STC SR03704NY

IMPORT SR03704NY AIR AMBULANCE TECHNOLOGY GmbH 5282 RANSHOFEN, AUSTRIA 27 Title 14 Code of Federal Regulations H88EU AIRBUS HELICOPTERS DEUTSCHLAND GmbH (AHD) *See attached FAA Approved Model List (AML) No. SR03704NY for a list of approved aircraft models and applicable airworthiness regulations.

1. Installation of Air Ambulance Equipment (EMS config) and VIP Interior (VIP config) must be in accordance with Air Ambulance Technology Master Data List as listed on FAA AML No. SR03704NY.

2. Aircraft is to be maintained in accordance with Air Ambulance Technology Instructions for Continued Airworthiness as listed on FAA AML No. SR03704NY.

(See Description of Type Design Change Continued on Page 3 of 3)

1. The installer must determine whether this design change is compatible with previously approved modifications.

(See Limitations and Conditions Continued on Page 3 of 3) April 5, 2016 May 25, 2016 February 14, 2024 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT SR03704NY 3

IMPORT SR03704NY Date Amended: February 14, 2024

Description of Type Design Change (continued):

3. Aircraft is to be operated in accordance with Air Ambulance Technology Flight Manual Supplement documentation as listed on FAA AML No. SR03704NY.

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 AML No. SR03704NY, must be maintained as part of the permanent records for the modified aircraft.

4. The Incubator installation referenced by CMM-EC135-AAT13 is not a part of this approval.

5. The aircraft must be operated in accordance with the “Limitations” section of Air Ambulance Technology Flight Manual Supplement FMS AAT 18, Rev. 7, dated March 2021 and/or FMS-EC135-EMS-000 Rev. 2, dated February 2021, or later EASA approved revisions.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for aircraft listed in FAA AML No. SR03704NY are as follows:

a. The type certification basis is shown on TCDS H88EU for parts not changed or not affected by the change.

b. The type certification basis is shown on TCDS H88EU for parts changed or affected by the change.

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