SUPPLEMENTAL TYPE CERTIFICATE - 10071632 REV. 1
Diamond DA42 VI · Supplemental Type Certificate
Overview
This document is a Supplemental Type Certificate (STC) issued by the European Union Aviation Safety Agency (EASA) for the Diamond DA 42 series aircraft. It certifies a design change involving the installation of a specific propeller model (MTV-6-()-C-F/CF190-69()) on the DA 42 series. The STC outlines the applicable Type Certification Basis and environmental protection requirements that must be adhered to when operating the aircraft under the specified conditions. The document is intended for aircraft operators and maintenance personnel involved with the Diamond DA 42 series, ensuring compliance with the latest airworthiness standards and operational limitations.
- This STC is for the Diamond DA 42 series, including DA 42, DA 42 M, DA 42-NG, and DA 42 M-NG.
- The design change involves the installation of the MTV-6-()-C-F/CF190-69() propeller.
- Operators must comply with EASA regulations and the specified certification basis.
- Prior to installation, ensure no adverse effects on airworthiness from previous changes or repairs.
- Refer to specific MT-Propeller documents for operational and maintenance guidelines.
Document
Source
Originally published by www.mt-propellerusa.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Year
- 2019
- Pages
- 2
- File size
- 86 KB
- Publisher
- www.mt-propellerusa.com
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Description of Design Change
The STC details the installation of the MTV-6-()-C-F/CF190-69() propeller on the Diamond DA 42 series aircraft, which includes the DA 42, DA 42 M, DA 42-NG, and DA 42 M-NG models.
EASA Certification Basis
The certification basis for the original product is amended by additional airworthiness requirements, specifically referencing CS-36, Amendment 4, and FAR 36, Amendment 36-30.
Limitations/Conditions
The document specifies that prior to the installation of the propeller change, it must be confirmed that there are no adverse effects on the airworthiness of the aircraft due to the interrelationship with any previously installed changes or repairs.
Associated Technical Documentation
Operators must refer to MT-Propeller AFM-S Document No. E-3470 for DA 42 and DA 42 M, and Document No. E-3473 for DA 42-NG and DA 42 M-NG for operational guidelines. Installation and maintenance must follow the instructions outlined in Documents No. E-3471 and E-3472, respectively.
Safety notes
- Prior to installation, verify that the new propeller does not adversely affect the airworthiness of the aircraft.
Full document text
E7EASAEuropean Union Aviation Safety Agency This Certificate/Approval is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to MT-PROPELLER ENTWICKLUNG GmbH FLUGPLATZSTRASSE 1 94348 A TTI NG GERMANY EASA.21J.020 \ \ \ III I and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and, if applicable, environmental protection requirements when operated within the conditions and limitations specified below: Type Certificate Number: EASA.A.005 Type Certificate Holder: DIAMOND AIRCRAFT INDUSTRIES Type: DA 42 Model: DA 42, DA 42 M DA 42-NG, DA 42 M-NG Description of Design Change: Installation of MTV-6-()-C-F/CF190-69() on DA42 series EASA Certification Basis: The Certification Basis for the original product as amended by the following additional or alternative airworthiness requirements: The following paragraph(s) at a later amendment: CS-36, Amendment 4, FAR 36, Amdt 36-30. This certificate/ approval involves a change to the requirements for environmental protection or a change to the certified noise or emissions levels. See Continuation Sheet(s) For the European Union Aviation Safety Agency Cologne, Germany, 13 November 2019 ~inique ROLAND (-""owesGeneral Aviation ~ LI 10060959 SUPPLEMENTAL TYPE CERTIFICATE - 10071632 - REV. 1- MT-PROPELLER ENTWICKLUNG GmbH - 302829 A Agency otue European union TE.CERT.OOO91-005 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 2 A so, EZJEASAEuropean Union Aviation Safety Agency --- ------ -- -- - _::. -=-==sos»» - »aOs»»no _-----=SUPPLEMENTAL TYPE CERTIFICATE- 10071632 REV. 1 ~ a =#N E --- - - --~ -~ -- -------== I 7:5 5Associated Technical Documentation: < - .e According to MT-Propeller Master Documentation List No.E-3468,Rev1 .. re To be operated in accordance with MT-Propeller AFM-S Document No. E-3470, Rev 1 for DA 42, DA 42(M) To be operated in accordance with MT-Propeller AFM-S Document No. E-3473, Rev 1 for DA 42-NG, DA 42(M)-NG To be installed i.a.w. Installation Instructions Doc. No. E-3471, Rev O To be maintained i.a.w. Instruction for continued airworthiness Doc. No. E-3472, Rev 0 or later revisions of the above listed document(s) approved/accepted under the EASA system. Limitations/Conditions: According to limitation section of AFM-S. Prior to installation of this change/repair it must be determined that the interrelationship between this change/repair and any other previously installed change and/ or repair will introduce no adverse effect upon the airworthiness of the product. \ \ - End- I [7 ~ 10060959 SUPPLEMENTAL TYPE CERTIFICATE - 10071632 - REV. 1- MT-PROPELLER ENTWICKLUNG GmbH - 302829 A Agency of he European union TE.CERT.OOO91-005 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 2
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