# STC SH5815SW - Type: Supplemental type certificate - Status: Current, Amended - Holder: Soloy LLC, United States - Description: 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. - Applied: May 3, 1984 - Status date: May 14, 2007 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) - Certificate PDF: https://openairdocs.org/files/sha256/ca/d1/cad1dcccfc2d8e6fded72b1b977faf801547d3404aafa901a3cc54ac1faeb2e0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/58BCFB7853512E7A8625794B0055467C.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SH5815SW ## ADs that name it (0) None. ## Approved models (3) - Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) - Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. 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)** ## Every issue (2) - May 14, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ca/d1/cad1dcccfc2d8e6fded72b1b977faf801547d3404aafa901a3cc54ac1faeb2e0) - June 15, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/96/d8/96d8395f9eb158a79508f32343922fdc8ab023da45d909b77fa559993c8c0367) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.