STC SR01848SE

Supplemental type certificate · Kenmore Air Harbor LLC

Holder
Kenmore Air Harbor LLC · United States
Status
Current · Reissued
Status date
April 5, 2019
Applied
September 9, 2006
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA-806

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Revise the routing of the existing water rudder retraction cables from the cockpit through the belly of the aircraft

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number SR01848SE

This certificate, issued to Kenmore Air Harbor, LLC.

6321 NE 175th Street Kenmore, WA 98028

Part 23 of the Federal Regulations.

Original ProductType Certificate Number: A-806 Make: DeHavilland Model: DHC-2 Mark I (S/N 1 through 79, 81 and subsequent) DHC-2 Mark II (S/N 80 only) DHC-2 Mark III (S/N 1 through 79, 81 and subsequent) Description of the Type Design Change: Revise the routing of the existing water rudder retraction cables from the cockpit through the belly of the aircraft in accordance with Kenmore Air Harbor, Inc. Master Drawing List, KAH0701MDL, Revision C, dated October 6, 2007, or later FAA approved revision. The water rudder retraction system must be maintained in accordance with Kenmore Air Harbor, Inc.

Instructions for Continued Airworthiness, KAH0701ICA, Revision A, dated April 23, 2007, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies only to the aircraft models listed above that are mounted on floats. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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 aircraft. A copy of this Certificate and FAA approved Instructions for Continued Airworthiness 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: September 9, 2006 Date reissued: April 5, 2019 Date of issuance: June 12, 2008 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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
de Havilland Inc. (Canada)DHC-2 Mk.IA-806
de Havilland Inc. (Canada)DHC-2 Mk.IIA-806
de Havilland Inc. (Canada)DHC-2 Mk.IIIA-806

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
April 5, 2019Reissued, currentCertificate
June 12, 2008Issued, earlier issueCertificate