# STC SR09498RC-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Airbus Helicopters Inc., United States
- Description: Activation of Eurocopter France Provisions of GPS with WAAS Vertical Guidance
- Applied: October 14, 2011
- Status date: July 7, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H10EU](https://openairdocs.org/tcds/H10EU)
- Certificate PDF: https://openairdocs.org/files/sha256/c9/32/c932d41ddb48e695a276829c32025679fb30a13a7dc15f84f7e9f88ff6b21fe6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/02810FDFC00DE43C862585D900609E25.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09498RC-D

## ADs that name it (0)

None.

## Approved models (1)

- Airbus Helicopters EC155B1 ([TCDS H10EU](https://openairdocs.org/tcds/H10EU))

## 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 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of .

SR09498RC-D Airbus Helicopters, Inc.

2701 N. Forum Drive Grand Prairie, Texas 75052-7099 29 Federal Aviation Regulations H10EU Airbus Helicopters EC155B1 Activation of Eurocopter France Provisions of GPS with WAAS Vertical Guidance in accordance with Drawing List 155A82-8010, Rev B, dtd.29 July 2013 or later ODA approved revision.

For 155A73-0021-01 configuration (dual Garmin GPS 400W system), Rotorcraft Flight Manual Supplement 155FMS-013, Rev IR, dtd.19 Aug 2013 or later ODA approved revision, and Instructions for Continued Airworthiness 155MMS-021, Rev. IR, dtd. 16 May 2013 or later ODA or AEG accepted revision are required.

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 the product, the holder must give the other person written evidence of that permission. --see continuation sheets 3 and 4-- 10/14/2011 04/15/2014 08/19/2013 07/07/2020 Gina Gonzales ODA Lead Administrator ODA-700097-SW 4

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

SR09498RC-D 4

SR09498RC-D Description of Type Design Change (continued from Sheet 1):

For 155A73-0021-02 configuration (dual Garmin GTN 750 system), Rotorcraft Flight Manual Supplement 155FMS-015, Rev IR, dtd. 7 July 2020 or later ODA approved revision, and Instructions for Continued Airworthiness 155MMS-022, Rev. IR, dtd. 7 April 2020 or later ODA or AEG accepted revision are required.

Certification Basis: Based on 14 CFR §§ 21.115 and 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis is the same as TCDS H10EU Rev. 20, 1/10/2014 with the following exception: FAR 29.773 at Amendment 29-57.

Limitations and Conditions (continued from Sheet 1):

3. For 155A73-0021-01 configuration (dual Garmin GPS 400W system), this STC is limited to helicopters equipped with the following:

(a) Type Certified Dual Pilot/Single Pilot or Single Pilot, Dual Garmin GPS-400WGPS/400W installation EC catalogue option 08-43056-00-C1

(b) Type Certified MEGHAS SMD-45 Primary and Navigation Displays part number C19267YA02

(c) TSO Certified Garmin Software Main Version 4.01 part number 010-00-44-6-11 or later FAA TSO approved

For 155A73-0021-02 configuration (dual Garmin GTN 750 system), this STC is limited to helicopters equipped with the following:

(a) Type Certified Dual Pilot installation AH catalogue option 08-43075-00-CI

(b) Type Certified MEGHAS SMD-45 Primary and Navigation Displays part number C19267YA02

(c) TSO Certified Garmin Software Main Version 6.11 and 6.51 are approved

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

(Continuation Sheet) Number: SR09498RC-D Limitations and Conditions (continued from Sheet 1 & 3):

4. For 155A73-0021-01 configuration (dual Garmin GPS 400W system), EC catalogue option 08-43056-00-C1, the installation is not compatible with Helicopter Terrain and Warning System (HTAWS) functionality of the GPS-400W and HTAWS cannot be enabled when this STC is installed.

5. For 155A73-0021-01 configuration (dual Garmin GPS 400W system), EC catalogue option 08-43056-00-C1, LPV GPS approaches are NOT AUTHORIZED when the intermediate course (segment between Intermediate Fix (IF) and Final Approach Fix (FAF)) is not aligned within 2-degrees of the final approach course.

6. For 155A73-0021-02 configuration (dual Garmin GTN 750 system), AH catalogue option 08-43075-00-CI, GPS/LPV and LP GPS approaches are NOT AUTHORIZED when the intermediate approach course (segment between Intermediate Fix (IF) and Final Approach Fix (FAF)) is not aligned within 45-degrees of the final approach course.

7. For 155A73-0021-02 configuration (dual Garmin GTN 750 system), AH catalogue option 08-43075-00-CI, MOD 07.22B72 must be installed to address AD 2012-15-04 and 2014-26-02 for helicopters equipped with AMP2000 Auto Pilot Module interfaced to GTN 750 navigation units.

--END-- The latest effective date of this STC is 07/07/2020.

## Every issue (2)

- July 7, 2020: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c9/32/c932d41ddb48e695a276829c32025679fb30a13a7dc15f84f7e9f88ff6b21fe6)
- April 15, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2c/87/2c87720d2cbff0da066c068a7b1c375b72bdb784620e0fe32d18583bfced0efc)

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