# STC SA02542SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Installation of a Lower Fuselage Tie Bar Assembly - Applied: February 27, 2017 - Status date: April 5, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A-815](https://openairdocs.org/tcds/A-815) - Certificate PDF: https://openairdocs.org/files/sha256/d5/84/d584cb0965c8257a1175377ec149ae36183722ae5b1f0d24c20977cc6621b096 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0F06B0BF3A86FC4862585CF003F3759.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02542SE ## ADs that name it (0) None. ## Approved models (1) - Viking Air Limited DHC-3 ([TCDS A-815](https://openairdocs.org/tcds/A-815)) ## 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 SA02542SE This certificate, issued to Kenmore Air Harbor, LLC. 6321 NE 175th Street Kenmore, WA 98028 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: A-815 Make: Viking Air Limited Model: DHC-3, U-1A (See TCDS note #4) Description of the Type Design Change: Installation of a Lower Fuselage Tie Bar Assembly in accordance with Installation Instructions Document KAC3FS14-INSTL, Revision --, dated February 15, 2017, or later Federal Aviation Administration (FAA) approved revision. Manufactured in accordance with Master Drawing List KAC3FS14-MDL, Revision --, dated February 15, 2017, or later FAA-approved revision. Maintained in accordance with Instructions for Continued Airworthiness (ICA) KAC3FS14-300, Revision --, dated February 15, 2017, or later FAA-accepted revision. 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 this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will int roduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and the ICA 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: February 27, 2017 Date reissued: April 5, 2019 Date of issuance: August 2, 2017 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/d5/84/d584cb0965c8257a1175377ec149ae36183722ae5b1f0d24c20977cc6621b096) - August 2, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/6e/40/6e40bf84463dd34fb506d7c623bb785b0b3936312cece19a3f80eb882513c655) --- 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.