# STC SE02291AT - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Continental Motors, Inc., United States - Description: Conversion of the engine from a carburetor fuel system and magneto ignition system to a full authority digital electronic control (FADEC) system for fuel injection and ignition. - Applied: June 15, 2000 - Status date: November 6, 2013 - Product: Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS E-286](https://openairdocs.org/tcds/E-286) - Certificate PDF: https://openairdocs.org/files/sha256/a4/d8/a4d837b917e69f2343ed58ee44d3d773e4348afa7794724c59e322a12951ca24 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/87501E1652EE5B3A86257C290059141E.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SE02291AT ## ADs that name it (0) None. ## Approved models (61, first 50) - Lycoming Engines O-360-A1A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1AD ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1C ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1F ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1F6 ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1F6D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1G ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1G6 ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1G6D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1H ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1H6 ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1LD ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A1P ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2E ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2F ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2G ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A2H ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A3A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A3AD ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A3D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4AD ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4G ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4J ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4K ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4M ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4N ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A4P ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-A5AD ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-B1A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-B1B ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-B2A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-B2B ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-B2C ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C1A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C1C ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C1E ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C1F ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C1G ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C2A ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C2B ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C2C ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C2D ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C2E ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C4F ([TCDS E-286](https://openairdocs.org/tcds/E-286)) - Lycoming Engines O-360-C4P ([TCDS E-286](https://openairdocs.org/tcds/E-286)) All 61: https://openairdocs.org/stc/SE02291AT/models.md ## 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 SE02291AT This certificate issued to Part 3 of the Civil Air Regulations. Original Product Type – Certificate Number: Description of Type Design Change: Conversion of the engine from a carburetor fuel system and magneto ignition system to a full authority digital electronic control (FADEC) system for fuel injection and ignition. Conversion to be accomplished in accordance with the installation instructions contained in Continental Motors Form FIM-LYC, entitled “Continued Airworthiness Instructions for Converting a 180 hp Lycoming O-360 Four–Cylinder Aircraft Engine to a FADEC Engine”, revision “N/C”, dated July 2001, or later FAA approved revision. Limitations and Conditions: 1). Engine conversion is subject to the requirements noted on the continuation sheet (see page 2). 2). This approval should not be extended to other engines of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modification will produce no adverse effect upon the airworthiness of that engine. 3). 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. Continental Motors, Inc. 2039 South Broad St. Mobile, AL 36615 E286 Make: Lycoming Model: O-360 Date reissued: November 6, 2013 (Signature) Melvin D. Taylor Manager, Atlanta Aircraft Certification Office (Title) Date of application: June 15, 2000 Date of issuance: July 26, 2001 Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and Street ) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and Street) (City, State, and ZIP code) Signature of grantor (In ink): ## Every issue (1) - November 6, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/d8/a4d837b917e69f2343ed58ee44d3d773e4348afa7794724c59e322a12951ca24) --- 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.