STC SR00871DE

Supplemental type certificate · Cert Works LLC

Holder
Cert Works LLC · United States
Status
Current · Amended
Status date
April 22, 2019
Applied
July 8, 2017
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 27
Data sheet
TCDSH9EU

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

What it approves

Installation of Garmin GTS 800 Traffic Avoidance System (TAS)

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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00871DE

This certificate and the supporting data which is the bases for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of Application: July 8, 2017 Date Reissued:

Date of Issuance: September 20, 2017 Date Amended: April 22, 2019

Signature Title Kreg R. Voorhies ODA Administrator, Cert Works ODA(AIR)-833887-NM

FAA Form 8110-2 (5/14) Page 1 of 3

This certificate, issued to: Cert Works, LLC 44110 East Arkansas Place Bennett, CO 80102

Part 27 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: H9EU Make: Airbus Helicopters Model: AS350B3, EC130T2

Description of the Type Design Change:

Installation of Garmin GTS 800 Traffic Avoidance System (TAS) in accordance with Cert Works Document CW0603-1017, Master Drawing List, EC130T2 GTS 800 Traffic Advisory System, Revision IR dated 8/15/2017, FAA approved 9/20/2017 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. CW0720-1122, Revision IR dated 8/26/2017, FAA Accepted 9/20/2017, or later FAA accepted revision are required to be made available at installation. FAA Approved Rotorcraft Flight Manual Supplement, Document No. CW0710-1124, Revision IR dated 8/10/2017 FAA Approved 9/20/2017, or later FAA approved revision is required for this modification.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(Certification Basis on page 3 of 3)

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: SR00871DE

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00871DE

Date of Issuance: September 20, 2017 Amended: April 22, 2019

FAA Form 8110-2 (5/14) Page 3 of 3

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Airbus Helicotpers AS350B3 and EC130T2 rotorcraft as follows:

a. The type certification basis for Airbus Helicotpers AS350B3 and EC130T2 rotorcraft is shown on TCDS H9EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, July 8, 2017, is based upon 14 CFR Part 27, effective February 1, 1965 plus Amendments 27-1 through 27-32, plus later amendments for certain regulations, as defined per the TCDS. Based on 14 CFR §§ 21.115 and

21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the TCDS Certification Basis (Part 27, Amendments 27-1 through 27-32):

14 CFR Sections: 27.251 Amdt. - ; 27.301 Amdt. - ; 27.303 Amdt. - ; 27.305(a) Amdt. - ; 27.307(a) Amdt. 27-26; 27.337(a) Amdt. 27-26; 27.341 Amdt. - ; 27.561(a),(b)(1)(3) Amdt. 27-32; 27.601(a) Amdt. - ; 27.603 Amdt. 27-16; 27.605(a) Amdt. 27-16; 27.609(a) Amdt. - ; 27.610 Amdt. 27-21;

27.611 Amdt. - ; 27.613 Amdt. 27-26; 27.619(b)(1) Amdt. - ; 27.625(a) Amdt. - ; 27.771(a) Amdt. - ;

27.773(a)(1)(b) Amdt. - ; 27.777 Amdt. - ; 27.853(a) Amdt. 27-17; 27.1301 Amdt. - ; 27.1309(a),(c) Amdt. 27-21; 27.1321(a,d) Amdt. 27-13; 27.1322 Amdt. 27-11; 27.1351(a),(b)(1)(i)(ii) Amdt. 27-13;

27.1357(a),(c) Amdt. 27-13; 27.1365(a) Amdt. - ; 27.1365(b) Amdt. - ; 27.1529 Amdt. 27-18; 27.1581 Amdt. 27-14; 27.1585(a) Amdt. 27-21

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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 · 2

MakeModelData sheet
Airbus HelicoptersAS-350B3H9EU
Airbus HelicoptersEC 130 T2H9EU