STC SH5815SW

Number SH5815SW

This certificate, issued to Soloy, LLC.

450 Pat Kennedy Way, SW Olympia, WA 98501-7298 Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H9EU Make: Eurocopter France (Aerospatiale, S.N.I.A.S.)

Model: AS-350B, AS-350BA and AS-350D

Description of the Type Design Change: Installation of Honeywell LTS 101-600A-3 or LTS 101-600A-3A engine with or without torque limiter in accordance with Soloy Drawing List 921-100, Revision A, dated March 23, 2007, or later FAA approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate 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 shall give the other person written evidence of that permission.

Date of application: May 3, 1984 Date reissued: August 1, 1997; December 13, 1999 December 22, 2004 Date of issuance: October 1, 1984 Date amended: December 10, 1986 Rev. 3;

December 22, 2004; June 15, 2005, May 14, 2007

__Original signed by Mike Pasion (Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

Number SH5815SW

Soloy, LLC Reissued: August 1, 1997; December 13, 1999, December 22, 2004 Amended: December 10, 1986 Rev. 3; December 22, 2004; June 15, 2005, May 14, 2007

Limitations and Conditions: (cont’d)

1. FAA approved Rotorcraft Flight Manual Supplement # 350FMS-020, Revision 3, dated February 17, 2005, or later FAA approved revision is required.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

- END -

FAA FORM 8110-2- 1 (10-69)