STC SR04616NY

IMPORT SR04616NY Boost Human External Cargo Systems Inc.

1476 20th Street East North Vancouver, British Columbia Canada V7J 1M8 Part 29 Title 14 Code of Federal Regulations H1SW, H4SW BELL 212, 412, 412 CF, 412 EP, 205A, 205A-1, and 205B

1. Installation of the Dual HEC Hook System Provisions is to be performed in accordance with Boost Human External Cargo Systems Inc. Master Document List (MDL) 1963-MD-001, Revision E, Transport Canada Civil Aviation (TCCA) approved on May 2, 2022, or later TCCA approved revision.

2. Maintenance is to be done in accordance with Boost Human Cargo Systems Inc. Instructions of Continued Airworthiness (ICA) 1963-CA-001, Revision C, TCCA accepted on February 3, 2022, or later (See Description of Type Design Change Continued on Page 3 of 5)

1. Airworthiness Limitations contained in Chapter 04 of Boost Human Cargo Systems Inc. ICA 1963-CA-001, Revision C, TCCA approved May 3, 2022, or later TCCA approved revision.

(See Limitations and Conditions Continued on Page 3 of 5) January 21, 2021 April 2, 2021 May 20, 2022 Anthony E. Gallo Manager, International Validation Branch (AIR-730) Compliance & Airworthiness Division Aircraft Certification Service (AIR) 5

IMPORT SR04616NY SR04616NY 5

IMPORT SR04616NY Date of Amendment: May 20, 2022 Description of Type Design Change (continued):

2. TCCA accepted revision.

3. Operation is to be done in accordance with Boost Human External Cargo Systems Inc. Rotorcraft Flight Manual Supplement (RFMS) 1963-FM-001, Revision D, TCCA approved May 2, 2022, or later TCCA approved revision for BELL models 212/412.

4. Operation is to be done in accordance with Boost Human External Cargo Systems Inc. RFMS 1963-FM-002, Revision B, TCCA approved May 2, 2022 or later TCCA approved revision for BELL models 205.

2. Limitations contained in Section 1 of Boost Human Cargo Systems Inc. RFMS 1963-FM-001, Revision D, TCCA approved May 2, 2022, or later TCCA approved revision for BELL models 212/412.

3. Limitations contained in Section 1 of Boost Human Cargo Systems Inc. RFMS 1963-FM-002, Revision B, TCCA approved May 2, 2022 or later TCCA approved revision for BELL models 205.

4. FAA STC SR02233SE (LH Pilot in Command Kits Installation) is a prerequisite for the installation of Dual HEC Hook System Provisions.

5. This does not constitute an operational approval, for using the Dual HEC Hook Systems Provisions, the operator will need approval from the Operations Regulatory Authority.

6. For Human External Cargo, approved Personnel Carrying Device System (PCDS) in accordance with FAA STC SR04615NY shall be used. Human External Cargo operations require the use of approved PCDS that have been demonstrated to be compatible with the Dual HEC Hook System. The PCDS and Dual HEC Hook System combination must fully meet 14 CFR Part 29 paragraph 29.865. Refer to Certification Basis section.

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

8. If the holder agrees to permit another person to use this certificate to alter a product, (See Limitations and Conditions Continued on Page 4 of 5) 3 5

IMPORT SR04616NY Date of Amendment: May 20, 2022 Limitations and Conditions (continued):

8. the holder must give the other person written evidence of that permission.

Certification Basis:

For BELL 205A, 205A-1, 205B Models:

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 8110.48, the certification basis for BELL Textron Inc. 205A, 205A-1, 205B is as follows:

(a) For parts not changed or not affected by the change: The type certification basis for the aircraft model as shown on the FAA Type Certificate Data Sheet (TCDS) H1SW

(b) For parts changed or affected by the change: The type certification basis for the aircraft model as shown on the TCDS H1SW with the following additional requirements:

• 14 CFR § 29.865 (c)(2) at Amendment 29-43

• 14 CFR § 29.865 (c)(4) at Amendment 29-43

• 14 CFR § 29.865 (c)(5) at Amendment 29-43

• 14 CFR § 29.865 (c)(6) at Amendment 29-43

• 14 CFR § 29.865 (d) at Amendment 29-43

For BELL 212, 412, 412 CF, 412 EP Models:

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 8110.48, the certification basis for BELL Textron Inc. 212, 412, 412 CF, 412 EP is as follows:

(a) For parts not changed or not affected by the change: The type certification basis for the aircraft model as shown on the FAA Type Certificate Data Sheet (TCDS) H4SW

(b) For parts changed or affected by the change: The type certification basis for the aircraft model as shown on the TCDS H4SW with the following additional requirements:

• 14 CFR § 29.865 (c)(2) at Amendment 29-43

• 14 CFR § 29.865 (c)(4) at Amendment 29-43

• 14 CFR § 29.865 (c)(5) at Amendment 29-43 (See Certification Basis Continued on Page 5 of 5) 4 5

IMPORT SR04616NY Date of Amendment: May 20, 2022 Certification Basis (continued):

• 14 CFR § 29.865 (c)(6) at Amendment 29-43

• 14 CFR § 29.865 (d) at Amendment 29-43 ----------END---------- 5 5