# STC SA2144NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Turboplus Aircraft Systems, Inc., United States - Description: Installation of a modified air induction system to the Continental TSIO-360 engine turbocharger compressor (Rayjay) system. - Applied: September 12, 1983 - Status date: February 24, 2017 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13) - Certificate PDF: https://openairdocs.org/files/sha256/e7/30/e7304cb557c86344be95b48ac2be5aa0f8d23bd1d1731facfc743cce8551f0f7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1E7E821B73617792862580D5005F70E0.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2144NM ## ADs that name it (0) None. ## Approved models (3) - Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28RT-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) ## 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 SA2144NM This certificate, issued to: Turboplus Aircraft Systems, Inc. 4117 35th Ave NW Gig Harbor, WA 98335 Part 3 of the Civil Air Regulations. Original Product Type Certificate Number: 2A13 Make: Piper Model: PA-28-201T, PA-28R-201T and PA-28RT-201T Description of the Type Design Change: Installation of a modified air induction system to the Continental TSIO- 360 engine turbocharger compressor (Rayjay) system in accordance with Turboplus, Inc., Installation Instructions and Assembly Drawing No. PA28-8000, dated March 6, 1984, or later FAA approved revisions. NOTE: This installation incorporates NASA submerged inlet; new filter and inlet plenum within pressure operated alternate air door and associated hardware as illustrated in PA28-8000. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 FAA Approved Model List, must be maintained as part of the permanent records for the modified aircraft. 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. (See Continuation Sheet page 3.) This certificate and the suppo rting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: September 12, 1983 Date reissued: 3/19/86; 10/30/87; 10/25/00; 8/25/05 10/15/07; 02/24/17 Date of issuance: October 13, 1993 Date amended: 3/19/86; 10/25/00 (Signature) Manager, Technical and Administrative Support Staff, Los Angeles Aircraft Certification Office (Title) Number SA2144NM Allied Eagles, LLC (Nevada LLC8556-2001) Reissued: 3/19/86; 10/30/87; 10/25/00; 8/25/05; 10/15/07 Amended: 3/19/86; 10/25/00 Limitations and Conditions: (cont’d) The conditions and limitations of Type Certificate Data Sheet E9CE apply except where superseded by the following: MODEL PA-28-201T, PA-28RT-201T AND PA-28RT-201T (TURBO ARROW III & IV), 4PCLM (NORMAL CATEGORY) AS MODIFIED BY STC SA2144NM PLACARD: Affix the following placard directly below throttle quadrant: -END- Alternate Air Automatic Alternate Air Automatic Alternate Air Automatic Manual Alt., Air Inop. ## Every issue (3) - February 24, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e7/30/e7304cb557c86344be95b48ac2be5aa0f8d23bd1d1731facfc743cce8551f0f7) - October 15, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c7/03/c70356b1356b1ad2719b310916446c284264858b64f898410f61460998c9036e) - August 25, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/fd/57/fd57aa8dd309a406888f9eaa093e3c1bb6b86838bad25589e2d763609afa4082) --- 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.