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1 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : E.208 Issue : 01 Date : 26 February 2010 Type : BRP-Powertrain GmbH & Co KG / Models without A A without List of effective Pages: Page Issue
2 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 2/7 Issue 01, 26 February 2010 / Intentionally left blank
3 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 3/7 Issue 01, 26 February 2010 / I. General 1. Type / Models: without A A without 2. Type Certificate Holder: Since February 3, 2009 Before February 3, 2009 Before June 16, 2004 Before December 29, 2001 BRP-Powertrain GmbH & Co KG DOA EASA.21J.048 BRP-Rotax GmbH & Co. KG DOA EASA.21J.048 Bombardier-Rotax GmbH & Co. KG Bombardier-Rotax Gesellschaft mbh 3. Manufacturer: As above 4. Certification Application Date: without A A without 09 October October April April April EASA Certification Date: without A A without 19 December June April April April 1986 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 3/78)
4 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 4/7 Issue 01, 26 February 2010 / II. Certification Basis 1. Airworthiness Standards: LFSM 1975, Appendix D, airworthiness requirements for engine powered sailplanes issued by Luftfahrt-Bundesamt Braunschweig, BRD (publication November 1 st, 1975) 2. Special Conditions (SC): 3. Deviations: 4. Equivalent Safety Findings (ESF): 5. Environmental Protection Requirements: III. Technical Characteristics 1. Type Design Definition: As defined the type design definition number (for ) and (for ) 2. : ROTAX 501 series engine: 2 cylinders in line, two stroke engine, ram air cooling, mixture lubrication, single magneto ignition, 2 diaphragm carburetor, belt driven propeller, electric starter, alternator, fuel pump Weight (dry): 33,5 kg (with muffler and starter) Bore: 2 x 72 mm Stroke: 61 mm Displacement: 496,7 cm 3 Compression Ratio: 10,8 Crankshaft drive rotation: counter clockwise (viewed from front) ROTAX 505 series engine: 2 cylinders in line, two stroke engine, ram air cooling, mixture lubrication, dual magnetic highvoltage condenser ignition, contact less, diaphragm carburetor, propeller drive by belt, electric starter, alternator, fuel pump Weight (dry): 34,4 kg (with muffler and electric starter) Bore: 2 x 72 mm Stroke: 61 mm Displacement: 496,7 cm 3 Compression Ratio: 10,8 Crankshaft drive rotation: counter clockwise (viewed from front)
5 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 5/7 Issue 01, 26 February 2010 / 3. Equipment: ROTAX 501 series engine: Carburetor: Fuel pump: Ignition system: Spark plugs: Starter: Power drive: Revolution measurement: 2 diaphragm carburetor Tillotson type HR., or 2 diaphragm carburetor Mikuni type BN 38 Mikuni diaphragm pump magneto ignition system (BOSCH) Generator SCP 2, 12 V, 140 W ignition point, 2,1 mm BTC Zündpunkt 2,1 mm v. OT NGK B 8 ES, Bosch W 250 T2 Bosch pinon starter, Type DG or screw drive-starter AB Trapper 1:10, 30 mm supply for an electronic tachometer, VDO ROTAX 505 series engine: Carburetor: Fuel pump: Ignition system: Spark plugs: Starter: Power drive: Revolution measurement: 2 diaphragm carburetor Tillotson type HR, or 2 diaphragm carburetor Mikuni type BN 38 Mikuni diaphragm pump Dual magnetic high-voltage condenser ignition, contactless 12 V 100 W gen. Ignition-box Bosch or Ducati For ignition-box Bosch: B8ES; Bosch W3CC, W3CP For ignition-box Ducati: BR8ES; Bosch WR3CC, WR3CP Bosch pinon starter, Type DG or screw drive-starter AB Trapper 1:10, 30 mm supply for an electronic tachometer, VDO 4. Dimension: not determined 5. Dry Weight: not determined 6. Ratings: ROTAX 501 / 505 engine: kw PS 1/min Take off power: 31, max. continous: 29,
6 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 6/7 Issue 01, 26 February 2010 / ROTAX 505 A engine: kw PS 1/min Take off power: 31, max. continous: 31, Fluids (Fuel/Oil/Additives/Coolant): 7.1 Fuel Fuel: 2 stroke mixture super gasoline min 96 ROZ or AVGAS 100 LL German English German English See Operator s Manual HB-501 OM-501 HB-505 OM-505 See Service Instruction n.a. n.a. n.a. n.a. 7.2 Oil Lubrication: Mixture lubrication mixing ratio 1:50 with super two stroke oil German English German English See Operator s Manual HB-501 OM-501 HB-505 OM-505 See Service Instruction n.a. n.a. n.a. n.a. 7.3 Coolant German English German English See Operator s Manual HB-501 OM-501 HB-505 OM-505 See Service Instruction n.a. n.a. n.a. n.a. 8. Aircraft Accessory Drives: IV. Operational Limitations 1. Temperature Limits: Cylinder head temperature max. 250 C measured with thermo couple under hottest cylinder
7 TCDS EASA.E.208 BRP-Powertrain GmbH & Co KG page 7/7 Issue 01, 26 February 2010 / 2. Speed Limits: ROTAX 501 / 505 engine: max. RPM 6800 recommended Cruising RPM: 6050 idling RPM: approx ROTAX 505 A engine: max. RPM 6800 recommended Cruising RPM: 6800 idling RPM: approx V. Operational and Service Instructions german english german english Operation- and Maintenance instruction HB-501 OM-501 HB-505 OM-505 Installation Manual EBHB-501 n.a. EBHB-505 n.a. Repair Manual RHB-501 RM-501 RHB-505 RM-505 Service Bulletins, Service Instructions and Service Letters as issued as issued as issued as issued VI. Notes Note 1: Fuel consumption ROTAX 501 / 505 engine: At 100 % power approx. 22,4 l/h (5,92 Gal/h) and at 75 % power approx. 17,2 l/h (5,54 Gal/h). ROTAX 505 A engine: At 100 % power approx. 22 l/h (5,9 Gal/h) and at 75 % power approx. 16 l/h (5,5 Gal/h)
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