# STC SR02230AK - Type: Supplemental type certificate - Status: Current, Amended - Holder: Genesys Aerosystems Inc., United States - Description: Installation of Chelton Flight Systems FlightLogic Electronic Flight Instrument System (EFIS) - Applied: July 17, 2003 - Status date: September 18, 2020 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU), [TCDS H11EU](https://openairdocs.org/tcds/H11EU) - Certificate PDF: https://openairdocs.org/files/sha256/18/bd/18bdc9abca2546af708297139e9f0fe6109b6b833c31a6f5c4ac2af6bbcd23ce - Approved model list and other attachments: [SR02230AK_AML.pdf](https://openairdocs.org/files/sha256/56/9b/569b42d8fdd584758896e7b734398de9a5d4cfb3a40e92362bfe71bbad5b23cc) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/495D12B2734ED94186258601006E756A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02230AK ## ADs that name it (0) None. ## Approved models (13) - Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350D1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS355E ([TCDS H11EU](https://openairdocs.org/tcds/H11EU)) - Eurocopter France AS355F ([TCDS H11EU](https://openairdocs.org/tcds/H11EU)) - Eurocopter France AS355F1 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU)) - Eurocopter France AS355F2 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU)) - Eurocopter France AS355N ([TCDS H11EU](https://openairdocs.org/tcds/H11EU)) ## 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. FAA Form 8110-2(10-68) Page 1 of 3 Number SR02230AK T his Certificate issued to c ertifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part * of the * Regulations. D escription of Type Design Change: Installation of Genesys Aerosystems, Inc, FlightLogic Electronic Flight Instrument System (EFIS) per design documentation for selected configuration, as listed in Genesys Aerosystems, Inc., Master Data List (MDL) Document Number 17-000025, Revision L, dated May 15, 2020, or later FAA approved revisions. L imitations and Conditions: 1. Installer must determine compatibility of this design change with previously approved modifications. 2. If the holder agrees to permit another person to us e this certificate to alter the product, the holder shall give the other person written evidence of that permission. 3. Installation is not permitted in Instrument Flight Rules (IFR) certified rotorcraft. Installation is limited to having Primary Flight Display (PFD) located above Multi-Function Display (MFD). * See attached FAA Approved Model List (AML) No. SR02230AK, dated November 17, 2004, for a list of approved rotorcraft models and ap plicable airworthiness regulations. Genesys Aerosystems, Inc. 4001 Old International Airport Drive, Unit #10 Anchorage, Alaska 99502 Date reissued: January 11, 2010 Date amended: December 21, 2007; March 28, 2008; March 14, 2011; December 19, 2012; February 18, 2015; May 1, 2017; September 18, 2020 By direction of the Administrator (S ignature) August A. Asay Manager, Anchorage ACO Branch (Title) Date of application: July 17, 2003 Date of issuance: November 17, 2004 FAA Form 8110-2(10-68) Page 3 of 3 Number SR02230AK Date of issuance: November 17, 2004 L imitations and Conditions (continued): 4. Activation of Fuel Flow functions requires installation of separately approved fuel flow transducers. 5. O ptional autopilot integration is approved for SFIM PA85 autopilots installed in accordance with American Eurocopter Corporation STC numbers SH6002SW-D or SH7000SW-D. 6. R efer to MDL Document Number 17-000025, Revision L, dated May 15, 2020, or later FAA approved revision, for applicable Rotorcraft Flight Manual Supplement (RFMS) and Instructions for Continued A irworthiness (ICA). Certification Basis: The certification basis for installation of Genesys Aerosystems, Inc. FlightLogic EFIS in Eurocopter AS350 and AS355 series Rotorcraft is as follows: R egulations at the latest amendment 27-0 through 27-47: 1 4 CFR §§ 27.301-27.307, 27.321, 27.337, 27.561, 27.601, 27.771, 27.773, 21.777, 21.1301, 27.1303, 27.1307 – 27.1329, 27.1351, 27.1357 – 27.1381, 27.1501, 27.1519, 27.1525, 27.1529 – 27.1545, 27.1581, 27.1583 ### SR02230AK_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. APPROVED MODEL LIST NO. SR02230AK Initial Release 17 November 2004 Rotorcraft Type Rotorcraft Specification Rotorcraft Make and Model Certificate No. and No. and Revision Level Certification Basis Eurocopter France HOEU HOEU Revision 13 AS350B, AS350B1, AS350B2, AS350BA, FAR Part 27 AS350B3, AS350C, AS350D, AS350D1 Eurocopter France H11EU H1 1EU Revision 8 AS355E, AS355F, AS355F1, AS355F2, AS355N FAR Part 27 This installation has been found to be compliant with FAR 27 effective February 1, 1965 plus amendments 27-1 through 27-40 FAA APPROVED: Ju D an Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska ## Every issue (4) - September 18, 2020: Amended, Current. [certificate](https://openairdocs.org/files/sha256/18/bd/18bdc9abca2546af708297139e9f0fe6109b6b833c31a6f5c4ac2af6bbcd23ce), [SR02230AK_AML.pdf](https://openairdocs.org/files/sha256/56/9b/569b42d8fdd584758896e7b734398de9a5d4cfb3a40e92362bfe71bbad5b23cc) - December 19, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/49/3a/493a39f6430b2221c98d451d0fc24484f8f296d42ecb0264f60e348c91440023), [SR02230AK_AML.pdf](https://openairdocs.org/files/sha256/56/9b/569b42d8fdd584758896e7b734398de9a5d4cfb3a40e92362bfe71bbad5b23cc) - March 14, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/11/42/11422cf6604bcbf5b8fe7416dbdaa9b0158bf6b52fc33dd09a0fb01037c20736), [SR02230AK_AML.pdf](https://openairdocs.org/files/sha256/90/fc/90fce245a83af9dabd5f8d8c6ece3191d9c665d92529a10aba6525c1463cfe17) - January 11, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/25/5c/255c61099910932b36db733ad35b671e3318cfccaadf248bcbd6545d1538613a) --- 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.