# STC SA01131SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Replace existing Strut Assembly - Front Fuselage - Applied: October 7, 2002 - Status date: April 5, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806) - Certificate PDF: https://openairdocs.org/files/sha256/3f/03/3f03bd5ebc8855609c507e687666fc74393d25e065ab61d37381948c5fef4f7b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/52B2B613D914781F862585CF003F31E8.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01131SE ## ADs that name it (0) None. ## Approved models (3) - de Havilland Inc. (Canada) DHC-2 (L-20A) MK.I ([TCDS A-806](https://openairdocs.org/tcds/A-806)) - de Havilland Inc. (Canada) DHC-2 (L-20A) MK.II ([TCDS A-806](https://openairdocs.org/tcds/A-806)) - de Havilland Inc. (Canada) DHC-2 (L-20A) MK.III ([TCDS A-806](https://openairdocs.org/tcds/A-806)) ## 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 SA01131SE This certificate, issued to Kenmore Air Harbor, LLC. 6321 NE 175th Street Kenmore, WA 98028 Part 3 of the Civil Air Regulations. Original ProductType Certificate Number: A-806 Make: DeHavilland Model: DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III Description of the Type Design Change: Replace existing Strut Assembly – Front Fuselage with Kenmore Strut Assembly – Front Fuselage KAC2FS3281(L.H.) and/or KAC2FS3282(R.H.), manufactured in accordance with Kenmore assembly drawing KAC2FS3281, Revision New, dated September 15, 2002, or later FAA approved revisions, and installed in accordance with installation procedures described in Airworthiness Directive (AD) 2002-14-28, dated July 15, 2002, or later FAA approved revisions. Installation of Kenmore Front Fuselage Strut Assemblies KAC2FS3281(L.H.) and/or KAC2FS3282(R.H) are an approved alternate method of compliance to AD 2002-14-28, dated July 15, 2002, or later FAA approved revisions. Limitations and Conditions: Kenmore replacement struts must be maintained in accordance with paragraph (d)(1) or (d)(2) of AD 2002-14-28, dated July 15, 2002. The approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft on which 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: October 7, 2002 Date reissued: April 5, 2019 Date of issuance: October 15, 2002 Date amended: FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator (Signature) Acting Manager, Seattle ACO Branch (Title) Transfer the ownership of Supplemental Type Certificate Number to (Name of Transferee) (Address of Transferee) (Number and Street) (City, State, and ZIP Code) from (Name of Grantor) (Print or Type) (Address of Grantor) (Number and Street) (City, State, and ZIP Code) Signature of Grantor (In Ink): U.S. GPO: 1987-763-289 ## Every issue (2) - April 5, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3f/03/3f03bd5ebc8855609c507e687666fc74393d25e065ab61d37381948c5fef4f7b) - October 15, 2002: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/8a/22/8a229a7d1a05a88ebf1370759ae626304ec5a808e817a89b034dd67739cb3eb1) --- 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.