# STC SA02250SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Installation of a Cleveland Wheel and Brake Kit Number 199-92, - Applied: May 2, 2012 - Status date: April 5, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A-815](https://openairdocs.org/tcds/A-815) - Certificate PDF: https://openairdocs.org/files/sha256/4a/f5/4af55737be9b38d06da5f5a1f273683c83e8513969e908874322a5450422665d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3978273C10F5E11C862585CF003F35E6.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02250SE ## 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 SA02250SE This certificate, issued to Kenmore Air Harbor, LLC. 6321 NE 175th Street Kenmore, WA 98028 Part 3* and 10* of the Federal Aviation Regulations. * CAR 10, ICAO Annex 8, 2nd Edition (Transport Category D), and CAR 3 as amended to November 1, 1949 Original ProductType Certificate Number: A-815 Make: Viking Air Limited (formerly de Havilland) Model: DHC-3 Description of the Type Design Change: Installation of a Cleveland Wheel and Brake Kit Number 199-92, in accordance with Cleveland Wheels & Brakes Drawing 050-10100, Revision J, or later FAA-approved revision. Maintained in accordance with Kenmore Air Harbor, Inc. Instructions for Continued Airworthiness K199-92 ICA dated October 31, 2012, or later FAA-accepted revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft equipped with landing gear or skis. 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 introduce no adverse effect upon the airworthiness of tha t 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 2, 2012 Date reissued: April 5, 2019 Date of issuance: November 21, 2012 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/sha256/4a/f5/4af55737be9b38d06da5f5a1f273683c83e8513969e908874322a5450422665d) - November 21, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/87/ae/87ae545fbcf7b546544b97a449f660817ffc7e9f7459c0acccaeeafabd4a240a) --- 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.