STC SR02238AK

Supplemental type certificate · Genesys Aerosystems, Inc.

Holder
Genesys Aerosystems, Inc. · United States
Status
Current · Amended
Status date
August 16, 2017
Applied
August 20, 2004
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 29
Data sheet
TCDSH1SW

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Chelton Flight Systems FlightLogic EFIS.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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 ~~~~~~

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 5

MakeModelData sheet
Bell Helicopter Textron204BH1SW
Bell Helicopter Textron205AH1SW
Bell Helicopter Textron205A-1H1SW
Bell Helicopter Textron205BH1SW
Bell Helicopter Textron210H1SW

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
August 16, 2017Amended, currentCertificateApproved model list
January 11, 2010Reissued, earlier issueCertificate
February 17, 2006Reissued, earlier issueCertificate
April 11, 2005Issued, earlier issueCertificate