STC SA3684NM

Supplemental type certificate · Kenmore Air Harbor LLC

Holder
Kenmore Air Harbor LLC · United States
Status
Current · Reissued
Status date
April 5, 2019
Applied
December 23, 1986
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDSA-806

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

What it approves

Installation of Pratt & Whitney PT6A-135 engine and a Hartzell HC-B3TN-3DCY)/T10282+0 propeller.

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 SA3684NM This certificate, issued to Kenmore Air Harbor, LLC.

6321 NE 175th Street Kenmore, WA 98028 Part * of the Federal Aviation Regulations.* 21.29(a)(ii) Original ProductType Certificate Number: A-806 Make: DeHavilland Model: DHC-2 Mk III (Turbo-Beaver) Description of the Type Design Change: Installation of a Pratt & Whitney Model PT6A-135 or PT6A-135A engine, Hartzell HC-B3TN-3D(Y)/T10282-0 propeller, EPA fuel drain, extended exhaust nozzles, battery box, rudder springs and horizontal tail tip-fins, in accordance with Kenmore Air Harbor, Inc. Drawing list No. K17209, dated July 17, 1989, and Installation Instructions No. K17209, revised May 10, 1990, or later FAA -approved revisions.

Limitations and Conditions: Approval of this change in type design applies to those DeHavilland Model DHC-2 Mk III airplanes equipped with Bristol 679-4930 floats or Bristol 348-1-4930 Amphibious floats only (PT6A-135); or Bristol 679-4930 floats only (PT6A-135A). 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 airplane. Airplanes modified in accordance with this STC must be operated in accordance with FAA approved Airplane Flight Manual Supplement Revised may 17, 1990, or later FAA-approved revision. A copy of this Certificate and the FAA-approved Flight Manual Supplement must be maintained as a part of the permanent records for the modified aircraft.

NOTE: For maintenance limits, refer to the AFM Supplement.

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, 1986; Date reissued: April 5, 2019 May 30, 1989 Date of issuance: April 25, 1988 Date amended: May 17, 1990

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 · 1

MakeModelData sheet
Viking Air LimitedDHC-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
May 17, 1990Issued, earlier issueCertificate