# STC SA00234SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Fabrication of Kenmore Air Harbor, Inc., wing strut fitting - Applied: November 22, 1994 - 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/sha256/5a/5b/5a5b35503b9a5b1a498996f0bdc44da261aa1c9e14580bfb9ba52182d89ae013 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F372C701D36439BD862585CF003F3075.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00234SE ## ADs that name it (0) None. ## Approved models (2) - Viking Air Limited DHC-2 Mk.I ([TCDS A-806](https://openairdocs.org/tcds/A-806)) - Viking Air Limited DHC-2 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 SA00234SE This certificate, issued to Kenmore Air Harbor, LLC. 6321 NE 175th Street Kenmore, WA 98028 Part 10 of the Civil Air Regulations. Original ProductType Certificate Number: A-806 Make: Viking Air Limited Model: DHC-2 Mk. I, DHC-2 Mk. III Description of the Type Design Change: Fabrication of Kenmore Air Harbor, Inc., wing strut fitting in accordance with Kenmore Air Harbor, Inc. Drawing KAC2W1097A, dated April 22, 2013. Installation of Kenmore Air Harbor, Inc., wing strut fitting in accordance with Kenmore Air Harbor, Inc. Installation Instructions KI23423, Revision A, dated April 22, 2013, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only with a maximum gross weight of 5370 pounds. This approval should not be extended to other aircraft of this model 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 aircr aft. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. This supplemental type certificate is not applicable for use as an alternative method of compliance to Airworthiness Directive (AD) 2007 -12-13. All requirements of AD 2007-12-13 remain applicable. 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: November 22, 1994 Date reissued: April 5, 2019 Date of issuance: September 15, 1995 Date amended: January 21, 2014 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 (3) - April 5, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5a/5b/5a5b35503b9a5b1a498996f0bdc44da261aa1c9e14580bfb9ba52182d89ae013) - January 21, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/af/73/af73a7f6dd8cd507e5d57a7e5b5338482aa6b6220202bdbb53a06106c29981e3) - September 15, 1995: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/19/12/1912037dbba198003e635a3adae10f19816fd122b96af53d5b3ac63cbcb18d56) --- 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.