# STC SR02206SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Garmin International Inc, United States - Description: Installation of Garmin G500H Avionics Display System including GDU 620 PFD/MFD, GRS 77H AHRS, GMU 44 Magnetometer, GDC 74H Air Data Computer, and GTP 59 Temperature Probe - Applied: March 22, 2011 - Status date: August 10, 2016 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H11NM](https://openairdocs.org/tcds/H11NM) - Certificate PDF: https://openairdocs.org/files/sha256/96/9f/969f5467130201120678056f71708fc99009b6368c5c7eb62f0543d538afa26e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3958A188F8D9670F8625800C004D05AA.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR02206SE ## ADs that name it (0) None. ## Approved models (2) - Robinson Helicopter Company R44 ([TCDS H11NM](https://openairdocs.org/tcds/H11NM)) - Robinson Helicopter Company R44 II ([TCDS H11NM](https://openairdocs.org/tcds/H11NM)) ## 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. Number SR02206SE This certificate, issued to: Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062 Part 27 of the Federal Aviation Regulations. Original ProductType Certificate Number: H11NM Make: Robinson Model: R44, R44 II Description of the Type Design Change: Installation of Garmin G500H Avionics Display System including GDU 620 PFD/MFD, GRS 77H AHRS, GMU 44 Magnetometer, GDC 74H Air Data Computer, and GTP 59 Temperature Probe in accordance with Garmin Master Drawing List (MDL), 005-C0663-00, Revision 2, dated December 5, 2011 or later Federal Aviation Administration (FAA) approved revision and Rotorcraft Flight Manual Supplement (RFMS) for G500H in the Robinson R44, 190-01190-12, Revision 1, dated January 5, 2012 or RFMS for G500H in the Robinson R44 II, 190-01190-13, Revision 1, dated January 5, 2012 or later FAA-approved revisions. 1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft. 3. Rotorcraft modified by this STC must be operated in accordance with the RFMS identified above. 4. Rotorcraft modified by this STC must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) listed in the MDL identified above. 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. Date of application: March 22, 2011 Date reissued: August 10, 2016 Date of issuance: January 20, 2012 Date amended: (Signature) ODA STC Unit Administrator, ODA-240087-CE (Title) Transfer the ownership of Supplemental Type Certificate Number To: (Name of Transferee) (Address of Transferee) (Number and Street) (City, State, and ZIP Code) From: (Name of Grantor) (Print or Type) (Address of Grantor) (Number and Street) (City, State, and ZIP Code) Signature of Grantor (In Ink): U.S. GPO: 1987-763-289 Number SR02206SE Garmin International, Inc. Issued: January 20, 2012 Reissued: August 10, 2016 Amended: *Certification Basis The original certification basis for the R44, R44 II is Part 27 as shown on the Type Certificate Data Sheet, H11NM. The certification basis applied to this modification is listed below. Section Amdt Section Amdt 27.1 (a)(b) 27-37 27.1317 (b)(c) 27-42 27.2 (a)(2) 27-37 27.1321 (a)(c)(d) 27-13 27.301 All Orig. 27.1322 All 27-11 27.303 Orig. 27.1323 (a) 27-13 27.305 All Orig. 27.1325 (a) 27-13 27.307 (a) 27-26 27.1327 (a) 27-13 27.337 All 27-26 27.1351 (a) 27-13 27.561 (a)(b)(3)(c) Orig. 27.1357 (a)(b)(c)(d) 27-13 27.601 (a)(b) Orig. 27.1365 All 27-35 27.603 All 27-16 27.1367 All Orig. 27.605 (a) 27-16 27.1381 All Orig. 27.607 (a) 27-4 27.1501 All 27-14 27.609 All Orig. 27.1523 All Orig. 27.610 All 27-37 27.1525 27-21 27.611 (a)(b) Orig. 27.1529 27-18 27.613 All 27-26 27.1541 All Orig. 27.771 (a) Orig. 27.1543 (b) Orig. 27.773 (a)(1)(b) Orig. 27.1545 All 27-16 27.777 All Orig. 27.1555 (a) 27-21 27.785 (a)(b)(1)(e) 27-21 27.1559 27-21 27.853 (a) 27-37 27.1581 (a)(b)(d) 27-14 27.1301 (a)(b)(c)(d) Orig. 27.1583 (d)(e) 27-16 27.1303 All Orig. 27.1585 (a) 27-21 27.1309 (a)(c) 27-46 -------- -------- ------------------------------------------------END------------------------------------------------ ## Every issue (2) - August 10, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/9f/969f5467130201120678056f71708fc99009b6368c5c7eb62f0543d538afa26e) - January 20, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/fb/b7/fbb75afa3755ef510f5b2a0c4234f2dc68bf209a305e1da9c5623e4bd8d2ebeb) --- 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.