STC SR00617DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00617DE

November 28, 2006 Date Reissued:

Date of Issuance: May 24, 2007 Date Amended:

September 28, 2007; February 23, 2012; March 16, 2017 By Direction of the Administrator

Signature

Title Robert C. Lazaroff, ODA administrator Air Methods Corporation, ODA-635841-NM

FAA Form 8110-2 (5/14) Page 1 of 4

This certificate, issued to: Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Part 27* of the Federal Aviation Regulations. *See Page 4

Original Product – Type Certificate Number: Make: Airbus Helicopters H9EU Model: AS350B2, AS350B3 Description of Type Design Change:

Installation of a Reduced Instrument Panel, Pedestal, Optional Avionics System, and Night Vision Imaging Systems in accordance with the Air Methods Corporation Master Drawing Lists as defined by the configuration identified in the Configuration Table below.

Configuration Table Configuration Master Drawing List Standard AS350B2 Pre-Mod 073273/4 741-9200 (Instrument Panel), Revision “-“ dated 5/7/2007, FAA approved 5/24/2007**, and 741-9202 (Avionics), Revision “-“, dated 5/7/2007, FAA approved 5/7/2007**, and 741-9204 (NVIS), Revision “-“ dated 5/7/2007, FAA approved 5/24/2007** Standard AS350B2 Post-Mod 073273/4 741-9200 (Instrument Panel), Revision B dated 6/13/2007, FAA approved 6/13/2007**, and 741-9206 (Avionics), Revision “-“ dated 9/7/2007, FAA approved 9/28/2007**, and 741-9204 (NVIS), Revision A dated 9/25/2007, FAA approved 9/28/2007** Standard AS350B3 Post-Mod 073273/4 741-9208 (Instrument Panel), Revision “-“ dated 9/5/2007, FAA approved 9/28/2007**, and 741-9206 (Avionics), Revision “-“ dated 9/7/2007, FAA approved 9/28/2007**, and 741-9204 (NVIS), Revision A dated 9/25/2007, FAA approved 9/28/2007** Configuration 001, AS350B3 741-9208-001 (Instrument Panel), Revision “IR“ dated 2/10/2012, FAA approved 2/23/2012**, and 741-9206- 001 (Avionics), Revision “IR“ dated 1/27/2012, FAA approved 2/23/2012**, and 741-9204 (NVIS), Revision D dated 5/24/2011, FAA approved 6/16/2011** per Light Source Control Drawing 749-1448-001, Revision “-“ dated 6/9/2010** AS350B2/B3 NVIS Modification 741-9204 MDL, NVIS Modification AS350, Revision “-“, FAA approved 5/7/2007** ** Or later FAA approved revision.

FAA Form 8110-2 (5/14) Page 2 of 4

Transfer the ownership of Supplemental Type Certificate Number: SR00617DE

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00617DE

FAA Form 8110-2 (5/14) Page 4 of 4

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.

3. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft.

4. FAA approved Rotorcraft Flight Manual Supplement (RFMS) is required. For configuration specific RFMS refer to table below.

5. FAA accepted Instructions for Continued Airworthiness (ICA) must be made available to the operator at the time of installation. For configuration specific ICA refer to table below.

Configuration RFMS ICA Standard AS350B2 Pre-Mod 073273/4 080-0370, Revision IR, FAA approved 5/23/2007** 050-0416 (Inst Panel, Pedestal, NVIS), Revision A dated 4/18/2007, FAA accepted 4/19/2007***, and 050-0421 (Avionics), Revision “-“ dated 4/26/2007, FAA accepted 5/24/2007*** Standard AS350B2 Post-Mod 073273/4 080-0370, Revision A, FAA approved 6/6/2007** 050-0416 (Inst Panel, Pedestal, NVIS), Revision A dated 4/18/2007, FAA accepted 4/19/2007***, and 050-0421 (Avionics), Revision A dated 6/24/2007, FAA accepted 7/19/2007*** Standard AS350B3 Post-Mod 073273/4 080-0371, Revision IR, FAA approved 10/7/2007** 050-0416 (Inst Panel, Pedestal, NVIS), Revision A dated 4/18/2007, FAA accepted 4/19/2007***, and 050-0421 (Avionics), Revision A dated 6/24/2007, FAA accepted 7/19/2007*** Configuration 001, AS350B3 080-0371, Revision E dated 2/10/2012, FAA approved 2/23/2012** 050-0416 (Inst Panel, Pedestal, NVIS), Revision H dated 7/27/2010 , FAA accepted 7/29/2010***, and 050-0421 (Avionics), Revision J dated 11/14/2011, FAA accepted 2/10/2012*** ** Or later FAA approved revision *** Or later FAA accepted revision

6. Each configuration is independent and each configuration must be individually installed with respect to the type design change defined by this STC. Multiple configurations or parts thereof cannot be installed concurrently on a single rotorcraft.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00617DE

FAA Form 8110-2 (5/14) Page 4 of 4

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 AS350B2 and AS350B3 installation of Reduced Instrument Panel, Pedestal, Optional Avionics System, and Night Vision Imaging Systems is as follows:

a. The type certification basis for Airbus Helicopters AS350B2 and AS350B3 is shown on TCDS H9EU 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, November 28, 2006, is based upon part 27 as amended by Amendment 27-40. 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 this modification was determined to be:

Regulations at the latest amendment level -NONE

Regulations at an intermediate amendment level For A/C incorporating Airbus Helicopters mod. OP3369 (2370 kg/5225 lb mass extension) the following 14 CFR Part 27 Amendments 27-1 through 27-40, are replacing the same requirement from the certification basis: 27 §1; §21; §25; §27; §33; §45; §51; §65; §71; §73; §75; §79; §141; §143; §173;

§175; §177; §241; §301; §303; §305; §307; §309; §321; §337; §339; §341; §351; §471; §473; §501;

§505; §521; §547; §549; §563(b); §571; §602; §661; §663; §695; §723; §725; §727; §737; §751; §753;

§801(b)(d); §927(c); §1041; §1043; §1045; §1301; §1501; §1519; §1529; §1581; §1583; §1585; §1587;

§1589.

For AS350B3 A/C incorporating Airbus Helicopters mod. OP-4605 (installation of a fuel system improving crashworthiness), 14 CFR 27.561(c) at Amendment 27-32 replaces the same requirements from the TCDS for the following elements of the fuel tank lower structure affected by this modification:

cradles, longitudinal beams, X-stops and rods.

Regulations at the amendment level in TCDS H9EU (27-1 through 27-10, plus FAA Special Conditions No. 27-79-EU-23, dated August 13, 1977) -All regulations not listed above at intermediate amendment level

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