Services Inc., United States - Description: Installation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010. - Applied: October 1, 2002 - Status date: October 22, 2005 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A17SW](https://openairdocs.org/tcds/A17SW), [TCDS A19SW](https://openairdocs.org/tcds/A19SW), [TCDS A9SW](https://openairdocs.org/tcds/A9SW) - Certificate PDF: https://openairdocs.org/files/sha256/4a/c2/4ac2dfee9078b9a1ad9439207035830672d6d084d9fb5fa055e7da66a3e8947c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C22CF6D4D1C956A28625738E0056D80D.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00171BO ## ADs that name it (0) None. ## Approved models (21) - Air Tractor Inc. AT-400 ([TCDS A9SW](https://openairdocs.org/tcds/A9SW)) - Air Tractor Inc. AT-400A ([TCDS A9SW](https://openairdocs.org/tcds/A9SW)) - Air Tractor Inc. AT-402 ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-402A ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-402B ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-501 ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-502 ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-502A ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-502B ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-503 ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-503A ([TCDS A17SW](https://openairdocs.org/tcds/A17SW)) - Air Tractor Inc. AT-602 ([TCDS A19SW](https://openairdocs.org/tcds/A19SW)) - Air Tractor Inc. AT-802 ([TCDS A19SW](https://openairdocs.org/tcds/A19SW)) - Air Tractor Inc. AT-802A ([TCDS A19SW](https://openairdocs.org/tcds/A19SW)) - Raytheon Aircraft Company 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Raytheon Aircraft Company C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - The Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - The Cessna Aircraft Company 208A ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - The Cessna Aircraft Company 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) ## 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 : See attached FAA Approved Model List (AML), Document No. ADAS-T- 225-1, dated July 3, 2003, or later FAA-approved revisions for the list of approved aircraft models and applicable airworthiness regulations. Installation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010, in accordance with Master Document List ADAS-T-100-1, Revision J, dated March 28, 2005, or later FAA-approved revision. Reference AML ADAS-T-225-1 for applicable installation instructions for a particular aircraft. 1. Pratt & Whitney Engine Services, Inc. Aircraft Flight Manual, Document No. ADAS-T-250-1, Revision C, FAA-approved on March 31, 2005, or later FAA-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 : October 1, 2002 Date of issuance : July 3, 2003 Date reissued : October 22, 2007 Date amended : March 31, 2005 ( Signature) Robert G. Mann Manager, Boston Aircraft Certification Office ( Title) FAA Form 8110-2-1(10-69) Page 2 of 2 Number SA00171BO Limitations and Conditions (Cont’d): 2. Instructions for Continued Airworthiness (ICA) as listed in AML ADAS-T-225-1, dated July 3, 2003, 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 (2) - October 22, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4a/c2/4ac2dfee9078b9a1ad9439207035830672d6d084d9fb5fa055e7da66a3e8947c) - March 31, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3c/12/3c12512464cd479cd4d7a5fc92681019c5a6f1f79f7dc2a30d21163a8fdee7ec) --- 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.