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Rotax 898851, Руководство оператора

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Страница 1: ...AIRCRAFT ENGINES ref no OM 915 i A part no 898851 OPERATORS MANUAL FOR ROTAX ENGINE TYPE 915 i A SERIES picture ROTAX 915 iS 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 2017 all rights reserved ROTA...

Страница 3: ...ter 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...

Страница 4: ...Page Notes 2 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 NOTES...

Страница 5: ...formation 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 procedures...

Страница 6: ...Page Notes 2 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 NOTES...

Страница 7: ...Dec 01 2017 5 Dec 01 2017 6 Dec 01 2017 7 Dec 01 2017 8 Dec 01 2017 Chapter Page Date 3 1 Dec 01 2017 2 Dec 01 2017 3 Dec 01 2017 4 Dec 01 2017 5 Dec 01 2017 6 Dec 01 2017 7 Dec 01 2017 8 Dec 01 2017...

Страница 8: ...017 9 Dec 01 2017 10 Dec 01 2017 11 Dec 01 2017 12 Dec 01 2017 Chapter Page Date 13 Dec 01 2017 14 Dec 01 2017 15 Dec 01 2017 16 Dec 01 2017 8 1 Dec 01 2017 2 Dec 01 2017 3 Dec 01 2017 4 Dec 01 2017 9...

Страница 9: ...048 cur rent no chapter page date of change remark for appro val date of appro val from authori ties date of inclu sion signa ture 0 INTRO all Dec 01 2017 DOA 0 LEP all Dec 01 2017 DOA 0 TOA all Dec 0...

Страница 10: ...s Summary of the relevant amendments in this context but without any claim to completeness current no chap ter page date of change comments Page TOA 2 December 01 2017 BRP Rotax Effectivity 915 i A Se...

Страница 11: ...is chapter 1 1 General 2 1 2 Abbreviations and terms 3 1 3 Safety 7 1 4 Safety information 9 1 5 Technical documentation 12 1 6 Type description 14 Effectivity 915 i A Series Edition 0 Rev 0 BRP Rotax...

Страница 12: ...s information to the end customer in an ap propriate way e g within the aircraft specific Operators Manual For detailed information related to aircraft and aircraft engine in stallation maintenance sa...

Страница 13: ...lutions per minute A Ampere AAPTS Ambient Air Pressure Temperature Sensor AC alternating current Ah Ampere hour A C Aircraft AR as required assy assembly ASB Alert Service Bulletin ACG Austro Control...

Страница 14: ...deral Aviation Administration FAR Federal Aviation Regulations hr hours HIC A Harness Interface Connector A HIC B Harness Interface Connector B IFR Instrument Flight Rules INJ 1 8 Injector 1 8 IPC Ill...

Страница 15: ...TFE Polytetrafluoroethylene PTO Power Take Off Rev Revision ROTAX is a trademark of BRP Rotax GmbH Co KG RON Research Octane Number RON 424 ROTAX Norm 424 s v still valid only Illustrated Parts Catalo...

Страница 16: ...nce Overhaul V Volt VFR Visual Flight Rules LEP List of Effective Pages MM Maintenance Manual XXXX shows the serial component number Page 1 6 December 01 2017 BRP Rotax Effectivity 915 i A Series Edit...

Страница 17: ...remove 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 a...

Страница 18: ...Environmental notes give you tips on environmental protection A revision bar outside the page margin indicates a change to text or graphic Page 1 8 December 01 2017 BRP Rotax Effectivity 915 i A Seri...

Страница 19: ...rcraft manufacturer assem bler and owner user Due to the varying designs equipment and types of aircraft BRP Rotax grants no warranty on the suitability of its en gine s use on any particular aircraft...

Страница 20: ...ion is not included in the ROTAX engine package Verification to the latest regulations such as FAR or EASA has to be conducted by the aircraft manufacturer Engine log book Keep an engine log book and...

Страница 21: ...for several minutes before turning off the engine Vacuum pump This engine may be equipped with a vacuum pump The safety warning accompanying the vacuum pump must be giv en to the owner operator of th...

Страница 22: ...tatus 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 revision pro vided on the ROTAX W...

Страница 23: ...2017 TYPICAL indicates a general view which may not represent ex act details NOTE The Illustrations in this Manual are stored in a graphic data base system and are provided with a consecutive irrelev...

Страница 24: ...4 cylinder horizontally opposed turbo charged engine Certifica tion iSc Certified to EASA CS E TC No EASA E 121 iS Approved to ASTM F2339 Configura tion 3 Propeller shaft with flange for constant spe...

Страница 25: ...icants 7 Introduction The operating limits for certified engines are also given in the type certificate for the relevant engine type This chapter of the Operators Manual contains the operating limits...

Страница 26: ...t system See latest Installation Manual ISA Condition International Standard Atmosphere Engine speed Parameter Min Max Engine speed at idle 1800 rpm Engine speed 5800 rpm max 5 minutes Performance The...

Страница 27: ...ne operation at zero gravity and in negative g condition Parameter Min Max Acceleration 0 5 g max 5 seconds Static roll angle The dry sump lubrication system warrants lubrication in every flight situa...

Страница 28: ...operation 50 C 120 F 130 C 266 F ATTENTION Operating the engine below 90 to 110 C 194 to 230 F may lead to formation of condensation water in the lubrication sys tem To evaporate possibly accumulated...

Страница 29: ...lit at 3 Liter hour Fuel consumption 500 C 932 F Ambient temperature Parameter Min Max Ambient temperature at ground idle start procedure and warm up 20 C 4 F 50 C 120 F Ambient temperature at normal...

Страница 30: ...s documentation Mixture ATTENTION Obey the operating media manufacturer s instructions 2 3 Operating media Fuel ATTENTION Obey the latest edition of Service Instruction SI 915 i 001 for the selection...

Страница 31: ...the selection of suitable lubricants refer to the additional in formation in the Service Information SI 915 i 001 latest edition Oil consumption Max 0 06 l h 0 13 liq pt h Oil specification Use only...

Страница 32: ...iations than single grade oils They are suitable for use throughout the seasons ensure rapid lubrication of all engine components at cold start and get less fluid at higher temperatures Table of lubr...

Страница 33: ...erating and maintenance instructions The following description of procedures depends on the respective type of installation in the aircraft and shall therefore only be seen functionally NOTE The contr...

Страница 34: ...ntenance Manual is necessary Do not release the engine in to service before rectification Coolant level ATTENTION Operating media must be observed Inappropriate coolant quantity can lead to serious en...

Страница 35: ...Effectivity 915 i A Series Edition 0 Rev 0 BRP Rotax Page 3 3 December 01 2017 Figure 1 Expansion tank 1 Radiator cap 2 Expansion tank coolant Figure 2 Overflow bottle 1 Overflow bottle 2 Coolant...

Страница 36: ...mpression 2 Verify free movement of throttle valve and the complete range 3 Inspect for damages leakage and general condition of exhaust system and turbocharger 4 Visual inspection for mechanical and...

Страница 37: ...red to when refilling oil Step Procedure 1 NOTE Propeller shouldn t be turned excessively reverse the normal direction of engine rotation Remove bayonet cap from the oil tank turn the propeller slowly...

Страница 38: ...nt Do not harm the environment by spilling oil Dispose of oil in an envi ronmentally friendly manner 3 3 Engine start m WARNING Non compliance can result in serious injuries or death Do not start the...

Страница 39: ...airframe ground and EMS ground will activate Start Power The temporary power supply must be maintained during steps 4 5 6 Example Symbolic Start Power Switch HOLD 5 Check if Warning In dicators illum...

Страница 40: ...e drop between Terminal 2 and Termi nal 8 permanent or oscillating is detected perform Lane and Ignition Check See abnormal operation if the voltage drop still persists HIC B If a 12 V voltage drop be...

Страница 41: ...oltage drop between Terminal 2 and Termi nal 8 permanent or oscillating is detected shut OFF engine and perform troubleshooting HIC B If a 12 V voltage drop between Terminal 2 and Termi nal 10 permane...

Страница 42: ...is detected shut OFF engine and perform troubleshooting Display CAN A B Check and ensure compliance with opera tional limits Example Symbolic Warning Lamp A Check Warning Lamp B Check Pilot Display Ch...

Страница 43: ...cillating is detected shut OFF engine and perform troubleshooting HIC B If a 12 V voltage drop between Terminal 2 and Termi nal 10 permanent or oscillat ing is detected shut OFF engine and perform tro...

Страница 44: ...compliance with opera tional limits Example Symbolic Warning Lamp A Check Warning Lamp B Check Pilot Display Check 2 Set Throttle Valve as required Set linearized throttle position so that engine spee...

Страница 45: ...olic Lane select Switch B OFF 8 Observe engine speed Display CAN A B Check en gine speed Example Symbolic Pilot Display Check ATTENTION Engine speed may not drop increase more than 250 rpm If the fuel...

Страница 46: ...ng Lane and Ignition check some sensor values are not displayed de pending on the activation of the Lanes Following sensor values are not available if Lane A is turned OFF and Lane B is activated Cool...

Страница 47: ...l 10 permanent or oscillat ing is detected shut OFF engine and perform troubleshooting Display CAN A B Check and ensure compliance with opera tional limits Example Symbolic Warning Lamp A Check Warnin...

Страница 48: ...le Symbolic Warning Lamp A Check 8 Deactivate ECU Lane B HIC B Disconnect Terminal 1 and Terminal 9 to turn OFF ECU Lane B Example Symbolic Lane Select Switch B OFF 9 Wait 15 seconds Example Symbolic...

Страница 49: ...00 rpm and continue with Fuel pump check Example Symbolic Set Throttle Fuel pump check It must be ensured that both fuel pumps are working and no loss of power or irregular running by deactivation of...

Страница 50: ...fied Step Step Description Procedure 5 Activate Fuel pump 1 HIC A Disconnect Terminal 3 and Terminal 9 to deactivate Fuel pump 1 Example Symbolic Fuel pump 1 OFF 6 Deactivate Fuel pump 2 HIC A Disconn...

Страница 51: ...is detected shut OFF engine and perform troubleshooting HIC B If a 12 V voltage drop between Terminal 2 and Termi nal 10 permanent or oscillat ing is detected shut OFF engine and perform troubleshooti...

Страница 52: ...ng of the fuel pumps is only allowed in emergency situations Step Step Description Procedure 5 Deactivate Fuel pumps HIC A Disconnect Terminal 3 and terminal 9 to turn OFF Fuel pump 1 HIC B Disconnect...

Страница 53: ...ands 5 4 1 3 Engine on fire or fire in the engine compartment 5 4 2 Failures during engine start 6 4 2 1 Engine does not start 6 4 3 Re Start during flight 6 4 4 The sprag clutch fails to decouple fro...

Страница 54: ...uct checks as per maintenance Manual Line Chapter 05 50 00 before the next flight Only qualified staff authorized by the Aviation Authorities trained on this particular engine is allowed to carry out...

Страница 55: ...missible Land the aircraft Oscillating 0 12 V Oscillating 0 12 V Flight not permissible Land the aircraft Oscillating 0 12 V 12 V Flight not permissible Land the aircraft 12 V 0 V Flight not permissib...

Страница 56: ...ng the EMS the airframe will not be supplied with electrical power by an internal generator This failure condition will be detected by the EMS Therefore see section Failures detected by the EMS for ap...

Страница 57: ...n the engine compartment ATTENTION Carry out emergency procedures as prescribed in the flight man ual of the engine manufacturer Aircraft Manufacturer is responsible for defining a procedure for this...

Страница 58: ...flight by windmilling but the speed is not sufficient to start the engine the electric starter can be used It is not required to wait until the propeller stand still 4 4 The sprag clutch fails to dec...

Страница 59: ...and carry out precautionary landing Exceeding fuel pressure If the pressure is too high switch the AUX pump OFF If this has no effect then limited flight operation with reduced power is possible If th...

Страница 60: ...Page Notes 8 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 NOTES...

Страница 61: ...mance and Fuel consumption Topics in this chapter 5 1 Performance data and fuel consumption 2 5 2 Explanation of the parameters 2 Effectivity 915 i A Series Edition 0 Rev 0 BRP Rotax Page 5 1 December...

Страница 62: ...nd throttle position ECU_throttle_lin Critical Altitude The engine was designed for a critical altitude up to 15000 ft 5 2 Explanation of the parameters Parameters Explantaion Case Number No Unit Sequ...

Страница 63: ...elivered power will be up to 1 4 kW higher than the stated power in the engine deck Therefore power loss due to the use of AVGAS is taken into account Fuel Flow kg h Fuel flow at given ambient engine...

Страница 64: ...Page Notes 4 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 NOTES...

Страница 65: ...troduction This chapter of the Operator Manual contains information about the general engine specification as well as a description of cooling system fuel system lubrication system electric system and...

Страница 66: ...controlling fuel injection ignition etc Propeller drive via gearbox with integrated mechanical shock absorber and overload clutch Oil tank Electric starter Turbocharged Electronic pneumatic control of...

Страница 67: ...tax Page 7 3 December 01 2017 7 1 3 Engine components Figure 1 Engine components 1 Propeller gearbox 2 ECU 3 Fusebox 4 Intercooler 5 Airbox 6 Wiring harness 7 Turbocharger 8 Air baffle 9 Electric star...

Страница 68: ...n of rotation Direction of rota tion on propeller shaft Direction of rotation on propeller shaft counter clockwise viewed from the front Figure 3 Normal direction of propeller rotation engine Page 7 4...

Страница 69: ...top of the engine allows for coolant expansion Expansion tank From the expansion tank the coolant is sucked back to the water pump In common installations the coolant passes a radi ator in between Ad...

Страница 70: ...fuel rails The fuel pres sure regulator 6 ensures that the pressure differential between the fuel injectors and the intake manifold remains constant This allows injecting same quantity of fuel indepe...

Страница 71: ...ing on the engine installation trough the oil cooler to the points of lubrication in the engine and the turbo charger The escaping oil emerging from the points of lubrication accu mulates on the botto...

Страница 72: ...er oil sump 9 Oil cooler Oil temperature sensor The oil temperature sensor for reading of the oil temperature is located on the crankcase on the mag side of the engine Oil pressure sensor The oil pres...

Страница 73: ...ber 01 2017 7 5 Electric system This System is responsible for supplying the Engine Manage ment System EMS and the Airframe with electrical power It consists of the Fusebox with Regulators and the Int...

Страница 74: ...l electric supply system changes to fail safe mode where Generator 2 again is in charge to supply the EMS In fail safe mode Genera tor 2 is not able to charge external power sources or supply the airf...

Страница 75: ...me measurement values and send the same output signals Non redundant sensors e g oil pressure sensors are connected to one Lane only and serve for the expanded monitoring of the en gine functionality...

Страница 76: ...s a maintenance and a display interface CAN bus While the maintenance interface is required to work with the BUDS Aircraft Diagnostic Software to perform vari ous diagnostic and maintenance activities...

Страница 77: ...BRP Rotax Page 7 13 December 01 2017 7 6 Air intake system and Boost pressure control Figure 10 Air intake system 1 Airfilter connection 2 Air intake hose 3 Turbo charger 4 Intercooler 5 Pop OFF valv...

Страница 78: ...exhaust gases have to pass the turbine The waste gate is powered by the boost pressure from the com pressor Pneumatic valves actuated by the ECU control the amount of the boost pressure necessary to a...

Страница 79: ...the air filter Boost Pressure Sensor BPS The boost pressure sensor for reading of the boost pressure is located right before the throttle near the overboost valve Manifold Air Pres sure Sensor MAP Th...

Страница 80: ...ther in the exhaust manifold From there the exhaust gas pass the turbine side of the turbo charger depending on the waste gate position From there the exhaust gases leave the engine thru the muffler E...

Страница 81: ...Only qualified staff authorized by the Aviation Authorities trained on this particular engine is allowed to carry out maintenance and repair work NOTE Other useful information for service and airworth...

Страница 82: ...of 5 min engine oil temperature between 50 to 70 C 122 to 160 F 2 Shut off engine 3 Allow the engine to cool down 4 Change oil 5 Remove the top spark plugs and spray all openings with corrosion inhibi...

Страница 83: ...e back to operation If preservation including oil change took place within a year of storage oil renewal will not be necessary For longer storage periods repeat preservation annually Step Procedure 1...

Страница 84: ...Page Notes 4 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 NOTES...

Страница 85: ...be filled out and sent to the responsible ROTAX authorized aircraft engines distributor or their independent Service Center NOTE The form is also available from the official ROTAX AIRCRAFT ENGINES We...

Страница 86: ...9 1 Form Figure 1 Form Page 9 2 December 01 2017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0...

Страница 87: ...espective 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 Flammable m...

Страница 88: ...AX 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 manufactu...

Страница 89: ...542568 29 65 1 3899 265 95 24 5800 0 724 18 98 8 8999 93 73580146 28 93 1 3741 260 05 25 5800 0 644 24 98 8 11998 92 50114367 28 58 1 3685 254 05 26 5800 0 572 30 98 8 15000 93 98842135 29 14 1 3821 2...

Страница 90: ...231 55 71 5800 1 013 0 56 5 0 7 693672667 5 78 0 3762 278 35 72 5800 0 908 6 56 5 2999 4 734707685 5 27 0 3318 272 65 73 5800 0 812 12 56 5 5997 3 306534463 5 01 0 3029 266 75 74 5800 0 724 18 56 5 89...

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Страница 92: ...800 0 572 15 99 4 15000 98 7425386 31 26 1 4412 263 45 177 5800 0 527 19 99 4 17001 99 62390871 31 13 1 4391 259 55 178 5800 0 485 23 99 4 18999 98 07559319 30 23 1 4020 255 75 179 5800 0 446 27 99 4...

Страница 93: ...879464 8 56 0 5263 286 25 223 5800 0 812 3 72 5997 18 66677549 7 76 0 4754 280 35 224 5800 0 724 3 72 8999 16 10175907 7 05 0 4293 274 45 225 5800 0 644 9 72 11998 13 52934195 6 44 0 3838 268 55 226 5...

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Страница 95: ...485 8 100 18999 99 45344938 31 33 1 4170 271 25 329 5800 0 446 12 100 21001 93 17776131 29 04 1 3539 267 45 330 5800 0 410 16 100 22999 86 1847955 27 06 1 2946 263 25 331 5800 1 013 30 99 4 0 101 5744...

Страница 96: ...9 32 88290382 10 73 0 6290 289 55 375 5800 0 644 6 84 5 11998 29 00280731 9 92 0 5729 283 55 376 5800 0 572 0 84 5 15000 25 79846647 9 15 0 5252 277 75 377 5800 0 527 4 84 5 17001 23 98035841 8 66 0 4...

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Страница 100: ...1 95 580 5500 0 410 1 99 4 22999 72 20276556 23 03 1 1577 278 05 581 5500 1 013 45 98 8 0 93 05864384 29 33 1 3551 323 05 582 5500 0 908 39 98 8 2999 92 00926255 28 61 1 3535 317 35 583 5500 0 812 33...

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Страница 102: ...21 60 0 9694 240 05 679 5000 0 446 42 97 4 21001 70 60089247 21 34 0 9041 236 05 680 5000 0 410 46 97 4 22999 66 51691313 20 72 0 8311 232 05 681 5000 1 013 0 94 1 0 67 4075405 18 84 1 0892 277 15 682...

Страница 103: ...0 572 30 100 15000 67 20836699 21 83 0 9685 247 85 727 4500 0 527 34 100 17001 65 26387332 21 23 0 8900 243 75 728 4500 0 485 38 100 18999 62 70991006 20 38 0 8034 239 75 729 4500 0 446 42 100 21001 5...

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Страница 113: ...0 527 11 100 17001 59 65505852 19 81 1 0775 289 15 1208 4500 0 485 7 100 18999 57 31658391 18 90 1 0345 285 15 1209 4500 0 446 3 100 21001 54 25224811 17 73 0 9826 281 15 1210 4500 0 410 1 100 22999...

Страница 114: ...36 47955111 10 79 0 7473 310 65 1254 4500 0 724 27 84 5 8999 33 1497912 9 92 0 6906 304 85 1255 4500 0 644 21 84 5 11998 29 23437644 8 98 0 6271 299 25 1256 4500 0 572 15 84 5 15000 25 03407453 7 89 0...

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Страница 116: ...34 95 1350 4000 0 410 46 72 22999 9 351427517 4 74 0 3111 230 95 1351 4000 1 013 0 56 5 0 14 8065624 5 86 0 5086 276 05 1352 4000 0 908 6 56 5 2999 13 29838274 5 32 0 4728 270 25 1353 4000 0 812 12 56...

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Страница 137: ...Management System 10 Engine not responding on throttle position commands 5 Engine preservation and storage 2 Engine run up 11 Engine shut off 19 Engine start 6 Exceedance of operational limits 6 Expl...

Страница 138: ...017 BRP Rotax Effectivity 915 i A Series Edition 0 Rev 0 S Safety notice 7 9 Sprag clutch Starter 6 T Table of amendments 1 Technical data 2 Technical documentation 12 Terms 3 Turbocharger Exhaust sys...

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Страница 140: ...________________________________________ Type of aircraft __________________________________________________________ Aircraft registration no ROTAX authorized distributor WWW FLYROTAX COM www abm at a...

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