Rotax 898851 Скачать руководство пользователя страница 52

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NOTE

The ECU needs to deactivated first. Shutting of the engine by
deactivating the fuel supply may result in fault and failure en-
tries in the ECU. Shutting down the engine by shutting of the
fuel pumps is only allowed in emergency situations.

Step

Step Description

Procedure

Deactivate Fuel pumps

HIC A: Disconnect Terminal 3 and
terminal 9 to turn OFF Fuel pump 1
HIC B: Disconnect Terminal 3 and
terminal 11 to turn OFF Fuel pump
2

Example (Symbolic)

Fuel pump 1:

OFF

Fuel pump 2:

OFF

Page 3-20
December 01 2017

BRP-Rotax

Effectivity: 915 i A Series

Edition 0 / Rev. 0

Содержание 898851

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...

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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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