STC SA04341NY

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Part of .

IMPORT SA04341NY Kenn Borek Air Ltd.

290 McTavish Road, N.E.

Calgary, Alberta Canada T2E 7S3 3/23 the Civil Air and Federal Aviation Regulations A9EA Viking Air Limited DHC-6-100, DHC-6-200, DHC-6-300

1. Removal of the Beta Back-up System must be done in accordance with Configuration 1 or Configuration . 2 as described in Infinion Certification Engineering Installation Instruction EO-1793-01, Issue 1, dated May 2, 2016, Transport Canada approved May 18, 2016, or later Transport Canada approved revision.

2. Operation must be done in accordance with Infinion Flight Manual Supplement FMS-1793-01, Issue 1, dated May 2, 2016, Transport Canada approved May 18, 2016, or later Transport Canada approved revision. (Description of Type Design Change Continued on Page 3 of 3)

1. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(Limitations and Conditions Continued on Page 3 of 3) 03/15/2019 12/17/2020 Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division Aircraft Certification Service 3

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

IMPORT SA04341NY SA04341NY 3

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

IMPORT SA04341NY Date of Issuance: December 17, 2020

Description of Type Design Change (continued):

3. Maintenance must be done in accordance with Infinion Maintenance Manual Supplement and Instructions for Continued Airworthiness MMS-1793-01, Issue 1, dated May 2, 2016, or later Transport Canada accepted revision.

4. Type Design Change is defined in Infinion Master Data List MDL-1793-01, Issue 1, dated May 02, 2016, Transport Canada approved May 18, 2016, or later Transport Canada approved revision.

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

3. This STC is applicable to any DHC-6-100/-200/-300 series aircraft with the PT6A-27 or PT6A-34 engines installed. The following Supplemental Type Certificates do engine conversions and are currently approved by the FAA:

SA01673NY; SA100CH; SA02642LA; SA03265NY; SA00837NY; SA743NE; and SA02682LA

Certification Basis:

Basis of Certification: 14 CFR Part 23 §§ 23.1, 23.301, 23.303, 23.305, 23.307, 23.561,

23.601, 23.603, 23.605, 23.609, 23.613, 23.615, 23.619, 23.625 23.1301, 23.1365,

23.1501, 23.1541, 23.1581, and 23.1585 at Amdt 23-0, plus 23.1529 at Amdt 23-8.

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