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Rotax 582 UL series Operator's Manual

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AIRCRAFT ENGINES

OperatOrs Manual

FOr rOtax® EnginE tYPE 582 UL SERIES

rOtaX® 582 ul dCdI Mod. 99

with OPtiOnS

rOtaX® 582 ul dCdI Mod. 17

with OPtiOnS

ref. no.: OM-582 UL | part no.: 899122

picture: rOtax® 582 UL DCDi Mod. 99 with options

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Summary of Contents for Rotax 582 UL series

  • Page 1
    FOr rOtax® EnginE tYPE 582 UL SERIES rOtaX® 582 ul dCdI Mod. 99 with OPtiOnS rOtaX® 582 ul dCdI Mod. 17 with OPtiOnS ref. no.: OM-582 UL | part no.: 899122 picture: rOtax® 582 UL DCDi Mod. 99 with options…
  • Page 2
    These technical data and the information embodied therein are the property of BRP-Rotax GmbH & CO KG, Austria, acc, BGBI 1984 no. 448, and shall not, without prior written permission of BRP-Rotax GmbH & Co KG, be disclosed in whole or in part to third parties.

  • Page 3: Table Of Contents

    4 – Abnormal operation Chapter 5 – Performance and Fuel consumption Chapter 7 – System Description Chapter 8 – Checks Chapter 9 – Supplement Chapter 10 – Proper disposal BRP-Rotax Page Content-1 Effectivity: 582 UL Edition 3 / Rev. 0 January 01/2018…

  • Page 4
    NOTES Page Notes-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 5
    INTRO) Introduction Topics in this chapter Foreword BRP-Rotax GmbH & Co KG (hereinafter “BRP-Rotax”) provides “Instructions of Continued Airworthiness”, which are based on the design, the tests and certification of the engine and its components. These instructions apply only to engines and components supplied by BRP-Rotax.
  • Page 6
    NOTES Page Notes-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 7
    Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Jan. 01 2018 Effectivity: 582 UL BRP-Rotax Page LEP-1 Edition 3 / Rev. 0 January 01/2018…
  • Page 8
    Chapter Page Date Chapter Page Date rear Jan. 01 2018 page Page LEP-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 9: Toa) Table Of Amendments

    INTRO Jan. 01 2018 DOA* Jan. 01 2018 DOA* Jan. 01 2018 DOA* 1 up to Jan. 01 2018 DOA* BRP-Rotax Page TOA-1 Effectivity: 582 UL Edition 3 / Rev. 0 January 01/2018…

  • Page 10
    Summary of the relevant amendments in this context, but without any claim to completeness. page current no. chapter date of comments change 1 up to 10 Jan. 01 2018 new layout and change of company name BRP-Rotax Effectivity: 582 UL Page TOA-2 January 01/2018 Edition 3 / Rev. 0…

  • Page 11: General Note

    ………………15 1.9 Technical data ………………16 1.9.1 Dimensions ………………16 1.9.2 Weights ……………….. 16 1.9.3 Fuel consumption …………….16 1.9.4 Direction of rotation …………….17 Effectivity: 582 UL BRP-Rotax Page 1-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 12: General

    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 When making inquiries or ordering parts, always indicate the number engine serial number.

  • Page 13: Abbreviations And Terms

    General Aviation Manufacturers Association g/kWh Gram per kilowatt hour High Altitude Compensation Horsepower Inch in³ Cubic inch in³/h Cubic inch per hour INTRO Introduction International Standard Atmosphere Effectivity: 582 UL BRP-Rotax Page 1-3 Edition 3 / Rev. 0 January 01/2018…

  • Page 14
    Newtonmeter Pounds per square inch Power Take Off Rev. Revision Research Octane Number ROTAX® Is a trademark of BRP-Rotax GmbH & Co KG Revolutions per minute Society of Automotive Engineers Service Bulletin Service Instruction Service Letter Type certificate Table Of Amendment…

  • Page 15: Safety

    The information and descriptions of components and systems contained in this Manual are correct at the time of publication. BRP-Rotax maintains a policy of continuous improvement of its products without imposing upon itself any obligation to retrofit products previously manufactured.

  • Page 16
    ENVIRONMENTAL 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 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 17: Safety Information

    Never fly the aircraft equipped with this engine at locations, air speeds, altitudes or in other situations which do not allow a success- ful no-power landing after sudden engine stoppage. Effectivity: 582 UL BRP-Rotax Page 1-7 Edition 3 / Rev. 0 January 01/2018…

  • Page 18
    • Due to the varying designs, equipment and types of aircraft, BRP-Rotax grants no warranty on the suitability of its engines use on any particular aircraft. Further, BRP-Rotax grants no warranty on this Engine’s suitability with any other part, com- ponents or system which may be selected by the aircraft manufacturer, assembler or user for aircraft application.
  • Page 19
    • Select and use proper aircraft instrumentation. This instru- Instrumentation mentation is not included in the ROTAX® engine package. Only approved instrumentation may be installed. Engine log book • Keep an engine log book and respect engine and aircraft maintenance schedules. Keep the engine in top operating condition at all times.
  • Page 20
    • To eliminate the risk of injury or damage, 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 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 21
    Reference Any reference to a document refers to the latest edition issued by BRP-Rotax if not stated otherwise. Illustrations The illustrations in this Manual are merely sketches and show typical arrangements.
  • Page 22
    This number (e.g. AE 2St_001) is of no significance for the content. 1.6) Description of design Figure 1 Page 1-12 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 23: 582 Ul Dcdi Mod. 99 / Mod. 17

    • Radiator (one-piece or two-piece radiator set). NOTE 582 UL DCDI mod. 99 and 582 UL DCDI mod. 17 are only avail- able as 48 kW version. Effectivity: 582 UL BRP-Rotax Page 1-13 Edition 3 / Rev. 0 January 01/2018…

  • Page 24: Type Description

    1.7) Type description The type description consists of the following: e.g. mod. ROTAX 99 / DCDI mod. type ignition model certification Designation Designation Description Type Two stroke engine, 2 cylinder in line with ro- tary valve inlet. Certifica- Non-certified aircraft engines…

  • Page 25: Engine Components, Engine Views, Cylinder Designation

    1.8) Engine components, engine views, cylinder designation 582 UL DCDI Figure 2 Engine serial number Propeller gearbox Electric starter Magneto side Power take off side Effectivity: 582 UL BRP-Rotax Page 1-15 Edition 3 / Rev. 0 January 01/2018…

  • Page 26: Technical Data

    582 UL DCDI / mod. 99 / mod. 17 at take-off performance 26.5 l/h (7 US gal/h) at 75 % continuous performance 20.5 l/h (5.4 US gal/h) specific fuel consumption 425 g/kWh (0.7 lb/hph) Page 1-16 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 27: Direction Of Rotation

    1.9.4) Direction of rotation Direction of Direction of rotation on propeller shaft: clockwise, viewed from rotation the front. Figure 3: Normal direction of propeller rotation Effectivity: 582 UL BRP-Rotax Page 1-17 Edition 3 / Rev. 0 January 01/2018…

  • Page 28
    NOTES Page Notes-18 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 29: Operating Instructions

    2.3 Operating media – Fuel…………….4 2.4 Operating media — Lubricants …………..6 Introduction This chapter of the Operators Manual contains the operating limits that must be observed to ensure the ROTAX® aircraft engine and standard systems operate safely. 2.1) Operating limits Speed Take-off speed 6800 rpm (max.

  • Page 30
    -25 °C (-13 °F) Coolant temperature Max. 80 °C (175 °F) Min. 65 °C (150 °F) Fuel pressure Max. 0.4 bar (5.8 psi) Min. 0.2 bar (2.9 psi) Page 2-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 31
    At verification of the coolant level replenish coolant at radiator cap (radiator or expansion tank). The coolant level in the over- flow bottle should be between min. and max. mark. Effectivity: 582 UL BRP-Rotax Page 2-3 Edition 3 / Rev. 0 January 01/2018…
  • Page 32
    Risk of vapor formation when using winter fuel for summer operation. ATTENTION If the engine is not equipped with injection lubrication, a 2 % Super two stroke oil must be added to the fuel. Page 2-4 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 33
    Non-compliance can result in serious injuries or death! At refueling use only metal containers and ground the aircraft in ac- cordance with the grounding specifications to avoid electrostatic charging. Effectivity: 582 UL BRP-Rotax Page 2-5 Edition 3 / Rev. 0 January 01/2018…
  • Page 34
    Gear oil API-GL5 or GL6, SAE 140 EP, or 85 W — 140 EP. lubrication Rotary valve drive Super two stroke oil (same as used for engine lubrication). lubrication Page 2-6 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 35: Standard Operation

    The control elements mentioned in this chapter are only symbolic and should support the understanding of the procedures. The execution of control elements is in the responsibility of the aircraft manufacturer. Effectivity: 582 UL BRP-Rotax Page 3-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 36: Daily Checks

    • Verify oil tank content (oil injection engines) • Inspect for coolant leaks • Inspect engine and gearbox for oil leaks Ignition system • Verify spark plug connectors for security Page 3-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 37: Engine Start

    If the engine fails to start or operates only on one cylinder, check whether the ignition wiring is correctly connected to the spark plug connectors, check spark plugs and check the igni- tion is in ON position. Effectivity: 582 UL BRP-Rotax Page 3-3 Edition 3 / Rev. 0 January 01/2018…

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

  • Page 39: After Engine Start

    Operate the engine at 3000 to 3500 rpm. Alternately ignition system 1 and 2 must be switched off. Speed drop with only one ignition circuit must not ex- ceed 300 rpm. Effectivity: 582 UL BRP-Rotax Page 3-5 Edition 3 / Rev. 0 January 01/2018…

  • Page 40: Operation In Flight

    A well designed and well maintained air intake system (e.g. RO- TAX® intake silencer with K & N oil impregnated air filter) will help to prevent water ingestion. Page 3-6 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 41
    Be aware that modifications will require a different carburetor setting. Enquire at your dealer for more information, and consult author- ized ROTAX® aircraft engines distributor or their independent Service Center. Winter Winter can create additional problems such as carburetor icing, frozen fuel lines, higher air densities etc., which may affect car-…
  • Page 42
    NOTES Page Notes-8 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 43: Abnormal Operation

    Further checks — see Maintenance Manual. The following description of procedures depends on the respective type of installation in the aircraft and shall therefore only be seen functionally. Effectivity: 582 UL BRP-Rotax Page 4-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 44
    Any exceeding of the max. admissible exhaust gas temperature haust gas temper- must be entered by the pilot into the logbook, stating duration ature max. and extent of excess-temperature condition. Page 4-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 45
    4.4.1) Too low fuel pressure m WARNING Non-compliance can result in serious injuries or death! Repair as necessary all discrepancies and shortcoming before flight. Effectivity: 582 UL BRP-Rotax Page 4-3 Edition 3 / Rev. 0 January 01/2018…
  • Page 46
    Start by checking the supply (tank), fittings (loose?), filter (plugged?), float chamber (fouled?). Spark Try new spark plugs. Problems of a more complex nature are best left to a ROTAX® engine technician: See your ROTAX® Authorized Distributor or their independent Service Centers. Knocking under load…
  • Page 47
    Those values need to determined and provided by the aircraft manufacturer. Effectivity: 582 UL BRP-Rotax Page 5-1 Edition 3 / Rev. 0 January 01/2018…
  • Page 48
    5.1) Performance data 582 UL DCDI mod.99 / mod. 17 Figure 1 Page 5-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 49: System Description

    The design shown in this chapter does not represent a specified execution but should support the understanding of the system. Effectivity: 582 UL BRP-Rotax Page 7-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 50
    Radiator screw cap, with ex- Hose from cylinder head to cess pressure valve and re- radiator turn valve Temperature gauge for 10 Overflow hose cooling water Page 7-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 51
    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. For preparation of fuel-oil mixture refer to sec- tion 2.3. Oil injection…
  • Page 52
    Gearbox lubrication operates with its own oil filled into gearbox lubrication housing. ATTENTION Never operate engine with a dry gearbox. NOTE For lubricants refer to section 2.4. Page 7-4 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 53
    The secondary winding supplies the high voltage for the ignition spark. NOTE The grey cable is provided for a rev-counter signal. Figure 3 Effectivity: 582 UL BRP-Rotax Page 7-5 Edition 3 / Rev. 0 January 01/2018…
  • Page 54
    3.00 : 1 Crankshaft : propeller shaft 3.47: 1 4.00 : 1 NOTE This type of gearbox designated as EL is also available with an incorporated lighting generator. Page 7-6 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 55: Checks

    ATTENTION Carry out all directives of Service Bulletins (SB), according to their priority. Observe applicable Service Instructions (SI) and Service Letter (SL). Effectivity: 582 UL BRP-Rotax Page 8-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 56
    • Remove air filters and inject approx. 6 cm³ of preservation oil or equivalent oil into the air intake of each carburetor • Stop engine and secure against inadvertent engine start Page 8-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 57
    • Spray all external steel parts with engine oil or appropriate preservation oil Effectivity: 582 UL BRP-Rotax Page 8-3 Edition 3 / Rev. 0 January 01/2018…
  • Page 58
    NOTES Page Notes-4 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 59: Supplement

    9) Supplement Authorized Overview of ROTAX® Authorized Distributor or their Distributor independent Service Center. Refer to the official ROTAX® AIRCRAFT ENGINES Website www.FLYROTAX.com. Effectivity: 582 UL BRP-Rotax Page 9-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 60
    NOTES Page Notes-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…

  • Page 61: Proper Disposal

    ENVIRONMENTAL NOTE Work with the utmost care to ensure that no water pollutants can penetrate into the soil, water or the sewerage system. Effectivity: 582 UL BRP-Rotax Page 10-1 Edition 3 / Rev. 0 January 01/2018…

  • Page 62
    Please return old/used parts (not periodic maintenance parts) Old/used parts from ROTAX® aircraft engines F.O.B to ROTAX® Authorized Distributors or their independent Service Centers. Chemical agents Please observe the safety and disposal instructions of the (cleaner, LOCTITE manufacturer. etc.) Page 10-2…
  • Page 63
    4 weeks up to 1 year……..2 Engine start ……. 2–3 Engine views …….15 Re-Start during flight ……2 Exceeding cylinder head temperature ………2 Exceeding engine speed ….2 Effectivity: 582 UL BRP-Rotax Page Index-1 Edition 3 / Rev. 0 January 01/2018…
  • Page 64
    Technical documentation ….11 Temperature ……..2 Safety notice ……5, 7 Trouble shooting ……4 Special operating conditions …6 Type description ……14 Table of amendments …..1 Weights……..16 Technical data ……16 Page Index-2 BRP-Rotax Effectivity: 582 UL January 01/2018 Edition 3 / Rev. 0…
  • Page 68
    AIRCRAFT ENGINES __________________________________________________________ Engine serial no. __________________________________________________________ Type of aircraft __________________________________________________________ Aircraft registration no. ROTAX® authorized distributor WWW.FLYROTAX.COM ® and TM are trademarks of BRP-Rotax GmbH & Co KG. © 2018 BRP-Rotax GmbH & Co KG. All rights reserved…

Источник

File Specifications:

1317/1317497-582_ul_series.pdf file (31 Aug 2023)

Accompanying Data:

Rotax 582 UL series Engine PDF Operator’s Manual (Updated: Thursday 31st of August 2023 11:28:54 AM)

Rating: 4.9 (rated by 98 users)

Compatible devices: 915 iSc 3 A, 125 MAX evo, 912 ULS 3, 503 UL DCDI, 24-30-00, 914 series, 912 Series, OM-912.

Recommended Documentation:

Operator’s Manual (Text Version):

(Ocr-Read Summary of Contents of some pages of the Rotax 582 UL series Document (Main Content), UPD: 31 August 2023)

  • 39, Rotax 582 UL series Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page 3-5 January 01/2018 3.5) After 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. Warming up period Step Procedure 1 Start warming up period at approx. 2000 rpm for approx. 2 minutes. 2 Continue at 2500 rpm, duration depending on ambient temperature, until operating temperatures are .reached. 3 Check temperatures and pressure. Throttle re…

  • 61, 10) Proper disposal ENVIRONMENTAL NOTE Please observe the disposal regulations applicable in your area. General All old/used parts, liquids and chemical agents should be disposed of according to local ordinance regulations. Packaging The disposal of the packaging is the customer’s responsibility and has to take place in accordance with the current regulations of the country in which it has been removed. Liquids • Engine oil: Dispose of engine oil at the respect…

  • 51, Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page 7-3 January 01/2018 11 Overflow bottle 12 Bottle venting 13 Expansion tank 14 Cylinder head venting hose 7.2) Fuel system Generally, the engines are planned to run on a gasoline-oil mix- ture of 50:1. This mixture supplies proper engine lubrication. If the engine has been assembled for oil injection lubrication, the carburetors are supplied wit…

  • 10, Summary of amendments Summary of the relevant amendments 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 01/2018 BRP-Rotax Effectivity: 582 UL Edition 3 / Rev. 0
    …

  • 5, INTRO) Introduction Topics in this chapter Foreword BRP-Rotax GmbH & Co KG (hereinafter “BRP-Rotax”) provides “Instructions of Continued Airworthiness”, which are based on the design, the tests and certification of the engine and its components. These instructions apply only to engines and components supplied by BRP-Rotax. Before operating the engine, read this Operators Manual carefully. If any passages of the Manual are no…

  • 41, Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page 3-7 January 01/2018 Noise The air intake silencer kit will provide significant engine noise reduction. Further noise reduction may be obtained by the use of an after-muffler kit. Be aware that modifications will require a different carburetor setting. Enquire at your dealer for more information, and consult author- ized ROTAX® aircraft engines distributor or their independent Service Cente…

  • 53, 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 igni…

  • 14, Rotax 582 UL series kg Kilograms kW Kilowatt lb Pound lb/hph Pound per horsepower hour LEP List of Effective Pages l/h Liter per hour MAG Magneto Side MM Maintenance Manual mm Millimeter N Newton Nm Newtonmeter psi Pounds per square 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 Service Ins…

  • 54, Rotax 582 UL series 7.5) Propeller gearbox There are three different gearboxes available as optional extras: Type «B» gearbox Available gear ratios Crankshaft : propeller shaft 2.00 : 1 2.24 : 1 2.58 : 1 Type «C» gearbox Available gear ratios Crankshaft : 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 r…

  • 63, Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page Index-1 January 01/2018 Index A Abbreviations …………………………..3 After engine start ………………………5 B Before engine start…………………….2 C Cooling system …………………………2 Cylinder designation ………………..15 D Description of design………………..12 Description of design 582 ………….13 Dimensions ……………………………16 Direction of rot…

  • 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
    …

  • 47, 5) Performance and Fuel consumption Topics in this chapter 5.1 Performance data ………………………………………………………………………. 2 Introduction The performance and fuel information shown in this chapter are intended to give an indication 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 m…

  • 7, LEP) LIST OF EFFECTIVE PAGES Chapter Page Date cover page INTRO 1 Jan. 01 2018 2 Jan. 01 2018 LEP 1 Jan. 01 2018 2 Jan. 01 2018 TOA 1 Jan. 01 2018 2 Jan. 01 2018 1 1 Jan. 01 2018 2 Jan. 01 2018 3 Jan. 01 2018 4 Jan. 01 2018 5 Jan. 01 2018 6 Jan. 01 2018 7 Jan. 01 2018 8 Jan. 01 2018 9 Jan. 01 2018 10 Jan. 01 2018 11 Jan. 01 2018 12 Jan. 01 2018 13 Jan. 01 2018 14 Jan. 01 2018 15 Jan. 01 2018 16 Jan.…

  • 3, Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page Content-1 January 01/2018 Table of Content Chapter INTRO – Introduction 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 – Performance and Fuel consumption Chapter 7 – System Description Chapter 8 – Checks Chapter 9 – Supplement Chapter 10…

  • 52, m WARNING In case of fresh oil injection, the carburetors are fed with pure gasoline (no oil/gasoline mixture). Figure 2 1 Oil pump 2 Oil pump gear 3 Rotary valve cover assy. Lubrication 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 gearbox housing. ATTENTION Never operate engine with a dry gea…

  • 46, 4.5) Trouble shooting m WARNING Non-compliance can result in serious injuries or death! Only qualified staff (experienced two stroke mechanics) trained on this particular engine, are allowed to carry out maintenance and re- pair work. ATTENTION If the following hints regarding remedy do not solve the prob- lem, contact an authorized workshop. The engine must not be operated until the problem is rectified. Your ROTAX engine requires basicly two essentials to run. Spark and correct fuel/ air mix…

  • Rotax 582 UL series User Manual

  • Rotax 582 UL series User Guide

  • Rotax 582 UL series PDF Manual

  • Rotax 582 UL series Owner’s Manuals

Recommended: EFM-01, MBP41, 638-136, BR221.3A

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Table of Contents for Rotax 582 UL series:

  • Effectivity: 582 UL Edition 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 off side MAG Magneto side

  • 4.5) Trouble shooting m WARNING Non-compliance can result in serious injuries or death! Only qualified staff (experienced two stroke mechanics) trained on this particular engine, are allowed to carry out maintenance and re- pair work. ATTENTION If the following hints regarding remedy do not solve the prob- lem, contact an authorized workshop. The engine must not be operated until the problem is rectified. Your ROTAX engine requires basicly two essentials to run. Spark and correct fuel/ air mixt

  • 8.1) Engine preservation If the engine is not going to be used for an extended period of time, certain measures must be taken to protect engine against heat, direct sun light, corrosion and formation of residues and ingress of contaminants. In particular the water bonded by the alcohol in the fuel causes increased corrosion problems at engine stops or storage. Espe- cially affected are essential engine components such as crank- shaft bearings and conrod bearings as well as crank pins and piston pins. 8.1.1) Aft

  • 2.3) Operating media – Fuel The following fuels can be used: European standard American standard Canadian standard Min. RON 91 Min. AKI 87 EN 228 regular ASTM D 4814 CAN/CGSB-3,5 EN 228 premium Quality 1 EN 228 premium plus AVGAS 100 LL Due to its high lead content AVGAS forms increased deposits in the combustion chamber and 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

  • Page Notes-2 January 01/2018 BRP-Rotax Effectivity: 582 UL Edition 3 / Rev. 0 NOTES

  • ENVIRONMENTAL 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 Edition 3 / Rev. 0

  • Aircraft equipped with this engine must only fly in DAYLIGHT VFR conditions. • This engine is not suitable for acrobatics (inverted flight, etc.). • It should be clearly understood that the choice, selection and use of this particular engine on any aircraft is at the sole dis- cretion and responsibility of the aircraft manufacturer, assem- bler and owner/user. • Due to the varying designs, equipment and types of aircraft

  • 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

  • Exhaust gas temperatures: 582 UL DCDI mod. 99 / mod. 17 Max. 650 °C (1202 °F) Normal 500 to 620 °C (932 to 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 psi) Min. 0.2 bar (2.9 psi) Page 2-2 January 01/2018 BRP-Rotax Effectivity: 582 UL Edition 3 / Rev. 0

  • Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page Content-1 January 01/2018 Table of Content Chapter INTRO – Introduction 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 – Performance and Fuel consumption Chapter 7 – System Description

  • kg Kilograms kW Kilowatt lb Pound lb/hph Pound per horsepower hour LEP List of Effective Pages l/h Liter per hour MAG Magneto Side MM Maintenance Manual mm Millimeter N Newton Nm Newtonmeter psi Pounds per square 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 Service Instruction SL Service Letter TC Type certificate TOA Table Of Amendment US g

  • LEP) LIST OF EFFECTIVE PAGES Chapter Page Date cover page INTRO 1 Jan. 01 2018 2 Jan. 01 2018 LEP 1 Jan. 01 2018 2 Jan. 01 2018 TOA 1 Jan. 01 2018 2 Jan. 01 2018 1 1 Jan. 01 2018 2 Jan. 01 2018 3 Jan. 01 2018 4 Jan. 01 2018 5 Jan. 01 2018 6 Jan. 01 2018 7 Jan. 01 2018 8 Jan. 01 2018 9 Jan. 01 2018 10 Jan. 01 2018 11 Jan. 01 2018 12 Jan. 01 2018 13 Jan. 01 2018 14 Jan. 01 2018 15 Jan. 01 2018 16 Jan. 01 2018 17 Jan. 01 2018 1

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Источник

Before starting the engine, read the Operators Manual, as it contains

important safety relevant information. Failure to do so may result in per-

sonal injuries including death. Consult the original eq uipment

manufactur-ers handbook for additional instructions!

These technical data and the information embodied therein are the property of

BRP-Rotax GmbH & CO KG, Austria, acc, BGBI 1984 no. 448, and shall not,

without prior written permission of BRP-Rotax GmbH & Co KG, be disclosed in

whole or in part to third 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.

ROTAX

is a trade mark of BRP-Rotax GmbH & Co KG. In the following

®

document the short form of BRP-Rotax GmbH & Co KG = BRP-Rotax is used.

Other product names in this documentation are used purely for ease of

identification and may be trademarks of the respective company or owner.

Copyright 2018 © — all rights reserved.

Translation into other languages might be performed in the course of language

localization but does not lie within ROTAX ® scope of responsibility.

In any case the original text in English language and the metric units are

authoritative.

WARNING

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Rotax 582 UL series Operator’s manual

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  • Operator’s manual for Rotax 582 UL series
  • rotax-582-ul-series-operator-s-manual-68_manual.pdf
  • 68 |

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  • Effectivity: 582 UL Edition 3 / Rev. 0 BRP-Rotax Page 3-3 January 01/2018 • Check operation of both ignition circuits Propeller • Inspect propeller for splits and chips. If any damage, repair and/or rebalance before use • Verify security of propeller mou …

  • 1) General note Topics in this chapter 1.1 General ……………………………………………………………………………………2 1.2 Abbreviations and terms ………………………………………………………………3 1.3 Safet …

  • Summary of amendments Summary of the relevant amendments 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 01/2018 BRP …

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