# STC SE2146NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Turboplus Aircraft Systems, Inc., United States - Description: Conversion of the Continental TSIO-360-FB engine (200 HP-2575 RPM) to the operating limits of the *(-KB) engine. - Applied: September 12, 1983 - Status date: February 24, 2017 - Product: Engine - Certification basis: Part 21, Part 33 - Data sheets: [TCDS E9CE](https://openairdocs.org/tcds/E9CE) - Certificate PDF: https://openairdocs.org/files/sha256/3a/3e/3a3e8858338fe99cf620b24fa203fc01456b980a147a4da03e260467589dea45 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D30EB50F86A62F59862580D500650CDB.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SE2146NM ## ADs that name it (0) None. ## Approved models (1) - Teledyne Continental Motors TSIO-360-FB ([TCDS E9CE](https://openairdocs.org/tcds/E9CE)) ## 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 SE2146NM This certificate, issued to Turboplus Aircraft Systems, Inc. 4117 35th Ave NW Gig Harbor, WA 98335 Part 33 of the Federal Aviation Regulations. Original Product Type Certificate Number: E9CE-15 Make: Continental Model: TSIO-360-FB Description of the Type Design Change: Conversion of the Continental TSIO-360-FB engine (200 HP-2575 RPM) to the operating limits of the *(-KB) engine in accordance with Turboplus, Inc., Conversion Instructions No. PA28- 11000, dated June 2, 1983, or later FAA approved revision. NOTE: The converted engine shall incorporate pressurized magnetos as per SE1760NM, SE4177NM, or SE4303NM. Limitations and Conditions: Approval of this change in type design applies to the above model engine only, and is limited to Piper PA-28-201T (Cherokee), PA-28R-201T and PA28RT-201T (Turbo Arrow III & IV) aircraft modified per STC SE2146NM. This approval should not be extended to other engines of this model on which other previously approved modifications are incorporated unless it is determined 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 engine. A copy of this Certificate must be maintained as part of the permanent records for the modified engine. 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: September 12, 1983 Date reissued: 3/19/86; 10/30/87; 10/25/00; 8/25/05; 10/15/07; 2/24/17 Date of issuance: October 17, 1983 Date amended: 11/28/83; 10/25/00, 7/2/08 (Signature) Manager, Technical and Administrative Support Staff, Los Angeles Aircraft Certification Office (Title) Number SE2146NM Allied Eagles, LLC (Nevada LLC8556-2001) Reissued: 3/19/86; 10/30/87; 10/25/00; 8/25/05; 10/15/07 Amended: 11/28/83; 10/25/00, 7/2/08 Limitations and Conditions: (cont’d) The conditions and limitations of Type Certificate Data Sheet No. E9CE apply except where superseded by the following: Engine: 1 Teledyne Continental TSIO-360-FB(C) Fuel: 100/100LL Minimum Grade Aviation Gasoline Engine Limits: * Takeoff, 5 minutes, 2800 RPM and 40“Hg * Manifold Pressure (220 HP) * Max Continuous, 2600 RPM and 40“ Hg * Manifold Pressure (200 HP) * Critical Altitude, 2600 RPM and 40“ Hg (18,000 ft) PLACARDS: Placards and Operating Limitations on Type Certificate Data Sheet E9CE apply except as noted herein: a. Original Engine Data Plate: Add a “suffix” (C) and the STC number to the model designation as follows: b. Supplemental Engine Data Plate: Install a supplemental data plate adjacent to the original data plate to read as follows: END FAA FORM 8110-2- 1 (10-69) Page 2 of 3 Model: TSIO-360-FB(C) – STC SE2146NM **TELEDYNE CONTINENTAL ENGINE** **SUPPLEMENTAL DATA PLATE STC SE2146NM** *Takeoff (5 min) 220 HP @ 2800 RPM *Maximum continuous power – 200 HP @ 2600 RPM *M.P. Limit – 40” ## Every issue (3) - February 24, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3a/3e/3a3e8858338fe99cf620b24fa203fc01456b980a147a4da03e260467589dea45) - October 15, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/74/49/7449c20bcccccc69978efd8f05cdc650f6a3a556644b185a6df708e5cd318635) - August 25, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/19/6c/196c0beeb110c0b6e570e279df4df982ea3e5abf0ec0c170a54946debb51096b) --- 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.