# STC SR09502RC - Type: Supplemental type certificate - Status: Current, Amended - Holder: Air Methods LLC, United States - Description: Installation of Air Methods Corporation Emergency Medical System and Avionics Package - Applied: May 13, 2014 - Status date: June 23, 2026 - Product: Aircraft, Rotorcraft - Certification basis: Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/2e/9f/2e9f7fca2048fb73bf326858ceef0c0451fc65e71ca0fcb81638822995c9af9c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191076313220260731140303.0001 - DRS record last changed: July 31, 2026 - Page: https://openairdocs.org/stc/SR09502RC ## ADs that name it (0) None. ## Approved models (1) - Airbus Helicopters EC130T2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR09502RC This certificate issued to: Air Methods, LLC 5500 South Quebec Street Suite 300 Greenwood Village, CO 80111 Part 27 of Title 14 of the Code of Federal Regulations Original Product Type Certificate Number: HOEU Make: Airbus Helicopters Description of Type Design Change: Model: EC130T2 Installation of Air Methods Emergency Medical System and Avionics Package in accordance with the Air Methods Master Drawing List No. 781-9000, Revision A, dated 5/21/2015, or later FAA approved revision; Rotorcraft Flight Manual Supplement (RFMS) number identified on Sheet 3; Description of Type Design Change: continued on Page 3 of 4) Limitations and Conditions: 1. The installer must determine whether this design change is compatible with previously approved modifications. Limitations and Conditions: continued on Page 3 of 4) Date of Application: 05/13/2014 Date Reissued: 01/15/2015 03/04/2015 Date of Issuance: 01/09/2015 Date Amended: 05/27/2015 06/23/2026 see continuation sheet for additional dates By Direction of the Administrator Digitally signed by JOE BOOKER CARRIER !!! Signature: Make: 2026.06.23 15:13:56 -06'00' Title: Joe B. Carrier, ODA administrator Air Methods, LLC, ODA-635841-NM United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR09502RC Effective Date: 06/23/2026 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR09502RC To (Name and address of transferee): The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STO holder. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: _ SR09502RC Effective Date: 06/23/2026 Description of Type Design Change: (Continued from Page 1): and Instructions for Continued Airworthiness (ICA) identified on Sheet 3. Rotorcraft Flight Manual Supplements) (RFMS): - EMS Systems, 080-0621, Revision A, dated 5/1/2015, or later FAA approved revision. - Avionic Systems, 080-0622, Revision A, dated 5/12/2015, or later FAA approved revision. - Aft Flooring, 080-0623, Revision A, dated 5/19/2015, or later FAA approved revision. Instructions for Continued Airworthiness (ICA): - EMS Systems, 050-0621, Revision B, dated 4/29/2015, or later FAA accepted revision. - Avionic Systems, 050-0622, Revision B, dated 5/11/2015, or later FAA accepted revision. - Aft Flooring, 050-0623, Revision A, dated 5/11/2015, or later FAA accepted revision. Limitations and Conditions: (Continued from Page 1): 2. 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. 3. A copy of this certificate and the appropriate FAA approved RFMS must be maintained as part of the permanent records for the modified rotorcraft. 4. A copy of the FAA accepted Instructions for Continued Airworthiness (ICA) must be made available to the operator at the time of installation. 5. Rotorcraft modified under this STC are required to have an approved Environmental Control System (ECS) installed on the rotorcraft. 6. The FAA approved Garmin AML STC SR02120SE must be installed as part of this STC. 7. The FAA approved AHI STC SR09497RC-D must be installed as part of this STC. 8. This STC requires the installation of a 200 amp generator. 9. This STC is applicable to all serial numbers for the Airbus Helicopters Model EC130T2. 10. Carry-on equipment (such as isolettes and medical portable electronic devices) may require FAA approval. Airworthiness considerations such as structural, electrical, electrical loads, electromagnetic compatibility, flammability, passenger compartment interior compliance, and operator considerations have not been approved for carry-on equipment. The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR09502RC Effective Date: 06/23/2026 Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Airbus Helicopters Model EC130T2 installation of Air Methods Emergency Medical System and Avionics Package is as follows: a. The type certification basis for Airbus Helicopters Model EC130T2 is shown on TCDS HEU for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, May 13, 2014, is based upon part 27 as amended by Amendment 27-32. Based on 14 CPR §§ 21.115 and 21.101, and the FAA policy for significant/not significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the latest amendment level (to match Garmin AML STC SR02120SE) - 14 CFR 27.1 (b) at Amdt 27-37 - 14 CFR 27.610(a)(b)(c)(d) at Amdt 27-46 - 14 CFR 27.1309(a)(c) at Amdt 27-46 - 14 CFR 27.1316(a)(b) at Amdt 27-46 - 14 CFR 27.1365 at Amdt 27-35 Regulations at an intermediate amendment level -NONE Regulations at the amendment level in TCDS HEU -ALL - - - - END- - ## Every issue (2) - June 23, 2026: Amended, Current. [certificate](https://openairdocs.org/files/sha256/2e/9f/2e9f7fca2048fb73bf326858ceef0c0451fc65e71ca0fcb81638822995c9af9c) - March 4, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/21/8a/218ad532e785f81946bfe28b799a547e260a400de6d540181a3e73579676689c) --- 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.