What it approves
Installation of an executive seating system
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.
Part 3 of the Civil Air Regulations.
(See Page 3 for complete certification basis)
Installation of an executive seating system in accordance with Wipaire, Inc. Drawing No. 1004310, Revision G, dated March 12, 2013, or later FAA approved revisions.
1. FAA Approved Wipaire, Inc. Flight Manual Supplement, Document No. W056144-25, Revision C, dated March 27, 2013, or later FAA approved revision is required. 2. Modified aircraft must be maintained in accordance with Wipaire, Inc. Instructions for Continued Airworthiness, Document No. W056144-24, Revision C, dated April 10, 2013, or later FAA accepted revision. 3. The installer must determine whether this design change is compatible with previously approved modifications. 4. 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.
Wipaire Inc.
1700 Henry Avenue - Fleming Field South St. Paul, MN 55075 A9EA Make : Viking Air Limited Model : DHC-6-200; DHC-6-300; DHC-6-400 Date of application : November 04, 2009
Date of issuance : February 11, 2010
Date amended : December 2, 2010; April 12, 2013
(Signature) Karol Mordasiewicz Manager, Airframe & Administrative Branch Chicago Aircraft Certification Office
(Title)
Original signed by:
Gregory J. Michalik
FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES
Number
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SA02808CH Date of Issuance: February 11, 2010 Date Amended: April 12, 2013
Certification Basis:
Based on 14 CFR Sections 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Viking Air Ltd Models DHC-6-200, DHC-6-300, and DHC-6-400 with the executive seating system is as follows:
a. The type certification basis for the Viking Air Ltd Models DHC-6-200 , DHC-6-300, and DHC-6-400 is as shown on TCDS A9EA for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, November 4, 2009, is based upon part 23 as amended by Amendment 23-6 and select later amendments. Based on 14 CFR Sections 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 23-0 through 23-6:
23.301, 23.303, 23.305, 23.307, 23.321, 23.331, 23.333, 23.335, 23.337, 23.341, 23.343, 23.347, 23.349, 23.351, 23.471,
23.473, 23.479, 23.481, 23.561, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.621, 23.623, 23.625,
23.627, 23.787, 23.1413, 23.1501, 23.1529, 23.1557(d), 23.1561, 23.1581, 23.1589 Regulations at later amendments:
23.2 Amendment 23-36
23.783(a), (b), (c)(1), (c)(3) Amendment 23-34
23.785(a), (b), (e), (f), (g), (i), (j), (k), (l) Amendment 23-34
23.803 Amendment 23-34
23.807(a), (b), (c), (d) Amendment 23-34
23.815 Amendment 23-34
23.851 Amendment 23-34
23.853(a), (c), (d)(3)(i), (d)(3)(ii) Amendment 23-49
--End--
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 3
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 12, 2013 | Amended, current | Certificate |
| February 11, 2010 | Issued, earlier issue | Certificate |