TYPE-CERTIFICATE DATA SHEET
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1 TYPE-CERTIFICATE DATA SHEET No. E.209 for Rotax 535 series engines Type Certificate Holder BRP-Rotax GmbH & Co. KG Rotaxstrasse 1 A-4623 Gunskirchen Austria For Models: Rotax 535 A Rotax 535 B Rotax 535 C TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 1 of 11
2 Intentionally left blank TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 2 of 11
3 TABLE OF CONTENTS I. General Type/ Model Type Certificate Holder Manufacturer Date of Application EASA Type Certification Date...4 II. Certification Basis EASA Certification Basis Airworthiness Standards Special Conditions (SC) Equivalent Safety Findings Deviations Environmental Protection...5 III. Technical Characteristics Type Design Definition Description Equipment Dimensions Dry Weight Ratings Fluids (Fuel, Oil, Coolant, Additives) Fuel Oil Coolant Aircraft Accessory Drives...8 IV. Operating Limitations Temperature Limits Speed Limits...8 V. Operating and Service Instructions...9 VI. Notes...9 SECTION: ADMINISTRATIVE I. Acronyms and Abbreviations II. Type Certificate Holder Record III. Change Record TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 3 of 11
4 I. General 1. Type/ Model Rotax 535 A Rotax 535 B Rotax 535 C 2. Type Certificate Holder Rotaxstraße 1 A-4623 Gunskirchen, Austria DOA EASA.21J Manufacturer As above 4. Date of Application Rotax 535 A Rotax 535 B Rotax 535 C 29 June June 1982 not known, but before EASA Type Certification Date Rotax 535 A Rotax 535 B Rotax 535 C 27 April April June 1987 Note: EASA type certificate for all these models is granted in accordance with article 2 paragraph 3(a) of EU Commission Regulation 1702/2003 replacing the BAZ/ACG Austria certification of these products (Austrian Type Certification no. TW 5/83) TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 4 of 11
5 II. Certification Basis 1. EASA Certification Basis 1.1. Airworthiness Standards JAR 22, Appendix H, airworthiness requirements for engines of powered sailplanes issued by Bundesanstalt für Flugsicherung, BRD (publication March 15, 1982) 1.2. Special Conditions (SC) none 1.3. Equivalent Safety Findings none 1.4. Deviations none 1.5. Environmental Protection none III. Technical Characteristics 1. Type Design Definition As defined the type design definition number TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 5 of 11
6 2. Description 3. Equipment ROTAX 535 A and 535 B: 2 cylinders in line, two stroke engine, liquid cooling, mixture lubrication, dual magneto highvoltage condenser ignition contact less, 2 x diaphragm carburetors, belt driven propeller, electric starter, alternator, fuel pump Weight (dry): 35 kg (with muffler and electric starter) Bore: 72 mm Stroke: 64 mm Displacement: 521,2 cm 3 Compression Ratio: 11,5 Crankshaft drive rotation: counter clockwise (viewed from front) ROTAX 535 C: 2 cylinders in line, two stroke engine, liquid cooling, mixture lubrication, dual magneto highvoltage condenser ignition contact less, 1 diaphragm carburetor, belt driven propeller, electric starter, alternator, fuel pump Weight (dry): 35 kg (with muffler and electric starter) Bore: 72 mm Stroke: 64 mm Displacement: 521,2 cm 3 Compression Ratio: 11,5 Crankshaft drive rotation: counter clockwise (viewed from front) ROTAX 535 A and 535 B: Carburetor: 2 x diaphragm carburetors Tillotson type HR, or 2 x diaphragm carburetors Mikuni type BN 38 Fuel pump: Mikuni diaphragm pump DF 44 Ignition system: dual magnetic high-voltage condenser ignition, contact less 12 V 100 W gen. Ignition-box Bosch or Ducati Spark plugs: for ignition-box Bosch: B8ES; Bosch W3CC, W3CP for ignition-box Ducati: BR8ES; Bosch WR3CC, WR3CP Starter: Inertia drive electric starter AB Power drive: trapper 1:10, 30 Revolution measurement: supply for an electronic tachometer TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 6 of 11
7 4. Dimensions ROTAX 535 C: not determined 5. Dry Weight Carburetor: 1 diaphragm carburetor BN 38 Fuel pump: Mikuni diaphragm pump DF 44 Ignition system: dual magnetic high-voltage condenser ignition, contact less 12 V 100 W gen. Ignition-box Bosch or Ducati Spark plugs: for ignition-box Bosch: B8ES; Bosch W3CC, W3CP for ignition-box Ducati: BR8ES; Bosch WR3CC, WR3CP Starter: Inertia drive electric starter AB Power drive: trapper 1:10, 30 Revolution measurement: supply for an electronic tachometer 35 kg (with muffler and electric starter) 6. Ratings ROTAX 535 A and 535 C: ROTAX 535 B: kw PS 1/min Take off power: max. continous: kw PS 1/min Take off power: max. continous: Fluids (Fuel, Oil, Coolant, Additives) 7.1. Fuel Fuel: 2 stroke mixture super gasoline min 96 ROZ or AVGAS 100 LL Rotax 535 A / 535 B Rotax 535 C Description German English German English See Operator s Manual HB-535 OM-535 HB OM See Service Instruction n.a. n.a. n.a. n.a. TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 7 of 11
8 7.2. Oil Lubrication: Mixture lubrication mixing ratio 1:50 with super two stroke oil Rotax 535 A / 535 B Rotax 535 C Description German English German English See Operator s Manual HB-535 OM-535 HB OM See Service Instruction n.a. n.a. n.a. n.a Coolant 8. Aircraft Accessory Drives none Rotax 535 A / 535 B Rotax 535 C Description German English German English See Operator s Manual HB-535 OM-535 HB OM See Service Instruction n.a. n.a. n.a. n.a. IV. Operating Limitations 1. Temperature Limits Cylinder head temperature max. 95 C (cooling liquid in cylinder head) 2. Speed Limits max. RPM 7200 idling RPM: approx TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 8 of 11
9 V. Operating and Service Instructions Description Operation- and Maintenance instruction Rotax 535 A / 535 B Rotax 535 C German English German English HB-535 OM-535 HB OM Installation Manual EBHB-535 n.a. EBHB-535 n.a. Repair Manual RHB RM RHB RM Service Bulletins, Service Instructions and Service Letters as issued as issued as issued as issued VI. Notes Note 1: Fuel consumption At 100 % power approx. 29 l/h (7,67 Gal/h) and at 75 % power approx. 22 l/h (5,82 Gal/h). TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 9 of 11
10 SECTION: ADMINISTRATIVE I. Acronyms and Abbreviations ACG AS 8020 AVGAS CHT CT CW CCW CS-E EASA FAA FAR HIRF IM IPC JAR JAR-E MMH MML OM OHM OHMA rpm RTCA SB SI TBO TCDS TCU Austro Control GmbH Aerospace Standard: General minimum performance standards for generators/starter-generators and associated voltage regulators for use in direct current (DC) electric systems for civil aircraft Aviation Gasoline Cylinder Head Temperature Coolant Temperature clockwise counter-clockwise Certification Specifications Engines European Aviation Safety Agency Federal Aviation Administration Federal Aviation Regulations High Intensity Radiated Fields Installation Manual Illustrated Parts Catalog Joint Aviation Requirements Joint Aviation Requirements Engines Maintenance Manual Heavy Maintenance Manual Line Operators Manual Overhaul Manual Overhaul Manual, Appendix revolutions per minute Radio Technical Commission for Aeronautics Service Bulletin Service Instruction Time between Overhaul Type Certificate Data Sheet Turbo Control Unit TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 10 of 11
11 II. Type Certificate Holder Record Before June 15, 2016 Before March 15, 2014 BRP-Powertrain GmbH & Co KG Rotaxstraße 1 A-4623 Gunskirchen Austria DOA EASA.21J.048 BRP-Powertrain GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria Before February 3, 2009 Before June 16, 2004 BRP-Rotax GmbH & Co. KG Welser Straße 32 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Bombardier-Rotax GmbH & Co. KG Welser Straße 32 A-4623 Gunskirchen, Austria Before December 29, 2001 Bombardier-Rotax Gesellschaft mbh Welser Straße 32 A-4623 Gunskirchen, Austria III. Change Record Issue Date Changes TC issue Issue February 2010 Initial Issue 26 February 2010, Initial Issue Issue May 2014 Issue September 2016 Name change to as of June 15, END- 05 September 2016 TE.CERT European Aviation Safety Agency, All rights reserved. ISO9001 Certified. Page 11 of 11
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