Type Acceptance Report

Similar documents
Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

Type Acceptance Report

European Aviation Safety Agency

Type Acceptance Report

Type Acceptance Report

European Aviation Safety Agency

Type Acceptance Report

European Aviation Safety Agency

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

TYPE CERTIFICATE DATA SHEET

REPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION TYPE CERTIFICATE DATA SHEET NO. A094

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

TYPE CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

Type Acceptance Report

European Aviation Safety Agency: Ottoplatz 1, D Cologne, Germany - easa.europa.eu

Type Acceptance Report

Type Acceptance Report

European Aviation Safety Agency

Type Acceptance Report

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency XA42

TYPE-CERTIFICATE DATA SHEET

Page 1 of 7 01-Mar-2013 EASA.IM.A.341. Company. Be-103. Issue 2 EASA. Taganrog, BE-103. For models: general

TYPE-CERTIFICATE DATA SHEET

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency: Ottoplatz 1, D Cologne, Germany - easa.europa.eu

TYPE CERTIFICATE DATA SHEET NO. A8SO

TYPE CERTIFICATE DATA SHEET

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

European Aviation Safety Agency

Airworthiness Directive Schedule

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

TYPE CERTIFICATE DATA SHEET

Hamilton. Hamilton. Jet A/A1 (See Approved Flight Manual for additional fuels) Engine Limits: Gas Gen RPM % Ng (2006)

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

Type Acceptance Report

European Aviation Safety Agency

C.G. Range Fwd Limit 30.2 in AOD )All Aft Limit 33.8 in AOD Acrobatic )Weights 36.0 in AOD Normal ) Empty Weight C.G. Range

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency

SYLLABUS. EASA 748/2012 Part-21 SUBPART F/G POA - ADVANCED (FLY Course code: 004-C-P) Issue of FLY EN

CERTIFICATION MEMORANDUM

P/N 135A FAA Approved: 5/14/2007 Section 9 Initial Release Page 1 of 10

European Aviation Safety Agency

European Aviation Safety Agency

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

European Aviation Safety Agency

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

European Aviation Safety Agency

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines)

TYPE-CERTIFICATE DATA SHEET

European Aviation Safety Agency: Ottoplatz 1, D Cologne, Germany - easa.europa.eu

Airworthiness Directive Schedule

Contents; 1. Introduction 2. Applicable regulations 3. Categories of parts 4. Shelf life and storage

European Aviation Safety Agency

DOA No. E HAWKER A200CT. NOTE: aircraft maintenance. Published EASA.21J.020

Transcription:

TAR 15/21B/1 MTV-27 Propeller Aircraft Certification Unit

TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE DETAILS 1 4. NZCAR 21.43 DATA REQUIREMENTS 2 ATTACHMENTS 4 APPENDIX 1 4 i TAR 15/21B/1 MTV-27-1

Executive Summary New Zealand Type Acceptance has been granted to the MTV-27 Series propeller based on validation of EASA Type Certificate number P.104. There are no special requirements for import. Applicability is limited to the Models and/or serial numbers detailed in Appendix 1, which are now eligible for installation on a NZ-registered aircraft. Additional variants or serial numbers approved under the foreign type certificate can become type accepted after supply of the applicable documentation, in accordance with the provisions of NZCAR 21.43(c). 1. Introduction This report details the basis on which Type Acceptance Certificate No.15/21B/1 was granted in the Standard Category in accordance with NZCAR Part 21 Subpart B. Specifically the report aims to: (a) Specify the foreign type certificate and associated airworthiness design standard used for type acceptance of the product in New Zealand; and (b) Identify any special conditions for import applicable to any model(s) covered by the Type Acceptance Certificate. 2. ICAO Type Certificate Details Manufacturer: MT-Propeller Entwicklung GmbH Type Certificate: EASA P.104 Issued by: European Aviation Safety Agency Model(s): MTV-27-1 3. Type Acceptance Details The application for New Zealand type acceptance was from the manufacturer, dated 8 July 2014. The MTV-27 is a 5-blade variable pitch propeller with hydraulically operated pitch change mechanism which provides for Constant Speed, Feather and Reverse modes. The hub is aluminium and the blades are laminated wood with composite covering. Type Acceptance Certificate No. 15/21B/1 was granted on 14 August 2014 to the MTV-27 Series propeller based on validation of EASA Type Certificate number P.104. Specific applicability is limited to the coverage provided by the operating documentation supplied. There are no special requirements for import into New Zealand. The first application of the propeller on a NZ-registered aircraft was on the Beechcraft B200GT, installed in accordance with FAA STC Number SA03209NY. 1 TAR 15/21B/1 MTV-27-1

4. NZCAR 21.43 Data Requirements The type data requirements of NZCAR Part 21B Para 21.43 have been satisfied by supply of the following documents, or were already held by the CAA: (1) ICAO Type certificate: EASA Type Certificate Number P.104 EASA Type Certificate Data Sheet number P.104 at Issue 03 dated 21 Dec 2011 Model MTV-27-1 approved 28 March 2002 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The original certification basis of the MTV-27 propeller is JAR-P Change 7 dated October 22, 1987, as modified by Amendment P/96/1 of August 8. Later blade dash numbers were approved with some paragraphs of CS-P at Amendment 01 dated 16 November 2006, as noted on the TCDS. This is an acceptable certification basis in accordance with NZCAR Part 21B Paragraph 21.41 and Advisory Circular 21-1A, as CS-P is the successor of JAR-P, the European equivalent of FAR Part 35 which is the basic airworthiness standard for propellers called up under Part 21 Appendix C. There are no non-compliances and no additional special conditions have been prescribed by the Director under 21.23. (ii) Special Conditions: Nil (iii) Equivalent Level of Safety Findings: Nil (iv) Airworthiness Limitations: See the Airworthiness Limitations Section in the applicable Operation and Installation Manual. (3) Environmental Certification: Nil (4) Certification Compliance Listing: MT-Propeller Certification Record Document E-1856 Project 010002883-001 Model MTV-27-1 Change to Type Certification Rev.7 Issue Date 13.10.2011 (5) Flight Manual: N/A (6) Operating Data for Propeller: (i) Maintenance Manual: E-124 Operation and Installation Manual Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) TAR 15/21B/1 MTV-27-1 2

E-504 Operation and Installation Manual Reversible Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) (M) E-610 Operation and Installation Manual Reversible Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) (G), (P), (W), (A) E-809 Overhaul Manual for Metal Blades E-1083 Operation and Installation Manual Reversible Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) for PT6A-67A (MTV-16, MTV-27) E-1290 Composite Blade Overhaul Manual E-1922 Operation and Installation Manual for reversible hydraulically controlled variable pitch propeller MTV-27-1-N-C-F-R(G)-J/CFR285-82 (ii) Current service Information: Service Bulletins (iii) Illustrated Parts Catalogue: E-220 Overhaul Manual and Parts List Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) E-519 Overhaul Manual and Parts List Reversible Hydraulically Controlled Variable Pitch Propeller (Dual-Piston-System) (Constant Speed Propeller) (M) E-680 Overhaul Manual and Parts List Reversible Hydraulically Controlled Variable Pitch Propeller (Constant Speed Propeller) (G), (P), (W), (A) (7) Agreement from manufacturer to supply updates of data in (5), and (6): CAA 2171 Form from MT-Propeller Certification Engineering dated 08.07.2014 (8) Other information: EASA STC Number 10036196 E-2040 Master Operation Manual List Model MTV-27-1-E-C-F-R(P)/CFR225-55f on Hawker Beechcraft Corporation 200, 200C, 200CT, 200T, A200 (C-12A, C- 12C), A200CT (C-12D, FWC-12D, RC-12D), A200CT (C-12F, RC-12G, RC- 12H), B200, B200C, B200CT, B200T, B200GT, B200CGT E-2041 Airplane Flight Manual Supplement Hawker Beechcraft Corporation 200 (Series) Equipped With MT-Propeller Model MTV-27-1-E-C-F-R(P)/CFR225-55f 5-Blade Constant Speed, Full-Feathering, Reversible Propeller E-2042 Installation Instructions Model MTV-27-1-E-C-F-R(P)/CFR225-55f on Hawker Beechcraft Corporation 200 (Series) 3 TAR 15/21B/1 MTV-27-1

E-2043 Instructions for Continued Airworthiness Model MTV-27-1-E-C-F-R(P)/ CFR225-55f on Hawker Beechcraft Corporation 200 (Series) Attachments The following documents form attachments to this report: Copy of EASA Type Certificate Data Sheet Number EASA P.104 Sign off.. David Gill Team Leader Airworthiness... Checked Greg Baum Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: MTV-27 Series MT-Propeller Entwicklung GmbH 15/21B/1 14 August 2014 TAR 15/21B/1 MTV-27-1 4