# STC SR02209AK - Type: Supplemental type certificate - Status: Current, Amended - Holder: Chelton Flight Systems Inc., United States - Description: Installation of Chelton Flight Systems FlightLogic Electronic Flight Instrument System (EFIS) - Applied: April 25, 2002 - Status date: December 19, 2012 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/e7/2a/e72a7efe65a43eb73d2584e03ee15378e11afb7a003b68004ae8e9182da3e24b - Approved model list and other attachments: [SR02209AK_AML.pdf](https://openairdocs.org/files/sha256/0e/fb/0efb41770331360f35a31679bbd5ddf574eaabff42c0802dfd26fa786943ede5) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B87F92EE8467C24D86257AEC00695481.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02209AK ## ADs that name it (0) None. ## Approved models (7) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) ## 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. This Certificate issued to Part * of the * Regulations. Installation of Chelton Flight Systems FlightLogic Electronic Flight Instrument System (EFIS) per design documentation for selected configuration, as listed in Chelton Flight Systems, Inc., Master Data List (MDL) Document Number 651-045950, Revision L, dated December 10, 2012 or later FAA approved revisions. 1. Compatibility of the design change with previously approved modifications must be determined by the installer. 2. 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. 3. Installation is not permitted in Instrument Flight Rules (IFR) certified rotorcraft. 4. Activation of fuel flow functions requires installation of separately FAA approved fuel flow transducers. (Continued on Sheet 3) Chelton Flight Systems, Inc. 4001 Old International Airport Drive, Unit #10 Anchorage, Alaska 99502 * See attached FAA Approved Model List (AML) No. SR02209AK, dated December 7, 2004, for a list of approved rotorcraft models and applicable airworthiness regulations Make: Date reissued: January 11, 2010 Date amended: June 12, 2003; December 7, 2004; April 3, 2008; March 16, 2011, December 19, 2012 ( Signature) August A. Asay Manager,Anchorage Aircraft Certification Office ( Title) Date of application: April 25, 2002 Date of issuance: May 30, 2003 FAA Form 8110-2-1(10-69) Page 3 of 3 Number SR02209AK Date of application: April 25, 2002 Date of issuance: May 30, 2003 Date amended: December 19, 2012 5. Optional autopilot integration is approved, on Model 407 only, with SFIM PA85 autopilots installed in accordance with Aeronautical Accessories STC No. SR00790NY. Integration with Flight Directors is prohibited. Integration with 3-axis autopilot is prohibited. 6. Refer to MDL Document Number 651-045950, Revision L, dated December 10, 2012, for applicable Rotorcraft Flight Manual Supplement (RFMS) and Instructions for Continued Airworthiness (ICA). Certification Basis: The certification basis for installation of Chelton Flight Systems FlightLogic EFIS in Bell 206 series and 407 Rotorcraft is as follows: Regulations at the latest amendment 27-0 through 27-47: 14 CFR §§ 27.301-27.307, 27.321, 27.337, 27.561, 27.601, 27.771, 27.773, 21.777, 21.1301, 27.1303, 21.1307 – 27.1329, 27.1351, 27.1357 – 27.1381, 27.1501, 27.1519, 27.1525, 27.1529 – 27.1545, 27.1581, 27.1583 ### SR02209AK_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. **FAA APPROVED MODEL LIST (AML) SR02209AK FOR** CHELTON FLIGHT SYSTEMS STC Issue date: May 30, 2003 Amended: June 12, 2003, 07 December 2004 Rotorcraft Type Rotorcraft Specification Rotorcraft Make and Model Certificate No. and No. and Revision Level Certification Basis Bell Helicopter Textron (Canada) H2SW H2SW Revision 40 206A, 206B, 206L, 206L-1, 206L-3 CAR Part 6 April 12, 2001 Bell Helicopter Textron (Canada) H2SW H2SW Revision 40 2061-4,407 FAR Part 27 April 12, 2001 This installation has been found to be compliant with FAR 27 effective February 1, 1965 plus amendments 27-1 through 27-40 FAA APPROVED: August Federal Aviation Administration Anchorage, Alaska Date: 07 December 2004 Page 1 of 1 ## Every issue (3) - December 19, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e7/2a/e72a7efe65a43eb73d2584e03ee15378e11afb7a003b68004ae8e9182da3e24b), [SR02209AK_AML.pdf](https://openairdocs.org/files/sha256/0e/fb/0efb41770331360f35a31679bbd5ddf574eaabff42c0802dfd26fa786943ede5) - March 16, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/14/8f/148f3e5a0fc2ca20e68353ca5c2417690db3778d0c4594f5a3f3f51c92289ded), [SR02209AK AML.pdf](https://openairdocs.org/files/sha256/02/53/025376e36ffd3c867c82ff5eea6741fcfac6ad9f5601b9c555d8f9ac815ea4f7) - January 11, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6b/b3/6bb3ecfa3e9f68fac78104b8f7048cc908c87a04f2e89694e86be066886cecc9) --- 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.