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Effectivity: 582 UL
Edition 3 / Rev. 0

BRP-Rotax

Page 7-5

January 01/2018

7.4) Electric system

The engine types 582 UL DCDI mod. 99 / mod. 17 are equipped
with a breakerless dual capacitor discharge ignition unit with in-
tegrated generator.

The ignition unit is completely free of maintenance and needs
no external power supply.

Two charging coils fitted on the generator stator and independ-
ent from each other feed one each ignition circuit. The energy
supplied is stored in the ignition capacitor. At the moment of
ignition the external triggers supply an impulse to the control cir-
cuits and the ignition capacitors are discharged via the primary
winding of the ignition coil. The secondary winding supplies the
high voltage for the ignition spark.

NOTE

The grey cable is provided for a rev-counter signal.

Figure 3

Содержание 582 UL DCDI 17

Страница 1: ...AIRCRAFT ENGINES ref no OM 582 UL part no 899122 Operators Manual e ROTAX 582 UL dCDI Mod 99with options ROTAX 582 UL dCDI Mod 17with options picture Rotax 582 UL DCDI Mod 99 with options...

Страница 2: ...hird parties This legend shall be included on any reproduction of these data in whole or in part The Manual must remain with the engine aircraft in case of sale Copyright 2018 all rights reserved ROTA...

Страница 3: ...Chapter LEP LIST OF EFFECTIVE PAGES Chapter TOA Table of amendments Chapter 1 General note Chapter 2 Operating instructions Chapter 3 Standard operation Chapter 4 Abnormal operation Chapter 5 Perform...

Страница 4: ...Page Notes 2 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 5: ...t information about safe operation of the engine together with descriptions of the systems technical data operating media and the operational limits of the engine The specified information and procedu...

Страница 6: ...Page Notes 2 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 7: ...n 01 2018 18 Jan 01 2018 2 1 Jan 01 2018 2 Jan 01 2018 3 Jan 01 2018 4 Jan 01 2018 Chapter Page Date 5 Jan 01 2018 6 Jan 01 2018 3 1 Jan 01 2018 2 Jan 01 2018 3 Jan 01 2018 4 Jan 01 2018 5 Jan 01 2018...

Страница 8: ...Chapter Page Date 2 Jan 01 2018 Chapter Page Date rear page Page LEP 2 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0...

Страница 9: ...21J 048 cur rent no chap ter page date of change remark for appro val date of approval from authori ties date of inclusion sig na ture 0 INTRO all Jan 01 2018 DOA 0 LEP all Jan 01 2018 DOA 0 TOA all J...

Страница 10: ...ndments in this context but without any claim to completeness current no chapter page date of change comments 0 1 up to 10 all Jan 01 2018 new layout and change of company name Page TOA 2 January 01 2...

Страница 11: ...ation 11 1 6 Description of design 12 1 6 1 582 UL DCDI mod 99 mod 17 13 1 7 Type description 14 1 8 Engine components engine views cylinder designation 15 1 9 Technical data 16 1 9 1 Dimensions 16 1...

Страница 12: ...dealer For additional information on engines maintenance or parts you can also contact your nearest ROTAX authorized aircraft engines distributor or their independent Service Center Engine serial num...

Страница 13: ...etwork cm Cubic centimeter cm h Cubic centimeter per hour CGSB Canadian General Standards Board cyl Cylinder DCDI Dual Capacitor Discharge Ignition DOA Design Organisation Approval EASA European Aviat...

Страница 14: ...inch PTO Power Take Off Rev Revision RON Research Octane Number ROTAX Is a trademark of BRP Rotax GmbH Co KG rpm Revolutions per minute SAE Society of Automotive Engineers SB Service Bulletin SI Serv...

Страница 15: ...ove replace or discontinue any design specification feature or other at any time and with out incurring obligation Measurement Specifications are given in the SI metric system with the imperi al and U...

Страница 16: ...NOTE Environmental notes give you tips on environmental protection A revision bar outside the page margin indicates a change to text or graphic Page 1 6 January 01 2018 BRP Rotax Effectivity 582 UL Ed...

Страница 17: ...ows this engine is subject to sudden stoppage Unless in a run up area never run the engine with the propel ler turning while on the ground Do not operate engine if by standers are close Never leave yo...

Страница 18: ...time This could lead to a crash landing and possible se vere injury or death For this reason we recommend strict compliance with the maintenance and operation and any ad ditional information which ma...

Страница 19: ...ed out and verified by a technician that has a current iRMT rating Check for fuel contamination air cleaners etc Protect en gine while not in use from any contamination entering fuel or carburetors sy...

Страница 20: ...ge ensure any loose equipment or tools are properly secured before starting the engine Allow the engine to cool at idle for several minutes before turning off the engine Page 1 10 January 01 2018 BRP...

Страница 21: ...ns Service Letters Status The status of Manuals can be determined by checking the table of amendments The first column of this table indicates the revi sion status which should be compared with the re...

Страница 22: ...a graphic data base system and are provided with a consecutive irrelevant number This number e g AE 2St_001 is of no significance for the content 1 6 Description of design Figure 1 Page 1 12 January 0...

Страница 23: ...eumatic fuel pump Propeller drive via flange connected gearbox with incorpo rated torsional shock absorber Exhaust system standard version 48 kW Rewind starter or optional electric starter Integrated...

Страница 24: ...ignition model Designation Designation Description Type 582 Two stroke engine 2 cylinder in line with ro tary valve inlet Certifica tion UL Non certified aircraft engines Ignition DCDI Dual Capacitor...

Страница 25: ...n 3 Rev 0 BRP Rotax Page 1 15 January 01 2018 1 8 Engine components engine views cylinder designation 582 UL DCDI Figure 2 1 Engine serial number 2 Propeller gearbox 3 Electric starter PTO Power take...

Страница 26: ...n the current Installation Manual Type 582 UL DCDI mod 99 mod 17 Weight 29 1 kg 64 0 lb Type 582 UL DCDI mod 99 mod 17 Exhaust system 5 1 kg 11 2 lb 2 carburetor 1 8 kg 4 lb Propeller speed reduction...

Страница 27: ...ition 3 Rev 0 BRP Rotax Page 1 17 January 01 2018 1 9 4 Direction of rotation Direction of rotation Direction of rotation on propeller shaft clockwise viewed from the front Figure 3 Normal direction o...

Страница 28: ...Page Notes 18 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 29: ...d 6800 rpm max 5 min Cruising speed 6500 rpm Idle speed approx 2000 rpm Performance Performance data relate to ISA International Standard Atmos phere conditions 582 UL DCDI mod 99 mod 17 48 kW Lubrica...

Страница 30: ...1148 F Difference between cyl 1 and 2 Max 25 C Max 43 F Engine start oper ating temperature Max 50 C 120 F Min 25 C 13 F Coolant temperature Max 80 C 175 F Min 65 C 150 F Fuel pressure Max 0 4 bar 5 8...

Страница 31: ...ng coolant after engine stop increase percentage of antifreeze gradually In all cases antifreeze to water ratios should not exceed the antifreeze manufacturer s recommendations Exceeding the antifreez...

Страница 32: ...lead sediments in the oil sys tem Therefore use AVGAS only if you encounter problems with vapour lock or if the other fuel types are not available or equivalent fuels according to this chapter ATTENT...

Страница 33: ...Agi tate slightly to dilute oil with gasoline 3 Add gasoline to obtain desired mixture ratio use fine mesh screen 4 Replace container cap and shake the container thor oughly Then using a funnel with...

Страница 34: ...UL DCDI mod 99 mod 17 Oil as specified above ATTENTION The pour point of the oil must be at least 10 C below the ambi ent temperature Gearbox lubrication Gear oil API GL5 or GL6 SAE 140 EP or 85 W 140...

Страница 35: ...refully observe all the operating and maintenance instructions The following description of procedures depends on the respective type of installation in the aircraft and shall therefore only be seen f...

Страница 36: ...accordingly 3 3 Pre flight checks m WARNING Non compliance can result in serious injuries or death Repair as necessary all discrepancies and shortcoming before flight Safety m WARNING Non compliance...

Страница 37: ...rpm during take off roll 3 4 Engine start m WARNING Non compliance can result in serious injuries or death Do not start the engine if any person is near the engine On cold engine apply choke fully Ens...

Страница 38: ...ATTENTION Ensure ignition switch is in correct position and wired correctly Page 3 4 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0...

Страница 39: ...temperature until operating temperatures are reached 3 Check temperatures and pressure Throttle response ATTENTION After a full load ground test allow a short cooling run at idle speed to prevent vap...

Страница 40: ...d be run until latent heat build up from previous high power settings has been dissipated ap prox 3000 rpm or at nearest smooth running rpm for a mini mum of two minutes followed by a short period of...

Страница 41: ...ish between two kinds of carburetor icing Icing due to water in fuel Water in fuel will accumulate at the lower parts of the fuel sys tem and leads to freezing of fuel lines filters or jets Icing beca...

Страница 42: ...Page Notes 8 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 43: ...Too low fuel pressure 3 4 5 Trouble shooting 4 Introduction m WARNING Non compliance can result in serious injuries or death At unusual engine behaviour conduct checks as per Maintenance Manual before...

Страница 44: ...of over engine speed 4 3 Temperature ATTENTION Reduce engine power setting to the minimum necessary and carry out precautionary landing 4 3 1 Exceeding of max admissible cyl head temperature Cylinder...

Страница 45: ...Fuel pressure ATTENTION Reduce engine power setting to the minimum necessary and carry out precautionary landing 4 4 1 Too low fuel pressure m WARNING Non compliance can result in serious injuries or...

Страница 46: ...e The majority of problems quite often are a simple lack of one or the other Follow an organized method of troubleshooting This will facili tate the identification of discrepancies or shortcomings Fue...

Страница 47: ...ication on the expected power output and fuel consumption of these engines The actual power and fuel consumption is highly dependent on the installation the compliance to predefined maintenance events...

Страница 48: ...5 1 Performance data 582 UL DCDI mod 99 mod 17 Figure 1 Page 5 2 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0...

Страница 49: ...ication system electric system and the propeller gearbox The system description refers only to the engine and not to a specific application in a particular aircraft The aircraft manufacturers Operator...

Страница 50: ...ber The expansion tank is closed by a pressure cap with excess pressure valve and return valve At temperature rise of the coolant the excess pressure valve opens and the coolant will flow via a hose a...

Страница 51: ...E For fuel refer to section 2 3 7 3 Lubrication system Lubrication Generally the engines are designed to run on a gasoline oil mixture of 50 1 unless equipped with optional ROTAX oil in jection system...

Страница 52: ...tion of the rotary valve drive A 90 spiral gear situated in the crankcase and running in oil bath drives the rotary valve Gearbox lubrication Gearbox lubrication operates with its own oil filled into...

Страница 53: ...al power supply Two charging coils fitted on the generator stator and independ ent from each other feed one each ignition circuit The energy supplied is stored in the ignition capacitor At the moment...

Страница 54: ...shaft propeller shaft 2 62 1 3 00 1 3 47 1 4 00 1 NOTE This type of gearbox designated as CL is also available with an incorporated lighting generator Type E gearbox Available gear ratios Crankshaft p...

Страница 55: ...current Maintenance Manual Line last revision m WARNING Non compliance can result in serious injuries or death Only qualified staff experienced two stroke mechanics trained on this particular engine...

Страница 56: ...d fuel tank vents venting tube and air filter to prevent entry of contamination and humidity 8 1 2 At engine stoppage of 1 to 4 weeks Let the engine run at increased idle speed Shut engine down and se...

Страница 57: ...parts Refit spark plugs Drain gasoline from float chambers fuel tank and fuel lines ENVIRONMENTAL NOTE Protect the environment Generally comply with standard rules for handling of chemicals Dis pose...

Страница 58: ...Page Notes 4 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 59: ...stributor Overview of ROTAX Authorized Distributor or their independent Service Center Refer to the official ROTAX AIRCRAFT ENGINES Website www FLYROTAX com Effectivity 582 UL Edition 3 Rev 0 BRP Rota...

Страница 60: ...Page Notes 2 January 01 2018 BRP Rotax Effectivity 582 UL Edition 3 Rev 0 NOTES...

Страница 61: ...he respective collecting point or hand it over to an approved disposal company Fuel Dispose of fuel at the respective collecting point or hand it over to an approved disposal company m WARNING Flammab...

Страница 62: ...ROTAX aircraft engines F O B to ROTAX Authorized Distributors or their independent Service Centers Chemical agents cleaner LOCTITE etc Please observe the safety and disposal instructions of the manuf...

Страница 63: ...engine stoppage of 1 to 4 weeks 2 Engine preservation at out of service periods or storage of engine for longer than 4 weeks up to 1 year 2 Engine start 2 3 Engine views 15 Exceeding cylinder head tem...

Страница 64: ...RP Rotax Effectivity 582 UL Edition 3 Rev 0 S Safety notice 5 7 Special operating conditions 6 T Table of amendments 1 Technical data 16 Technical documentation 11 Temperature 2 Trouble shooting 4 Typ...

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Страница 68: ...______________________________________ Type of aircraft __________________________________________________________ Aircraft registration no ROTAX authorized distributor www abm at WWW FLYROTAX COM 465...

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