STC SR02827LA

FAA Form 8110-2 (03/21) Page 1 of ___ (See Continuation Sheet Page 3 of 3 Pages) SR02827LA Aerocraft Incorporated 5088 Hillsdale Circle, Suite B El Dorado Hills, CA 95762 the Code of Federal Regulation 27 Bell 407 H2SW Installation of Aerocraft's Bell 407 Side Pull Kit (ARC-B407SP) in accordance with FAA approved Aerocraft Inc. Master Data List, ARC-B407SP-MDL, Revision "A", dated May 23, 2024 or later FAA approved revisions and FAA approved Aerocraft Inc. Rotorcraft Flight Manual Supplement, ARC-B407SP-RFMS, Revision "IR", dated June 28, 2024 or later FAA approved revisions.

This 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. (continued) 10/11/23 7/17/24 for Manager, West Certification Branch 3

The approval of this modification applies to the above noted rotorcraft model series only. This approval is for the structural provisions of a side-mounted primary cargo hook for a 1,400 pound external load and other aspects of the external loads system have not been certified.

Installation of the Side Pull Kit requires the rotorcraft to be equipped with the Onboard Systems International Cargo Hook Kit STC No. SR01943SE or Onboard Systems Dual Cargo Hook System STC No.

SR02724LA. This STC only certifies the relocation of the cargo hook and other certification requirements for the cargo hook were approved by STC No. SR01943SE.

Additional FAA approval is required for civil external loads operations as specified in 14 CFR Part 133 or equivalent operating requirements. A copy of this STC must be included in the permanent records of the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

FAA Accepted Instructions for Continued Airworthiness, ARC-B407SP-ICA, Revision A, dated May 29 2024, or later FAA Accepted revisions must be made available to the operator at the time of installation.

A copy of this Certificate, dated July 17, 2024 or later FAA Approved revision, must be maintained as part of the permanent records for the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

Certification Basis:

Certification basis is set forth in Type Certificate Data Sheet H2SW. Compliance with the following regulations is at the specified later amendment levels:

Regulations at Amd’t (27-30): 27.29(a), 27.141, 27.143, 27.251, 27.301, 27.303, 27.305(a)(b)(1), 27.307(a),

27.337, 27.561, 27.601, 27.603, 27.605, 27.607, 27.609, 27.613, 27.625, 27.863(a)(b), 27.959, 27.1301,

27.1351(b)(1)(i)(ii), 27.1365 (a)(b)(c), 27.1435(a), 27.1505, 27.1529, 27.1541, 27.1581, 27.1583, 27.1585,

27.1589, Amd’t (27-36): 27.865(a)(b)(d)(e) 3 3