STC SR00650DE

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SR00650DE

This certificate and the supporting data which is the bases for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: March 6, 2007 Date reissued:

Date of issuance: May 23, 2007 Date amended: January 30, 2012 By direction of the Administrator

Kreg R. Voorhies, ODA administrator (Signature) ODA-635841-NM Air Methods Corporation (Title)

FAA FORM 8110-2 (10-68) P AGE 1 OF 3

This certificate, issued to Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Part 29* of the Federal Aviation Regulations. *See Continuation Page 3 Original ProductType Certificate Number: H13EU Make: Eurocopter Deutschland GmbH (ECD) Model: MBB-BK 117 C-2 Description of the Type Design Change:

Installation of an Instrument Panel, Pedestal and Optional Avionics Package in accordance with Air Methods Corporation Master Drawing List as defined by the configuration identified as follows:

Configuration Master Drawing List Standard 771-9046, Revision “-“ da ted 1/14/2008, FAA approved 1/16/2008** Geisinger 771-9062, Revision “-“ da ted 4/28/2008, FAA approved 5/13/2008** Mayo 771-9064, Revision “-” date d 12/23/2008, FAA approved 12/24/2008** Geisinger, Single DME 771-9062-001, Revision IR dated 1/25/2012 , FAA approved 1/30/2012** ** Or later FAA approved revision.

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.

2. 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.

(Limitations and Conditions continued on page 3 of 3)

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SR00650DE

FAA FORM 8110-2 (10-68) P AGE 3 OF 3

3. A copy of this Certificate and FAA approved Rotorcraft Flight Manual Supplement (RFMS) must be maintained as part of the permanent records for the modified rotorcraft, and Instructions for Continued Airworthiness (ICA) are required for this installation; configuration specific RFMS and ICA as defined by the configuration identified as follows:

Configuration RFMS ICA Standard (MDL 771-9046) 080-0389, Revision IR, FAA approved 1/16/2008** 050-0434, Revision IR dated 11/6/2007, FAA accepted 1/9/2008***, and 050-0458, Revision IR dated 11/26/2007, FAA accepted 1/9/2008*** Geisinger (MDL 771-9062) 080-0415, Revision IR, FAA approved 5/13/2008** 050-0434, Revision A dated 2/29/2008, FAA accepted 3/12/2008 ***, and 050-0458, Revision A dated 2/29/2008, FAA accepted 3/14/2008*** Mayo (MDL 771-9046) 080-0444, Revision IR, FAA approved 12/22/2008** 050-0434, Revision B dated 11/7/2008, FAA accepted 12/17/2008***, and 050-0458, Revision B dated 11/5/2008, FAA accepted 12/9/2008*** Geisinger, Single DME (MDL 771-9062-001 ) Refer to Master Data Index (MDI) 771-9063-001, Revision IR dated 1/25/2012, FAA approved 1/30/2012**, for configuration specific RFMS and ICA.

** Or later FAA approved revision *** Or later FAA accepted revision

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.

Certification Basis:

The certification basis for this modification is as follows:

In accordance with Type Certificate Data Sheet, H13EU, revision 12 dated November 14, 2007;

MBB-BK 117 C-2 Certification Basis;

FAR 21.29 and FAR 29 effective Feb. 1, 1965 plus Amendments 29-1 through 29-40 with the following exeptions.

FAR 29.903 at Amendment 29-26 FAR 29.923 at Amendment 29-26 FAR 29.927 at Amendment 29-17 FAR 29.547 at Amendment 29-16 FAR 29.571 at Amendment 29-16 FAR 29.863 at Amendment 29-16 FAR 29.901(c) at Amendment 29-16 FAR 29.917 at Amendment 29-16 FAR 29.1011 at Amendment 29-16 FAR 29.1019(a) at Amendment 29-16 FAR 29.1021 at Amendment 29-16 FAR 29.1163 at Amendment 29-16 FAR 29.1181 at Amendment 29-16 FAR 29.1183 at Amendment 29-16 FAR 29.1189 at Amendment 29-16 FAR 29.1309(b),(d),(e) at Amendment 29-16 FAR 29.1521 at Amendment 29-16 and the following FAR’s that revert to the original Amendment 29-16 certification basis and were not codified at that time FAR 29.610(d)(4) FAR 29.631 FAR 29.1027 FAR 29.1305(a)(21 and (23) FAR 29.1337(e) FAR Part 36 Appendix H at Amendment 36-22 Equivalent level of safety fingings for FAR 29.807(a)(4), FAR 29.1303(a) and (j), FAR 29.1549(b), and 29.1151(b)

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U.S. GPO: 1987-763-289

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