# STC SR04614NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: Alpine Aerotech LP, Canada - Description: Installation of the Garmin G500H TXi Integrated Flight Display System (IFDS) - Applied: April 2, 2020 - Status date: March 24, 2021 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/2b/6e/2b6e24841a473cea2726d4468532df8cec1b7734c284f59e8b64c33d94616830 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4BE03216E2EBDC7B862586AE005BA7B5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR04614NY ## ADs that name it (0) None. ## Approved models (1) - Bell Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) ## 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 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: IMPORT SR04614NY Alpine Aerotech LP 1260 Industrial Road West Kelowna, British Columbia V1Z 1G5 Part 29 Title 14 Code of Federal Regulations H4SW Bell 212 1. The following configurations are approved for the installation of the Garmin G500H TXi Integrated Flight Display System (IFDS): Configuration 1: Avionics Upgrade Kit (Dual G500H TXi) Configuration 2: Minimal Avionics Upgrade Kit (Single G500H TXi) (See Description of Type Design Change Continued on Page 3 of 6) 1. Airworthiness Limitations: Installation of the Garmin G500H TXi Integrated Flight Display System is limited to helicopters certified for Day/Night Visual Flight Rules (VFR) operations only. (See Limitations and Conditions Continued on Page 4 of 6) April 2, 2020 March 24, 2021 Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division Aircraft Certification Service 6 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: **IMPORT SR04614NY 6** FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: IMPORT SR04614NY Date of Issuance: March 24, 2021 Description of Type Design Change (continued): 2. The following documents are required for these installations and for the Instructions for Continued Airworthiness: Configuration 1: a. Installation of the Avionics Upgrade Kit (Dual G500H TXi) must be in accordance with Alpine Aerotech Installation Instructions AAL-280-025-001 Revision NI, Transport Canada Civil Aviation (TCCA) approved on March 31, 2020, or later TCCA approved revisions. b. Operation of the Avionics Upgrade Kit (Dual G500H TXi) must be in accordance with Alpine Aerotech Flight Manual Supplement AAL-280-025-401 Revision NI, TCCA approved on March 26, 2020, or later TCCA approved revisions. c. Maintenance of the Avionics Upgrade Kit (Dual G500H TXi) must be in accordance with Alpine Aerotech Instructions for Continuing Airworthiness AAL-280-025-701 Revision NI, dated March 23, 2020, or later TCCA accepted revisions. d. Definition of Type Design Change: Alpine Aerotech Master Data List AAL-280-024-001 Revision NI, TCCA approved on March 31, 2020, or later TCCA approved revisions. Configuration 2: a. Installation of the Minimal Avionics Upgrade Kit (Single G500H TXi) must be in accordance with Alpine Aerotech Installation Instructions AAL-280-025-002 Revision NI, TCCA approved on March 31, 2020, or later TCCA approved revisions. b. Operation of the Minimal Avionics Upgrade Kit (Single G500H TXi) must be in accordance with Alpine Aerotech Flight Manual Supplement AAL-280-025-402 Revision NI, TCCA approved on March 26, 2020, or later TCCA approved revisions. (See Description of Type Design Change Continued on Page 4 of 6) 3 6 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: IMPORT SR04614NY Date of Issuance: March 24, 2021 Description of Type Design Change (continued): 2. Configuration 2 (continued) c. Maintenance of the Minimal Avionics Upgrade Kit (Single G500H TXi) must be in accordance with Alpine Aerotech Instructions for Continuing Airworthiness AAL-280-025-702 Revision NI, dated March 23, 2020, or later TCCA accepted revisions. d. Definition of Type Design Change: Alpine Aerotech Master Data List AAL-280-024-001 Revision NI, TCCA approved on March 31, 2020, or later TCCA approved revisions. Limitations and Conditions (continued) 2. The "Limitations" section of the Alpine Aerotech Flight Manual Supplement AAL-280-025-401 Revision NI, TCCA approved on March 26, 2020, or later TCCA approved revisions is applicable as part of the Configuration 1 installation. 3. The "Limitations" section of the Alpine Aerotech Flight Manual Supplement AAL-280-025-402 Revision NI, TCCA approved on March 26, 2020, or later TCCA approved revisions is applicable as part of the Configuration 2 installation. 4. The installer must determine whether this design change is compatible with previously approved modifications. 5. 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. 6. This STC is applicable to all serial numbers for these Make-Models. (See Limitations and Conditions Continued on Page 5 of 6) 4 6 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: IMPORT SR04614NY Date of Issuance: March 24, 2021 Limitations and Conditions (continued) Certification Basis Based on title 14 Code of Federal Regulations (CFR) 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the type certification basis for the Bell 212 helicopter is as follows: a. The type certification basis for the Bell 212 helicopter as shown on Type Certificate Data Sheets (TCDS) H4SW for parts not changed or not affected by the change. b. The type certification basis for the Bell 212 helicopter for parts changed or affected by the change is TCDS H4SW in addition to: • 14 CFR Part 29.29 at Amendment 29-15 • 14 CFR Part 29.610 at Amendment 29-53 • 14 CFR Part 29.613 at Amendment 29-30 • 14 CFR Part 29.771(a) at Amendment 29-24 • 14 CFR Part 29.773(a) at Amendment 29-57 • 14 CFR Part 29.853(a) at Amendment 29-23 • 14 CFR Part 29.1303 at Amendment 29-24 • 14 CFR Part 29.1307(e) at Amendment 29-12 • 14 CFR Part 29.1309 at Amendment 29-53 • 14 CFR Part 29.1316 at Amendment 29-53 • 14 CFR Part 29.1317 at Amendment 29-49 • 14 CFR Part 29.1321 at Amendment 29-21 • 14 CFR Part 29.1322 at Amendment 29-12 • 14 CFR Part 29.1323(a) at Amendment 29-44 • 14 CFR Part 29.1325(a)(d)(e) at Amendment 29-24 • 14 CFR Part 29.1331 at Amendment 29-24 • 14 CFR Part 29.1333 at Amendment 29-24 (See Certification Basis Continued on Page 5 of 6) 5 6 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: IMPORT SR04614NY Date of Issuance: March 24, 2021 Certification Basis (continued) b. (continued) • 14 CFR Part 29.1351(a)(d) at Amendment 29-42 • 14 CFR Part 29.1355 at Amendment 29-24 • 14 CFR Part 29.1357 at Amendment 29-24 • 14 CFR Part 29.1359 at Amendment 29-42 • 14 CFR Part 29.1501 at Amendment 29-15 • 14 CFR Part 29.1529 at Amendment 29-20 • 14 CFR Part 29.1545 at Amendment 29-17 • 14 CFR Part 29.1555(a) at Amendment 29-24 • 14 CFR Part 29.1581 at Amendment 29-15 • 14 CFR Part 29.1583 at Amendment 29-24 • 14 CFR Part 29.1585 at Amendment 29-24 • Equivalent Level of Safety (ELOS) Findings have been made for title 14 Code of Federal Regulations (CFR) 29.1545 (Amdt. 29-17) Airspeed indicator, documented in ELOS Memorandum ST09373NY-R-S-1, dated December 16, 2020. ----------END---------- ## Every issue (1) - March 24, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/2b/6e/2b6e24841a473cea2726d4468532df8cec1b7734c284f59e8b64c33d94616830) --- 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.