STC SR04539NY

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance and Airworthiness Division Aircraft Certification Service IMPORT SR04539NY Boost Human External Cargo Systems Inc.

1476 20th Street East North Vancouver, British Columbia Canada V7J 1M8 27 Federal Aviation Regulations.

H3WE 369D, 369E, 369F, 369FF, 500N

1. Installation of the Human External Cargo (HEC) System must be in accordance with Boost Human External Cargo Systems Inc. Document Control List DCL1025-1, Revision 3, Transport Canada Civil Aviation (TCCA) approved on April 17, 2020, or later TCCA approved revision.

2. Operation must be in accordance with Boost Human External Cargo Systems Inc. Rotorcraft Flight Manual Supplement FMS1025.90 Revision 2, TCCA approved on October 01, 2020 or later TCCA approved revision.

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

1. Airworthiness Limitation contained in Chapter 4 of Boost Human External Cargo System Inc. Supplemental Instructions for Continued Airworthiness ICA1025.91 Revision 2, dated April 17, 2020 and TCCA accepted on April 17, 2020 or later TCCA accepted revision.

2. Operation must be in accordance with Boost Human External Cargo Systems Inc. Rotorcraft Flight Manual Supplement FMS1025.90 Revision 2, TCCA approved on October 01, 2020 or later TCCA approved revision.

(See Limitations and Conditions Continued on Page 3 of 3) MD Helicopters Inc.

April 15, 2020 October 21,2020

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SR04539NY

FAA Form 8110-2 (5/14) Page 3 of Date of Issuance: October 21,2020 Description of Type Design Change (continued):

3. Maintenance must be in accordance with Boost Human External Cargo Systems Inc. Supplemental Instructions for Continued Airworthiness ICA1025.91 Revision 2, TCCA accepted on April 17, 2020 or later TCCA accepted revision.

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

4. 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.

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 modified MD Helicopters Inc. 369D, 369E, 369F, 369FF & 500N is as follows:

(a) For parts not changed or not affected by the change: The existing type certification basis for the aircraft model as shown on the FAA Type Certificate Data Sheet (TCDS) H3WE.

(b) For parts changed or affected by the change is TCDS H3WE in addition to:

• 14 CFR § 27.143(a),(b),(c), amendment 27-21

• 14 CFR § 27.865, amendment 27-36

• 14 CFR § 27.1301, amendment 27-0

• 14 CFR § 27.1309, amendment 27-46

• 14 CFR § 27.1322, amendment 27-11

• 14 CFR § 27.1529, amendment 27-18 ----------END----------

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