# STC SR02360LA - Type: Supplemental type certificate - Status: Current, Issued - Holder: Air Evac EMS Inc., United States - Description: Installation of the Honeywell Bleed-Air Driven Environmental Control System (ECS) in accordance with the FAA approved Air Evac Lifeteam s Master Drawing List No. 10010-01005-MDL Revision C dated July 25, 2011 or later FAA approved revision, Instructions for Continued Airworthiness No. 10010-01005-ICA Revision A dated June 20, 2011 or later FAA approved revision and Rotorcraft Flight Manual Supplement No. 10010-01005-FMS Revision IR approved on August 26, 2011 or later FAA approved revision. - Applied: December 11, 2008 - Status date: August 29, 2011 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/03/9e/039e032d78353463606123712d9ba17109473b6e65381da44aa901ab764d44cd - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E7F53EA646D492EA86257906006B4C29.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR02360LA ## ADs that name it (0) None. ## Approved models (3) - Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) ## 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. This Certificate issued to Air Evac EMS Inc. 306 Davis Drive West Plains, Missouri 65775 Part 27* of the Federal Aviation Regulations. *Certification basis is set forth on Continuation Sheet. Original Product Type Certificate Number : H2SW Make: Bell Model: 206L-1, 206L-3, and 206L-4 Description of Type Design Change: Installation of the Honeywell Bleed-Air Driven Environmental Control System (ECS) in accordance with the FAA approved Air Evac Lifeteam’s Master Drawing List No. 10010-01005-MDL Revision “C” dated July 25, 2011 or later FAA approved revision, Instructions for Continued Airworthiness No. 10010-01005-ICA Revision “A” dated June 20, 2011 or later FAA approved revision and Rotorcraft Flight Manual Supplement No. 10010-01005-FMS Revision “IR” approved on August 26, 2011 or later FAA approved revision. Limitations and Conditions: This 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. A copy of this STC must be included in the permanent records of the modified aircraft. 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 : December 11, 2008 Date of issuance : August 29, 2011 ( Signature) Manager, Cabin Safety, Mechanical and Environmental Systems Branch Los Angeles Aircraft Certification Office ( 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 1987-763-28 Number SR02360LA Certification Basis: The certification basis for this modification met 14 CFR part 27 as follows: 14 CFR part 27 Amendment 27-0 through Amendment 27-28 with Compartment Interiors at Amendment 27-37: 14 CFR part 27 Amendment 0: 27.1, 27.301, 27.303, 27.305(a), 27.601(a), 27.611, 27.771(a)(c), 27.773(a)(1)(b), 27.777, 27.831, 27.1301, 27.1365, 27.1367, 27.1381, 27.1541, 14 CFR part 27 Amendment 2: 27.1191(d)(e)(f), 27.1461 14 CFR part 27 Amendment 11: 27.1322(b)(c)(d), 14 CFR part 27 Amendment 13: 27.1351(a)(b)(1)(ii), 27.1357, 14 CFR part 27 Amendment 14: 27.29(a), 27.1043(a)(1)(2)(4)(b)(c), 27.1501(b), 27.1581(a)(b)(d), 14 CFR part 27 Amendment 16: 27.603, 27.605(a), 14 CFR part 27 Amendment 18: 27.1529, Appendix A to Part 27: A27.1, A27.2, A27.3, 14 CFR part 27 Amendment 21: 27.1309(a)(c), 27.1555(a), 27.1585(a), 27.1587, 14 CFR part 27 Amendment 23: 27.859(b)(h), 27.901(a)(3)(b)(1)(2)(5), 27.1041, 27.1045(b)(c), 27.1141(d) 14 CFR part 27 Amendment 24: Appendix A to Part 27: A27.4, 14 CFR part 27 Amendment 25: 27.561(b)(c), 14 CFR part 27 Amendment 26: 27.307(a), 27.337, 27.613, and 14 CFR part 27 Amendment 37: 27.853(a). -END- ## Every issue (1) - August 29, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/03/9e/039e032d78353463606123712d9ba17109473b6e65381da44aa901ab764d44cd) --- 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.