# STC SR02238AK

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Genesys Aerosystems, Inc., United States
- Description: Installation of Chelton Flight Systems FlightLogic EFIS.
- Applied: August 20, 2004
- Status date: August 16, 2017
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW)
- Certificate PDF: https://openairdocs.org/files/sha256/7b/71/7b71d8353b2f6d9bb4600bd1bf43b0c3b3c49d8bf42785d7a128798e0660361a
- Approved model list and other attachments: [SR02238AK_AML.pdf](https://openairdocs.org/files/sha256/11/c7/11c773c07669fc21596344ca8588effac4660c8a6f6d31501e7a0124c5e03c16)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/23564394F33D83C786258186004B608B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02238AK

## ADs that name it (0)

None.

## Approved models (5)

- Bell Helicopter Textron 204B ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 205A ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 205B ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 210 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))

## 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.

Installation Genesys Aerosystems, Inc. FlightLogic Electronic Flight Instrument System (EFIS) in accordance with Genesys Aerosystems Installation Instructions 150-045264, Revision W, dated April 23, 2007 or later approved revisions.

1. Installer must determine compatibility of this design change with previously approved modifications.

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. FAA approved Rotorcraft Flight Manual Supplement 150-045709-0204, Revision E, dated August 16, 2017 or later FAA approved revision is required.

4. For Instructions for Continued Airworthiness, refer to Chelton Rotorcraft Instructions for Continued Airworthiness 150-045284, Revision M, dated March 3, 2017 or later FAA accepted revision.

5. The four-display installation does not satisfy the requirements of CAR 7.612(f) or 14 CFR Part 29.1333(a) that required duplicate flight instruments have independent systems. If duplicate instruments are required by operational rules a separate instrument system like Bell Helicopter 204/205 co-pilot instrument kit is required.

Limitations and conditions Continued on Sheet 3

Genesys Aerosystems, Inc.

4001 Old International Airport Drive, Unit #10 Anchorage, Alaska 99502 * See attached FAA Approved Model List (AML) No. SR02238AK, dated February 17, 2006, for a list of approved rotorcraft models and applicable airworthiness regulations

January 11, 2010; February 18, 2015

February 17, 2006; August 16, 2017

(Signature) August A. Asay Manager, Anchorage ACO Branch

(Title)

FAA Form 8110-2-1(10-69) Page 3 of 3

August 20, 2004 April 11, 2005

FAA Form 8110-2-1(10-69) Page 3 of 3

SR02238AK

August 20, 2004 April 11, 2005 August 16, 2017

6. Activation of Fuel Flow functions requires installation of separately FAA approved fuel flow transducers.

7. Installation is not permitted in Instrument Flight Rules (IFR) certified rotorcraft.

~~~~~~ End ~~~~~~

### SR02238AK_AML.pdf

- Genesys Aerosystems, Inc. Approved Model List (AML) 4001 Old International Airport Dr, Unit #10 Number SR02238AK Anchorage, AK 99502 Date of Issuance: 11 April 2005 Date of Amendment: 17 February 2006

Page 1 of 1

Approved Model List For: Chelton Flight Systems FlightLogic EFIS

NOTES:

Original Product Make Original Product Model Original Product Type Certificate No.

Certification basis Bell Helicopter Textron 204A, 205A, 205A-1, 205B H1SW CAR Part 7 August 1 1956 Amendments as listed on TCDS H1SW Bell Helicopter Textron 210 H1SW 14 CFR Part 29 Amendments as listed on TCDS H1SW

## Every issue (4)

- August 16, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/7b/71/7b71d8353b2f6d9bb4600bd1bf43b0c3b3c49d8bf42785d7a128798e0660361a), [SR02238AK_AML.pdf](https://openairdocs.org/files/sha256/11/c7/11c773c07669fc21596344ca8588effac4660c8a6f6d31501e7a0124c5e03c16)
- January 11, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/14/e8/14e8236e44043493699fc6bf0174876100998959c61e5b52e7817b343c743568)
- February 17, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/9f/76/9f76658cea7b75c7a95a6d9dba9273d01ff6d0ebb480d289da305c5f5cc402aa)
- April 11, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/4a/af/4aaf1e2b99ad731f09b1677d9f8475237f1e32b7127a354427e882d5eca6eef6)

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