Supplemental type certificate · Airbus Helicopters, Inc.

Holder
Airbus Helicopters, Inc. · United States
Status
Current · Amended
Status date
July 18, 2018
Applied
December 14, 2006
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 29
Data sheet
TCDSH13EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of NVIS/NVG Cockpit Lighting System

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.

FAA Form 8110-2 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

SR09304RC-D Airbus Helicopters, Inc.

2701 N. Forum Drive Grand Prairie, Texas 75052-7099 29 H13EU

Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2

Installation of NVIS/NVG Cockpit Lighting System in accordance with Drawing List 145A82-8005, Rev. Z, Dated 09/26/13, or later ODA approved revision, Rotorcraft Flight Manual Supplement 117FMS-222, Rev. H, dated 11/07/13, or later ODA approved revision, and Instructions for Continued Airworthiness 145MMS-004, Rev. N, dated 10/29/13 or later FAA accepted revision.

--SEE CONTINUATION SHEET on Page 3-- Installation of Night Vision Goggle (NVG) Cockpit Compatible Lighting does not include or imply approval for flight operation with NVG. The operator must receive approval from their Civil Aviation operational authority to operate with NVG. Any deviation to the cockpit/cabin configuration or position/anti-collision lights specified in the type design of this STC may affect the compatibility with the NVG and may require a re-evaluation by the FAA Aircraft Certification Office (ACO). Once the aircraft is modified with this STC, any future modification to the aircraft may also affect the compatibility with NVG and may require a re-evaluation by the FAA ACO.

--SEE CONTINUATION SHEET on Page 3-- 12/14/2006 2/1/2007 04/15/2014 9/21/2010, 7/18/2011, 11/07/2012, 11/07/2013, 07/18/2018 Gina Gonzales ODA Lead Administrator ODA-700097-SW

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SR09304RC-D

FAA Form 8110-2 (8/13) Page 3

SR09304RC-D Description of Type Design Change (continued from Page 1):

Certification Basis Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for all configurations is the same as TCDS H13EU, Rev 16 and dated 4/11/2016 except for the following: 14 CFR § 29.773 at Amendment 29-57

Limitations and Conditions (continued from Page 1):

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

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.

Latest STC amendment date July 18, 2018 ---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 · 1

MakeModelData sheet
Eurocopter Deutschland GmbHMBB-BK 117 C-2H13EU

Every issue · 4

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

DateStatusFiles
July 18, 2018Amended, currentCertificate
November 7, 2013Amended, earlier issueCertificate
November 7, 2012Amended, earlier issueCertificate
February 1, 2007Issued, earlier issueCertificate