# STC SR09495RC-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Airbus Helicopters, Inc., United States
- Description: Installation of IFR Single or Dual Pilot WAAS GPS Upgrade
- Applied: August 10, 2010
- Status date: June 12, 2017
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/91/0e/910e322e5b4fe19c90cde665291328fa98d7d9ede3867fd2e2dd63326711e411
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4CB130EA320C9A4E8625814500590F38.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09495RC-D

## ADs that name it (0)

None.

## Approved models (1)

- Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))

## 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.

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

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

SR09495RC-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 IFR Single or Dual Pilot WAAS GPS Upgrade in accordance with Drawing List 145A82-8018, Revision M, Dated September 12, 2013 or later ODA approved revision. For configuration 145A73-0054-01, Rotorcraft Flight Manual Supplement (RFMS) 117FMS-237 Rev B dated September 20, 2013 or later ODA approved revision is required and Instructions for Continued Airworthiness 145MMS-020, Revision -, dated November 30, 2010 or later FAA accepted revision is required.

For configuration 145A73-0054-02 Rotorcraft Flight Manual Supplement 145FMS-507 Rev IR Dated September 20, 2013 or later ODA approved revision is required and Instructions for Continued Airworthiness 145MMS-023, Revision IR, dated September 17, 2013 or later FAA accepted revision is required.

Prior to or concurrently with installation of this STC, the Type Certified Dual Pilot/Single Pilot or Single Pilot Dual Garmin GNS 430W installation and Type Certificated MEGHAS part number C19267ZG-12 or C19267YA02 SMD-45 displays must be installed. This installation is not compatible with Helicopter Terrain and Warning System (HTAWS) functionality of the GNS 430W and HTAWS cannot be enabled when this STC is installed. Compatibility of this design change with previously approved modifications must be determined by the installer.

“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.”

8/10/2010 12/22/2010 11/08/2013, 04/24/2014, 06/12/2017 09/23/2013 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):

SR09495RC-D

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

SR09495RC-D

## Every issue (2)

- June 12, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/91/0e/910e322e5b4fe19c90cde665291328fa98d7d9ede3867fd2e2dd63326711e411)
- December 22, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/c9/14/c91400863c18a15aa9468504029d70cd0c002a6db87483cbc63666d2f58130a8)

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