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Rotax 898851, Operator'S Manual

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Rotax 898851 Operator'S Manual Download Page 94

Number rpm p_amb T_amb Throttle

alt

power

FuelFlow

p_Plenum T_Plenum

-

RPM

bar

C

%

ft

kW

kg/h

bar

K

254 5500

0,724

-3

99,4

8999 94,13409003

29,45

1,3668

275,05

255 5500

0,644

-9

99,4

11998 93,24979463

29,07

1,3546

269,15

256 5500

0,572

-15

99,4

15000 94,03513813

29,38

1,3905

263,25

257 5500

0,527

-19

99,4

17001 95,42379408

29,75

1,3865

259,25

258 5500

0,485

-23

99,4

18999 95,15075552

29,26

1,3636

255,35

259 5500

0,446

-27

99,4

21001 92,01207992

28,12

1,3170

251,55

260 5500

0,410

-31

99,4

22999 85,73831353

26,89

1,2372

247,65

261 5500

1,013

15

98,8

0 93,88515075

29,58

1,3753

292,85

262 5500

0,908

9

98,8

2999 92,57934477

28,61

1,3592

286,95

263 5500

0,812

3

98,8

5997 90,93977423

27,90

1,3241

281,05

264 5500

0,724

-3

98,8

8999 88,92753139

26,95

1,2966

274,95

265 5500

0,644

-9

98,8

11998 87,33727969

26,33

1,2748

269,15

266 5500

0,572

-15

98,8

15000 88,70951834

26,88

1,3141

263,15

267 5500

0,527

-19

98,8

17001 90,84297885

27,44

1,3229

259,15

268 5500

0,485

-23

98,8

18999 91,11427758

27,26

1,3091

255,25

269 5500

0,446

-27

98,8

21001 88,42109635

26,43

1,2690

251,25

270 5500

0,410

-31

98,8

22999 82,68373657

25,41

1,1956

247,45

271 5500

1,013

15

97,4

0 87,46870538

26,53

1,2948

292,85

272 5500

0,908

9

97,4

2999 84,81463841

24,99

1,2646

286,95

273 5500

0,812

3

97,4

5997 81,28462149

23,41

1,2015

280,95

274 5500

0,724

-3

97,4

8999 77,48765238

21,91

1,1457

274,85

275 5500

0,644

-9

97,4

11998 75,19387424

21,15

1,1120

268,95

276 5500

0,572

-15

97,4

15000 77,55179913

21,93

1,1529

262,95

277 5500

0,527

-19

97,4

17001 80,47319962

22,68

1,1794

258,95

278 5500

0,485

-23

97,4

18999 81,44103495

22,95

1,1805

255,05

279 5500

0,446

-27

97,4

21001 79,52478591

22,68

1,1521

251,05

280 5500

0,410

-31

97,4

22999 74,98170382

22,10

1,0931

247,05

281 5500

1,013

15

94,1

0 71,52872505

20,62

1,1093

292,55

282 5500

0,908

9

94,1

2999 66,67151938

18,60

1,0537

286,65

283 5500

0,812

3

94,1

5997

61,0464453

16,63

0,9660

280,55

284 5500

0,724

-3

94,1

8999 56,08564836

15,46

0,8869

274,65

285 5500

0,644

-9

94,1

11998 54,63607011

15,42

0,8564

268,65

286 5500

0,572

-15

94,1

15000 57,22842779

16,09

0,8840

262,75

287 5500

0,527

-19

94,1

17001

59,3785806

16,54

0,9074

258,75

288 5500

0,485

-23

94,1

18999 60,17971906

16,79

0,9134

254,75

289 5500

0,446

-27

94,1

21001 59,10062305

16,78

0,8967

250,75

290 5500

0,410

-31

94,1

22999 56,47275517

16,58

0,8603

246,75

291 5500

1,013

15

84,5

0 44,44179185

13,63

0,8036

292,05

292 5500

0,908

9

84,5

2999 41,62633233

12,69

0,7483

286,25

293 5500

0,812

3

84,5

5997

38,6357526

11,85

0,6971

280,15

294 5500

0,724

-3

84,5

8999 34,91873267

11,08

0,6441

274,25

295 5500

0,644

-9

84,5

11998 31,32857079

10,32

0,5914

268,45

296 5500

0,572

-15

84,5

15000 28,15848278

9,49

0,5431

262,65

297 5500

0,527

-19

84,5

17001 26,14786993

8,92

0,5130

258,75

298 5500

0,485

-23

84,5

18999 24,28432094

8,39

0,4852

254,85

299 5500

0,446

-27

84,5

21001 22,58145169

7,95

0,4596

251,05

300 5500

0,410

-31

84,5

22999 21,04721733

7,62

0,4364

247,35

APPENDIX

Performance data and Fuel consumption model

APPENDIX

Edition 0/Rev. 0

December 01 2017

Summary of Contents for 898851

Page 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...

Page 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...

Page 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...

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

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 91: ...35 16 87 0 9616 265 45 124 5500 0 724 18 94 1 8999 56 49366466 15 84 0 8976 259 55 125 5500 0 644 24 94 1 11998 55 38485484 15 94 0 8815 253 55 126 5500 0 572 30 94 1 15000 58 17634027 16 73 0 9025 24...

Page 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...

Page 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...

Page 94: ...1120 268 95 276 5500 0 572 15 97 4 15000 77 55179913 21 93 1 1529 262 95 277 5500 0 527 19 97 4 17001 80 47319962 22 68 1 1794 258 95 278 5500 0 485 23 97 4 18999 81 44103495 22 95 1 1805 255 05 279 5...

Page 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...

Page 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...

Page 97: ...10 274 35 428 5500 0 485 8 98 8 18999 88 01821911 26 03 1 2735 270 35 429 5500 0 446 12 98 8 21001 84 31471604 24 84 1 2465 266 45 430 5500 0 410 16 98 8 22999 78 8808922 23 57 1 2102 262 65 431 5500...

Page 98: ...75 5500 0 644 6 56 5 11998 2 327691822 4 44 0 2490 283 65 481 5800 1 013 45 100 0 103 7771844 33 60 1 4887 323 15 482 5800 0 908 39 100 2999 104 017314 33 84 1 5031 317 35 483 5800 0 812 33 100 5997 1...

Page 99: ...93260538 15 40 0 9189 293 05 527 5800 0 527 11 94 1 17001 58 17329394 15 66 0 9244 289 05 528 5800 0 485 7 94 1 18999 57 96799899 15 75 0 9137 285 05 529 5800 0 446 3 94 1 21001 55 86137716 15 61 0 8...

Page 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...

Page 101: ...3308 292 65 627 5500 0 527 11 72 17001 8 827037232 5 03 0 3042 288 65 628 5500 0 485 7 72 18999 7 128032754 4 73 0 2794 284 55 629 5500 0 446 3 72 21001 5 552272968 4 47 0 2569 280 45 630 5500 0 410...

Page 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...

Page 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...

Page 104: ...57384941 12 08 0 8523 271 25 773 4500 0 812 12 84 5 5997 38 8642317 11 29 0 7930 265 35 774 4500 0 724 18 84 5 8999 34 99534968 10 52 0 7230 259 45 775 4500 0 644 24 84 5 11998 31 68753056 9 70 0 6465...

Page 105: ...251 35 820 5000 0 410 31 99 4 22999 75 31665877 23 58 1 0472 247 45 821 5000 1 013 15 98 8 0 84 36614695 25 76 1 3156 292 35 822 5000 0 908 9 98 8 2999 83 52486879 24 55 1 3020 286 55 823 5000 0 812 3...

Page 106: ...90 0 3641 262 15 867 5000 0 527 19 72 17001 12 20222922 5 55 0 3332 258 05 868 5000 0 485 23 72 18999 10 47766046 5 23 0 3056 253 95 869 5000 0 446 27 72 21001 8 905829888 4 95 0 2824 249 85 870 5000...

Page 107: ...0 0 9360 263 05 917 4500 0 527 19 97 4 17001 55 42371492 16 24 0 8909 259 05 918 4500 0 485 23 97 4 18999 54 05532375 15 98 0 8312 255 05 919 4500 0 446 27 97 4 21001 51 669736 15 43 0 7586 250 95 920...

Page 108: ...000 0 724 12 100 8999 87 13295007 27 01 1 3537 290 15 965 5000 0 644 6 100 11998 86 99739162 27 72 1 3379 284 25 966 5000 0 572 0 100 15000 86 47079903 27 80 1 3078 278 25 967 5000 0 527 4 100 17001 8...

Page 109: ...43 13 96 0 8254 262 15 1011 5000 1 013 30 84 5 0 43 78631555 13 26 0 8201 307 15 1012 5000 0 908 24 84 5 2999 41 54775693 12 40 0 7747 301 15 1013 5000 0 812 18 84 5 5997 38 81908735 11 60 0 7300 295...

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Page 117: ...5 0 5794 247 15 1397 3500 0 527 34 97 4 17001 22 32024178 6 85 0 4603 243 45 1398 3500 0 485 38 97 4 18999 19 65738397 6 19 0 3507 239 45 1399 3500 0 446 42 97 4 21001 17 52228191 5 67 0 2596 235 35 1...

Page 118: ...4 4000 0 724 3 100 8999 52 82790932 16 37 1 1240 274 45 1445 4000 0 644 9 100 11998 48 53740077 15 37 1 0019 268 65 1446 4000 0 572 15 100 15000 42 2147823 13 74 0 8520 262 75 1447 4000 0 527 19 100 1...

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Page 122: ...572 306 35 1632 4000 0 908 24 97 4 2999 53 59695912 14 98 1 1778 300 65 1633 4000 0 812 18 97 4 5997 50 21430645 13 88 1 1278 295 15 1634 4000 0 724 12 97 4 8999 46 85134587 12 89 1 0577 289 45 1635 4...

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Page 125: ...3 4000 0 812 33 99 4 5997 53 57112197 15 87 1 1561 310 05 1774 4000 0 724 27 99 4 8999 50 70466538 15 05 1 1035 304 45 1775 4000 0 644 21 99 4 11998 45 07037907 13 81 0 9998 298 85 1776 4000 0 572 15...

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Page 129: ...41 0 1191 229 05 1961 3000 1 013 0 94 1 0 33 03534968 9 82 0 9932 275 25 1962 3000 0 908 6 94 1 2999 31 19436206 9 42 1 0004 269 35 1963 3000 0 812 12 94 1 5997 28 03657184 8 72 0 9028 263 45 1964 30...

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Page 135: ...6 318667534 3 91 0 3867 277 95 2470 3000 0 410 1 72 22999 5 583626302 3 81 0 3576 274 05 2471 3000 1 013 45 56 5 0 14 73000322 6 02 0 6225 319 55 2472 3000 0 908 39 56 5 2999 12 82960742 5 30 0 5881...

Page 136: ......

Page 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...

Page 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...

Page 139: ......

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

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