What it approves
Installation of Replacement Engine Mount Kit
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 29 of the Federal Aviation Regulations.
Installation of Replacement Engine Mount Kit to be in accordance with Transport Canada Approved Dart Aerospace Ltd. Installation Instructions IIN-D205-770, Revision A dated November 1, 2008 or later Transport Canada approved revision.
1. Installation of Replacement Engine Mount Kit to be in accordance with Transport Canada Approved Dart Aerospace Ltd.
Installation Instructions IIN-D205-770, Revision A dated November 1, 2008 or later Transport Canada approved revision.
2. Manufacture of replacement engine mount kit to be in accordance with Transport Canada approved Dart Aerospace Ltd.
Master Document List MDL-D205-770, Revision B dated November 24, 2008 or later Transport Canada approved revision.
3. Maintenance is to be in accordance with Dart Aerospace Ltd. Instructions for Continued Airworthiness document ICA- D205-770, Revision 0 dated November 24, 2008, or later Transport Canada accepted revision.
Dart Aerospace Limited 1270 Aberdeen Street Hawkesbury, Ontario K6A 1K7, Canada H1SW Make : Bell Model : 205A-1, 205B, 210 Date of application : December 16, 2008
Date of issuance : April 17, 2009
(Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) IMPORT
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SR02690NY Date of Issuance: April 17, 2009
4. If the holder agrees to permit another person to use th is certificate to alter a product, the holder must give the other person written evidence of that permission.
5. The Installer must determine whether this design change is compatible with previously approved modifications.
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification is as follows:
The type certification basis for this modification is 14 CFR 29 at Amendment 51 with the following exceptions:
§ 29.561 Amendment 29-0 § 29.571 Amendment 29-20
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ADs that name this STC · 0
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