Supplemental type certificate · Airbus Helicopters, Inc.

Holder
Airbus Helicopters, Inc. · United States
Status
Current · Reissued
Status date
June 30, 2017
Applied
September 19, 2012
Product
Aircraft · Rotorcraft
Certification basis
Part 21
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 G500H Electronic Flight Instrument System (EFIS) with optional Garmin GRA 5500 Radar Altimeter 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

SR09497RC-D Airbus Helicopters, Inc.

2701 N. Forum Drive Grand Prairie, Texas 75052-7099 27 H9EU Airbus Helicopters EC130T2

Installation of Garmin G500H Electronic Flight Instrument System (EFIS) with optional Garmin GRA 5500 Radar Altimeter System in accordance with Drawing List 130A82-8019, Rev W, dtd. 18 July 2016 or later ODA approved revision. Rotorcraft Flight Manual Supplement 130FMS-506 Rev B, dtd. 10 Aug. 2016 or later ODA approved revision is required.

For configurations -01 through -06, Instructions for Continued Airworthiness (ICA) 130MMS-020 Rev. C, dtd. 14 March 2016 or later FAA AEG/ODA approved revision is required.

---SEE CONTINUATION SHEET on page 3---

1. This G500H EFIS installation approves the Garmin GDU 620 display (left and right hand PFD versions), GRS 77H AHRS, GMU 44 Magnetometer, GDC 74H ADC and GTP 59 OAT only.

2. This STC approves the interface of Garmin GNS400W/500W and GTN650/750 series GPS/NAV/COM, GMA340H audio panel, GTX330 transponder, and optional GRA 5500 Radar Altimeter to the G500H EFIS.

3. The VEMD OAT sensor must be used for performance calculations

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

---SEE CONTINUATION SHEET on page 3--- 9/19/2012 3/27/2013 04/15/2014, 07/24/2015, 6/30/2017 08/10/2016 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):

SR09497RC-D

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

SR09497RC-D Description of Type Design Change, cont. from page 1:

For configuration -07 (dual pilot), ICA 130MMS-027 Rev. IR, dtd 14 July 2016 or later FAA AEG/ODA approved revision is required.

For configuration -15 (optional radar altimeter), ICA 130MMS-026 Rev. IR, dtd 23 July 2016 or later FAA AEG/ODA approved revision is required.

Limitations and Conditions, cont. from page 1:

5. 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.

---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
Airbus HelicoptersEC 130 T2H9EU

Every issue · 3

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

DateStatusFiles
June 30, 2017Reissued, currentCertificate
August 10, 2016Amended, earlier issueCertificate
March 27, 2013Issued, earlier issueCertificate