STC SA02413AK

Supplemental type certificate · TAG Aerospace Inc.

Holder
TAG Aerospace Inc. · Canada
Status
Current · Reissued
Status date
November 15, 2013
Applied
December 10, 2012
Product
Aircraft · Small 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 6, 2025.

What it approves

Modification to Viking Air Limited model DHC-2 Mk. I with gross weight increase to 5,600 lbs. to incorporate wing angle change

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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate IMPORT Number SA02413AK

Date of application: December 10, 2012 Date Reissued: November 15, 2013 Date of issuance: May 3, 2013 Date Amended: November 15, 2013 By direction of the Administrator

(Signature) August A. Asay Manager, Anchorage Aircraft Certification Office (Title)

7350-72nd St., Suite 115 Delta, British Columbia Canada V4G 1H9

Part 03 of the Civil Air Regulations.

Original Product Type Certificate Number: A-806 Make: Viking Air Limited Model: DHC-2 Mk. I Description of Type Design Change: Modification to Viking Air Limited model DHC-2 Mk. I with gross weight increase to 5,600 lbs. to incorporate wing angle change in accordance with TAG Aerospace Inc. Master Document List, Report Number 001020-10, Revision B, dated December 10, 2012, or later Transport Canada approved revision.

1) The following modifications are required for the Viking Air Limited model DHC-2 Mk. I as part of this approval:

a) Gross Weight Increase to 5,600 lbs., STC SA00299NY

b) Beaver Wing Angle Modification, STC SA01258NY. As part of STC SA01258NY, STC number SA1070NE is required.

2) For Instructions for Continued Airworthiness and Airworthiness Limitations for wing strut life limits, reference TAG Aerospace Inc. Maintenance Manual Supplement, DHC-2 Beaver 5,600 lb. Maximum Gross Weight with Stolairus Wing Angle Change, Report Number 001020-07-1, Revision NC, dated April 5, 2013, or later Transport Canada accepted revision.

(continued on page 3)

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA02413AK

FAA Form 8110-2-1(10-69) Page 3 of 3

3) The following DHC-2 Mk. I configurations are approved:

a) Landplane: Maximum gross weight 5,600 lbs.

b) Skiplane: Maximum gross weight 5,600 lbs.

c) Floatplane: Maximum gross weight 5,500 lbs. with EDO 679-4930 or EDO 58-4580 floats

d) Floatplane: Maximum gross weight 5,600 lbs. with Wipline Model 6000 or 6100 Amphibian Floats in accordance with STC SA01324CH

e) Floatplane: Maximum gross weight 5,600 lbs. with Aerocet Model 5850 Twin Seaplane Floats in accordance with STC SA01722SE

4) The installer must determine whether this design change is compatible with previously approved modifications.

5) 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.

Certification Basis: Based on Civil Air Regulations part 03, dated November 13, 1945, and Title 14 Code of Federal Regulations, part 23, section 1529 as amended by 23-26.

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ADs that name this STC · 0

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No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Viking Air LimitedDHC-2 Mk.IA-806