What it approves
Installation of the Replacement Cabin Roof Escape Hatch
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.
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 SA04565NY Rocky Mountain Aircraft 129 MacLaurin Drive, Springbank Airport Calgary, Alberta Canada T3Z 3S4 23 Title 14 Code of Federal Regulations A9EA Viking Air Limited DHC-6 Series 100, 200, 300, 400
1. Installation of the Replacement Cabin Roof Escape Hatch must be in accordance with Transport Canada Civil Aviation (TCCA) approved Rocky Mountain Aircraft (RMA) Modification Instruction E117110, Revision "-" , dated June 05, 2020, or later TCCA approved revision.
2. Maintenance must be in accordance with TCCA accepted RMA Maintenance Manual Supplement E117131, Revision "-" dated May 22, 2020, or later TCCA accepted 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) 08/12/2020 11/20/2020 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 SA04565NY SA04565NY 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 SA04565NY Date of Issuance: November 20, 2020
Description of Type Design Change (continued):
3. Definition of the Type Design Change can be found in TCCA approved RMA Engineering Data Summary E117100, Revision B, dated May 22, 2020, or later TCCA approved revision.
2. The installer must determine whether this design change is compatible with previously approved modifications.
3. This STC is applicable to all serial numbers for this Make-Model-Series.
Certification Basis:
14 CFR Part 23 including amendments 23-1 through 23-6 plus FAR 23.807 Amendment 23-34, FAR 23.1529, Amendment 23-8, FAR 23.1557(d), and Amendment
23-7.
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ADs that name this STC · 0
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