# STC SR00592DE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Air Methods Corporation, United States - Description: Installation of an Emergency Medical System (EMS) interior. - Applied: November 4, 2005 - Status date: June 22, 2022 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU) - Certificate PDF: https://openairdocs.org/files/sha256/38/46/3846efa4b434f895d56c660ba43cc2b55e9c90835a7419c8f4170e3c6124c292 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1331A416DAE36E99862588A7004BFFD0.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00592DE ## ADs that name it (1) - [AD 2019-10-51](https://openairdocs.org/ad/2019-10-51): Fuselage main frame · Airbus Helicopters Deutschland MBB-BK 117 C-2. Effective Sep 19, 2019. Cited in the text ## Approved models (1) - Eurocopter Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) ## 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: SR00592DE Air Methods Corporation 5500 South Quebec Street, Suite 300 Greenwood Village, CO 80111 29 Code of Federal Regulations H13EU Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 Installation of an Emergency Medical Systems (EMS) Interior in accordance with Configuration Control Drawing (CCD) 779-9262, Revision A, Dated 12/09/2020 or later FAA-approved revision and Master Drawing List 771-9040, Revision R, Dated 06/08/2022 or later FAA-approved revision; This change has been introduced in order to comply with Airworthiness Directive (AD) 2019-10-51 related to Airbus Helicopters Deutschland GmbH Model MBB-BK 117 C-2. 1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. (see Continuation Sheet 3) November 4, 2005 April 19, 2006 12/19/2007; 12/22/2007; 4/26/2012; 10/03/2018; 6/22/2022 Luke Walker Acting Manager, Denver ACO Branch Compliance and Airworthiness Division 3 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: SR00592DE SR00592DE 3 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: SR00592DE Description of Type Design Change Continued: Operated in accordance with Rotorcraft Flight Manual Supplement (RFMS) number 080-0523, Rev F, FAA approved 8/13/2021, or later FAA approved revision; Maintained in accordance with Instructions for Continued Airworthiness (ICA) number 050-0591, Rev G dated 5/25/2021, FAA accepted 7/8/2021, or later accepted revision. 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 FAA approved RFMS as listed above must be maintained as a part of the permanent records for the modified rotorcraft, and ICA as listed above are required for this installation. 4. Each configuration is independent and each configuration must be solely installed with respect to the type design change defined by this STC. Multiple configurations cannot be installed concurrently on a single rotorcraft. 5. This STC is applicable to all serial numbers for this Make/Model. Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant changes in FAA Order 8110.48, the certification basis for the Airbus Helicopters Deutschland GmbH Model MBB-BK 117 C-2 installation of Emergency Medical Systems (EMS) is as follows: a. The type certified basis for parts not changed or not affected by the change is shown on TCDS H13EU. b. The modification certification basis for parts changed or affected by the change since the reference date of application, November 4, 2005, is based upon part 29 as amended by Amendment 29-47. Regulations at the latest amendment level -NONE Regulations at an intermediate amendment level -NONE Regulations at the amendment level in TCDS H13EU - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - 3 3 ## Every issue (6) - June 22, 2022: Amended, Current. [certificate](https://openairdocs.org/files/sha256/38/46/3846efa4b434f895d56c660ba43cc2b55e9c90835a7419c8f4170e3c6124c292) - October 3, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/43/56/4356e25c1000476b0627c7196cfe306b594e1077a5f8007bbe2a336615397fbc) - April 26, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e5/54/e55431fd8eae83fcdde25db8fc4f1289a272bc9e411deeb5481e297cd6d5da04) - December 22, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/67/2a/672a187f6160ff47721f67c43beccd1b005d329b4167e535eda170f6d41ae278) - December 19, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f5/25/f52501c2e976fa05180e708a0efa07ee9b6b716a7e405d1784cb750ae34bd430) - April 19, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/8b/16/8b1675ccd9f5a9654595ac8a3ba9502d11a1fe1616aa98418020b301aad816e5) --- 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.