# STC SR11944WI - Type: Supplemental type certificate - Status: Current, Issued - Holder: Garmin International Inc., United States - Description: Installation of a Garmin GFC 600H Helicopter Flight Control System - Applied: August 18, 2023 - Status date: June 13, 2025 - Product: Aircraft, Rotorcraft - Certification basis: Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/b8/a8/b8a8d8fffd98412169bc8559eeb122d8579bd4ca5ab5b3c6e5d881832d0c462f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145110521020260723175539.0001 - DRS record last changed: July 23, 2026 - Page: https://openairdocs.org/stc/SR11944WI ## ADs that name it (0) None. ## Approved models (1) - Airbus Helicopters EC130T2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental TypeCertificate FAA Form 8110-2 (03/21) Page 1 of This certificate issued to: Certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirementVRI3DUW RIWhe Federal Aviation Regulations . (See Continuation Sheet on Page 3) Title SR11944WI Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062 27 H9EU Airbus Helicopters EC 130 T2 Installation of a Garmin GFC 600H Helicopter Flight Control System in accordance with Garmin Master Drawing List, 005-01095-87 Rev. 1, dated June 13, 2025 or later FAA-approved revision. Instructions for Continued Airworthiness are provided in the Maintenance Manual, 190-02081-13 Rev. 1, dated June 13, 2025 or later FAA-approved revision. Operating information is provided in the Rotorcraft Flight Manual Supplement, 190-02081-12 Rev. 1, dated June 13, 2025 or later FAA-approved revision. (1) This STC is applicable to all serial numbers for this Airbus Helicopters EC 130 T2. (2) The installer must determine whether this design change is compatible with previously approved modifications. (3) 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. August 18, 2023 June 13, 2025 JR Brownell ODA STC Unit Administrator ODA-240087-CE 3 United States of America Department of Transportation Federal Aviation Administration Supplemental TypeCertificate FAA Form 8110-2 (03/21) Page 2 of Number: Transferr Endorsementt Transfer the ownership of Supplemental Type Certificate Number: Too (Name and address of transferee): Fromm (Name and address of grantor): 3 SR11944WI United States of America Department of Transportation Federal Aviation Administration Supplemental TypeCertificate FAA Form 8110-2 (03/21) Page 3 of (Continuation Sheet) Number: Issued: Certification Basis: Amdt. Amdt. SectionSection Amdt. Section 3 SR11944WI June 13, 2025 (4) A copy of this certificate, the approved RFMS, and the approved ICA must be maintained as part of the permanent records for this modified rotorcraft. (5) Installation of the G500H TXi Display System (including the GSU 75H) and Garmin GTN navigator are prerequisites to installing the GFC 600H Helicopter Flight Control System. (6) Rotorcraft equipped with a Dynamic Ventilation System are not approved for installation of the GFC 600H Helicopter Flight Control System. (7) This STC is applicable to VFR rotorcraft only. Based on 14 CFR ยงยง 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this change is at amendment Initial through 27-51, as shown below. 27.1(a)(b) 27.141(a)(1)(2)(3)(b)(2)(c) 27.143(a)(c)(d)(e)(f)(1) 27.151(a)(b) 27.161(a)(b) 27.171 27.251 27.301(a)(b)(c) 27.303 27.305(a) 27.307(a)(b)(2)(3) 27.337(a) 27.395(a)(b)(1)(2)(3) 27.397(a) 27.561(a)(b)(3) 27.601(a)(b) 27.603(a)(b)(c) 27.605(a) 27.607(a)(b) 27.609(a)(b) 27.610(a)(b)(1)(d) 27.611(a)(b)(c) 27.613(a)(b)(c)(d) 27.619(a)(b)(1) 27.625(a) 27.671(a)(b) 27.672(a)(b)(c) 27.674 27.675(a)(b)(c) 27.681(a) 27.683(a)(b)(c) 27.685(a)(b)(c)(e)(f) 27.771(a)(b)(c) 27.773(a)(1)(b) 27.777(a)(b) 27.779(a) 27.853(a) 27.863(a)(b)(3)(4) 27.865(c)(5)(e) 27.1301(a)(b)(c)(d) 27.1309(a)(b)(c)(d) 27.1316(a) 27.1317(a)(b)(c) 27.1321(a)(c)(d) 27.1322(a)(b)(c)(d) 27.1329(a)(c)(d)(e)(f) 27.1351(a) 27.1357(a)(b)(c)(d) 27.1365(a)(b)(c) 27.1367(a)(b)(c) 27.1381(a)(b) 27.1501(a)(b) 27-37 27-21 27-44 27-21 27-21 Initial Initial Initial Initial Initial 27-26 27-26 27-26 27-40 27-32 Initial 27-16 27-16 27-4 Initial 27-46 Initial 27-26 Initial 27-35 Initial 27-21 27-26 27-16 Initial Initial 27-49 Initial 27-50 Initial 27-21 27-37 27-16 27-36 Initial 27-51 27-46 27-42 27-13 27-11 27-51 27-13 27-13 27-35 Initial Initial 27-14 ----END---- 27.1503(a)(b) 27.1523(a)(b)(c) 27.1525 27.1527 27.1529 27.1541(a)(b) 27.1555(a)(d)(2) 27.1581(a)(b)(d) 27.1583(e)(g) 27.1585(a) Initial Initial 27-21 27-14 27-18 Initial 27-51 27-14 27-16 27-21 ## Every issue (1) - June 13, 2025: Issued, Current. [certificate](https://openairdocs.org/files/sha256/b8/a8/b8a8d8fffd98412169bc8559eeb122d8579bd4ca5ab5b3c6e5d881832d0c462f) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.