# STC SA02101SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Fabrication of the Kenmore 70-Amp Alternator Kit - Applied: December 23, 2009 - Status date: April 5, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806) - Certificate PDF: https://openairdocs.org/files/sha256/a4/a4/a4a4045cbe21dd14ed776629c01acdee61ab49ef3ca51536680c7702036cda73 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0D0C627E92CCE048862585CF003F3542.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02101SE ## ADs that name it (0) None. ## Approved models (1) - Viking Air Limited DHC-2 Mk.I ([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 SA02101SE 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-806 Make: Viking Air Limited (formerly DeHavilland) Model: DHC-2 Mk. I Description of the Type Design Change: Fabrication of the Kenmore 70-Amp Alternator Kit in accordance with Kenmore Air Harbor, Inc. Master Drawing List K8883MDL, Revision --, dated January 12, 2010, or later FAA- approved revision; and installation in accordance with Kenmore Air Harbor Installation Instructions Number K8883, Revision--, dated January 12, 2010, or later FAA-approved revision; and maintenance in accordance with Kenmore Air Harbor Instructions for Continued Airworthiness K8883ICA, Rev -, dated April 2, 2010 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 on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of the 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 and K8883ICA must be maintained as part of the permanent records for the modified airplane. 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: December 23, 2009 Date reissued: April 5, 2019 Date of issuance: February 16, 2011 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/a4/a4/a4a4045cbe21dd14ed776629c01acdee61ab49ef3ca51536680c7702036cda73) - February 16, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1f/c6/1fc61cfdc6d4005d0709b703634416df251d03210397916c3e61e85bfe47dfe5) --- 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.