INSTALLATION MANUAL FOR JABIRU 2200 AIRCRAFT ENGINE
Contents
1. OPTIONAL FRONT 1 73 BED MOUNT Figure 1 Drawing 9404041 1 Engine Dimensions meo Te ST T TT T WGatewayMibraryMilesvengine manuals 2200 engine manualsWHydraulic LiftersWorking copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty Me Installation Manual Jabiru 2200 Aircraft Engine 6 Denomination Of Cylinders 05 E Coro M tC m 5 or F CN H 1 H 0 Z ue Drawing 9483093 1 Figure 2 Cylinder Firing Order Cylinder Firing Order 1 3 2 4 Dated March 2006 Page 10 REVISION Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft Mee Installation Manual Jabiru 2200 Aircraft Engine ie w NOTE 1 ALL DISTRIBUTORS SHOWN LOOKING FROM THE PROP DRIVE END OF THE ENGINE 2 EXHAUST amp INTAKE REFER TO THE POSITION OF THE SPARK PLUGS IN THE CYLINDER ON THE EXHAU2. A N gt E E z gt u x L_Installation_Manual_2200_Rev_0 doc Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies H Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft Pty Pta Installation Manual Jabiru 2200 Aircraft Engine Figure 17 Engine Mount Detail uel line from irewall fitting o mechanical uel pump uel line from nechanical uel pump to carburettor Figure 18 Fuel Connections General Fuel line from firewall Fuel line from fuel Fuel pump breather line fitting to fuel pump pump to carburettor to be vented overboard Figure 19 Fuel Connection Detail i Connect the fuel line to fuel pump Refer to photo Ensure the fireproof sleeve is in place ToT T E Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies VHL_ Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty Ms gt Installation Manual Jabiru 2200 Aircraft Engine j Ensure the fuel line from fuel pump to the carburettor is connected amp protected by fireproof sleeve k Ensure that the fuel overflow line is in place and secured to vent overboard Oil vent line from Oil vent line Oil collector bottle engine breather venting overboard Figure 20 Oil Collector
3. Installation Manual Jabiru 2200 Aircraft Engine e 6 T L ZE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft 9e i Installation Manual Jabiru 2200 Aircraft Engine 21 Appendix E Typical Installation Gradual bends only in SCAT hose Glass duct removes a sharp corner in SCAT tube Glass duct prevents bunched SCAT hose from blocking sensor holes on carburettor inlet Gradual bends only in SCAT hose CHT cold junction positioned well clear of engine Glass duct removes a sharp corner in SCAT tube Glass duct prevents bunched SCAT hose from blocking sensor holes on E carburettor inlet Figure 10 Intake Detail 2 Dated March 2006 Page 35 WGatewayNibraryMilesvengine manuals2200 engine manuals LiftersWorking Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM REVISION Jabiru Aircraft pty Me Installation Manual Jabiru 2200 Aircraft Engine Ram air ducts fixed to Oil cooler soft engine with rocker cover mounted on Torque on propeller cap screws front amp rear rubber grommets bolts 6 ft Ib Figure 11 Engine Installation 1 ir pipes direct ooling air from ram air ducts over coils Figure 1
4. Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 14 Cooling Systems 141 Air Ducts The engine should be installed using RAM AIR ducts provided with the engine Each duct must have a 25mm hole at the inside top front to bleed air over the crankcase Cylinder and cylinder head cooling is achieved by ducting air over the cylinders and heads The Static Air Pressure inside the cooling ducts must not be lower than 4 3cm 1 7 water gauge at 1 3 times the stall speed The cooling ducts provided are only a starting point in establishing effective engine cooling The ducts may require to be increased in size and additional baffles provided to achieve the specified maximum cylinder head temperature of 180 C see page 19 14 2 Oil Cooling The dipstick cap must be screwed fully in before removal for reading oil level An oil cooler adapter is supplied with the engine and is fitted under the oil filter Oil coolers are available from Jabiru Aircraft Unless operating in environments of low temperatures oil coolers are mandatory The cooler can be plumbed either way to the adaptor flow direction through the cooler is not important In continuous operation oil temperatures between 80 C and 90 C 176 F 194 F are desirable 70 158 is the minimum allowable temperature for continuous running 100 C 212 is the maximum allowable temperature for continuous
5. 7 washer amp Heat Proof nut 2 LI ZE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty me Installation Manual Jabiru 2200 Aircraft Engine d To place the nuts on the mount bolts the rubbers must be compressed Do this by using a deep reach socket inside the engine mount pins amp clamping the rubber mount assembly using a G clamp with the swivel taken off the ball See Photo Start nuts on both upper mount bolts Once bolts of the upper rubbers are started continue lowering the front of the engine amp align the lower engine mount pins with the engine backing plate f Use the weight of the engine to compress the lower rubbers amp fit the nuts to the bolts Male engine Engine Female engine mount rubber backing plate mount rubber Engine mount Washer Figure 15 Upper Engine Mount Detail Heat proof nut 5 Pr g The lower engine mount rubbers are assembled in the same way except the male engine mount rubber is fitted to the engine mount pins first Refer to drawing below h Tighten nuts until firm Engine mount washer will touch the engine mount pin as the rubbers compress ToT LL ZE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation
6. 2400rpm e Maximum moment of inertia 0 25 kgm2 Applications outside this range should be referred to Jabiru Engine MUST NEVER BE RUN WITHOUT THE PROPELLER Damage will occur in this state ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 16 Auxiliary Units 16 1 Vacuum Pump For the installation of an artificial horizon and or a direction gyro a vacuum pump is necessary A Tempest 212CW or equivalent vacuum pump can be fitted to the alternator mounting plate and directly coupled to the crankshaft The drive pad is dry The pad and spline are SAE Standard T oarsmen ae TE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 109 SOc OO OOO OQ OC OC 11109 8 7 5 21 OFF ON OFF F r _ 7j FUEL MAIN N U
7. Bottle Fit the oil over flow bottle to the firewall by drilling and Riveting oil bottle holder in place using 73AS 6 6 rivets Refer to photo m Connect the oil breather line from the engine breather n Ensure that the oil overflow line is in place and vents overboard Fit Scat hoses from NACA duct to Air Inlet Housing Assembly from hot air muff to carburettor heat inlet on the hot air mixer box and from the hot air mixer box to carburetor Note It is most important to remove any sharp edges or lips off the inside of the mixer box cover See Photos below e 6 ZE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pry eta 9m Installation Manual Jabiru 2200 Aircraft Engine Incorrect plumbing Note sharp lips Figure 21 Hot Air Plumbing Incorrect Correct plumbing sharp lips amp abrupt corners rounded amp smoothed off Figure 22 Hot Air Plumbing Correct e 6 E Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty ee Installation Manual Jabiru 2200 Aircraft Engine SCAT hose from NACA inlet to mixer box SCAT hose from hot air muff on
8. Jabiru 2200 Aircraft Engine 1 4 Table of Figures Figure 1 Drawing 9404041 1 Engine Dimensions eese rennen ener en neret tnnt tenen ens 9 2 Cylinder Firing iR EOD IER P UD ERR HER HEU m EDU IEEE 10 Figure 3 Engine Mount Point Locations rr enne enne rre 12 Figure 4 Engine Mount sean itn etes ennt tenete 13 Figure 5 Wiring Dia gt ain sc ioter dei e eene 18 Figure 6 Regulator Plug erret tere e rec ere eia 20 Fig re 7 Wiring Details u u mPP 28 5 Intake Detail A l rsrsrsrs 35 Figure 9 Intake Detail 2 EA 35 Figure 10 Engine Installation 11 iere Hee eas Fede eat ee 36 Fig re 11 Coil Cooling a Re a ERR GR eee ete ve 36 Figure 12 Cooling Detal 2 u qasqa 37 Figure 13 Engine Accessory Pack Contents 37 Figure 14 Upper Engine Mount Detatll 38 Figure 16 Lower Engine Mount Detail 0 ee eceeceseeesseceeese
9. Lubricant complying with MIL L 22851C or Lycoming Spec 301F or Teledyne Continental Spec MHF 24B 2 3 L 2 2 quarts D9EA Automotive Static sea level ratings under the following conditions International Standard Atmospheric conditions at sea level Aircraft service equipment drives unloaded Vacuum Pump not fitted 3 2 Full rich fuel air mixture Maximum cylinder head temperature Standard Jabiru air filter and cold air Standard exhaust muffler 1 Engine Ratings Takeoff Max Continuous Fuel Consumption Oil Consumption REVISION 85 hp 3300 RPM 21 L hr Takeoff Max Continuous Rating 0 1 L hr max Dated March 2006 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 4 Operating Limitations 41 RPM Continuous 3300 RPM Full Throttle Recommended Cruise 2750 RPM 3100 RPM 4 2 Engine Cooling Maximum Cylinder Head Temperatures measured under exhaust spark plug Maximum Peak Temperature 200 C 392 F Continuous Operation 180 C 356 F 43 Fuel 4 3 1 Specifications Avgas 10011 amp Avgas 100 130 Leaded and Unleaded Automotive Gasoline above 95 Octane RON 4 44 Pressure to Carburettor above ambient e Maximum 20 kPa 3 p
10. System 111 Fuel Tank The fuel tank must be fitted with an outlet strainer of between 8 and 16 mesh per inch with a minimum total mesh area of 5 cm 11 2 Fuel Filtration A Fuel filter capable of preventing the passage of particles larger than 0 1mm 100um must be installed between the fuel tank outlet and the fuel pump The filter must be present in the system for the fuel flow test The size of the filter should give consideration to allow adequate flow with a used filter A Ryco 215 or similar filter has been used successfully 11 3 Mechanical Fuel Pump The mechanical fuel pump is mounted on the engine crankcase and is camshaft driven It is designed to supply fuel at the pressure described in the following paragraph f fitted the electrical boost pump must also fulfill the fuel input criteria for the carburettor given below 11 4 Carburettor A Bing constant depression type 94 40 is used This carburettor has a minimum delivery pressure of 5 kPa 0 75 Psi and a maximum pressure of 20 kPa 3 psi To confirm that the fuel system is capable of delivering this pressure a fuel flow test must be performed To check pressure insert piece between the mechanical pump and the carby Test boost pump with engine off then mechanical fuel pump with engine on then combine with electrical boost pump as well before first flight A method for performing a fuel flow test is available from Jabiru if required A drip deflect
11. Valve Lifters with Automatic Adjustment Ram Air Cooled Wet Sump Lubrication Direct Propeller Drive Dual Transistorised Magneto Ignition Integrated AC Generator Electric Starter Mechanical Fuel Pump Naturally Aspirated 1 Pressure Compensating Carburettor 6 Bearing Crankshaft 2 3 Manufacturer Jabiru Aircraft Pty Ltd P O Box 5186 Bundaberg West Queensland 4670 2 4 Manuals Instruction and Maintenance Manual Installation Manual Parts Catalogue e 6 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty S Installation Manual Jabiru 2200 Aircraft Engine 3 3 1 3 2 Specifications General Displacement Bore Stroke Compression Ratio Direction of Rotation of Prop Shaft Ramp Weight Ignition Timing Firing Order DC Output Fuel Consumption 75 Power Fuel Oil Oil Capacity Spark Plugs Performance 2200 cc 97 5 mm 74 mm 8 1 Clockwise Pilot s view Applications 61 kg 134 Ibs Complete including Exhaust Carburettor Starter Motor Alternator amp Ignition System 25 BTDC 1 3 2 4 10 Amps 13 I hr 3 5 US gal hr AVGAS 100 130 MOGAS with RON Octane Rating 95 or above may be used if AVGAS is not available Aero Oil W Multigrade 15W 50 or equivalent
12. exhaust to mixer box Figure 23 SCAT Hose Detail 1 REVISION Dated March 2006 Page 44 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copiesHL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N Installation Manual Jabiru 2200 Aircraft Engine 7 ege E Y 5 t lt E 8 E 2 5 5 a 58 w 2 8 ES ja 2 8 9 5 gt g E 8 3 5 z 3 z Ex B 2 3 5 2 8 5 8 6 9 X esr l REVISION 01112 Dated March 2006 Page 45 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty me Cr Installation Manual Jabiru 2200 Aircraft Engine Figure 24 Typical Hot Air Mixer Box Kit Throttle Cable A TT Dek Lethe BEER ter ee Throttle lever end Jabiru Aircraft Throttle cable connected Figure 25 Control Connections to Ca
13. running Over filling with oil is not desirable Over filling may result in elevated temperatures and excessive oil loss through the crankcase vent When installed in a tail dragger aircraft recalibration of the dipstick will be required by the owner Hoses should be nominally 10mm 3 8 bore Hoses must be changed every two years or when visible degradation cracking hardening is visible during inspections The limits in the Specification Sheet contained in Appendix B must be strictly adhered to Warranty will not be paid on engine damage attributed to overheating of cylinders or oil ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 15 Propeller Selection e The hub of the propeller must be drilled with holes to match the flange e The propeller must be carefully selected to match the airframe and the engine Propellers up to 1727mm 68 in diameter and between 762mm 30 and 1219mm 48 in pitch may be used The propeller flange is drilled with 6 holes at both 4 PCD and 100mm PCD total of 12 holes e All Propellers must be able to obtain 2800rpm static and 3150rpm to 3300rpm wide open throttle straight and level Do not cruise or climb in the range 2100rpm
14. 2 Coil Cooling Detail 1 gt 4 3 V N E meme epo waren TE WGatewayNibraryMilesvengine manuals2200 engine manuals LiftersWorking Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty Me Installation Manual Jabiru 2200 Aircraft Engine Figure 13 Coil Cooling Detail 2 21 1 Engine Installation Procedure Male rubber engine mount Female rubber engine mount Washer engine mount spacer Air duct Spring Lock wire to attach ram air cooling ducts Belleville washer 21 1 1 Procedure Propeller guide bush Spring m bracket a o MM spring EM mount ce Figure 14 Engine Accessory Pack Contents a Attach male engine mount rubbers to all engine mount pins on the engine mount Place an AN4 31A bolt through each mount see details below Note that an engine mount spacer washer is fitted between the male rubber amp the lower engine mount pins Refer to Figure below b With the Back of the Aircraft Supported 4 the wheels chocked lift the engine onto the engine mount C Insert the upper engine mount rubbers into the engine backing plate first by tilting the front of the engine up Once both upper rubbers are through the engine backing plate fit the female rubber engine mount spacer washer engine mount washer
15. 8 Figure 33 Tachometer Sensor Installation eeseeesseeeseseeee eene enne nen etre enne 49 meo Te ST T TT T WGatewayMibraryMilesvengine manuals 2200 engine manualsWHydraulic LiftersWorking copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty eta _ Installation Manual Jabiru 2200 Aircraft Engine 1 2 List of Effective Pages The dates of issue for original amp revised pages are Page Revision Date Page Revision Date 1 0 29 6 05 21 0 29 6 05 2 0 29 6 05 22 0 29 6 05 3 0 29 6 05 23 0 29 6 05 4 0 29 6 05 24 0 29 6 05 5 0 29 6 05 25 0 29 6 05 6 0 29 6 05 26 0 29 6 05 7 0 29 6 05 8 0 29 6 05 9 0 29 6 05 10 0 29 6 05 11 0 29 6 05 12 0 29 6 05 13 0 29 6 05 14 0 29 6 05 15 0 29 6 05 16 0 29 6 05 17 0 29 6 05 18 0 29 6 05 19 0 29 6 05 20 0 29 6 05 Issue Notes REVISION Dated March 2006 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N Installation Manual Jabiru 2200 Aircraft Engine 2 Description 21 Model All Jabiru 2200 Engine Models from S No 2068 on 2 2 Details 4 Stroke 4 Cylinder Horizontally Opposed 1 Central Camshaft Push Rods Over Head Valves OHV Hydraulic
16. Cooling Cowls should have adequate entry and exit areas As a general guide cowl outlets should have approximately 3 times as much area as the inlets Care must be taken not to flood the cowl area with oil cooler air excessive oil cooler duct size Too much air coming in through the oil cooler will reduce the amount of air flowing through the ram air ducts amp increase CHTs Air ducts as supplied are starting points and for best performance must be optimized by the builder Poor connections and air gaps around ducts cooler etc give second rate cooling Damage caused by overheating due to poor installation techniques would not be covered under warranty 19 4 Air Induction Air must enter from outside the cowl All scat hoses should have only slight bends with all sharp edges removed from the induction path including hot air sources Ensure the filter used has adequate size 19 5 Carburettor The bowl vent line must be connected to the filtered side of air box Ensure that the two sense holes on the rear of venturi intake side of carburettor have not been obscured Set engine idle when warm Ensure throttle and choke movement is correct ZE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt 22 gt Installation Manual Jabiru 2200 Airc
17. INSTALLATION MANUAL FOR JABIRU 2200 AIRCRAFT ENGINE 2 Oe d eL Sf a 4 7 7 7 A ty N J e This Manual has been prepared as guide to correctly install the Jabiru 2200 engine into an airframe Should you have any questions or doubts about the contents of this manual please contact Jabiru Aircraft Pty Ltd Applicable to Jabiru 2200cc Enginers S No 2068 Onwards Hydraulic Lifter Type Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 1 TABLE OF CONTENTS 1 TABLE OF CONTENTS 2 2 Description 5 3 Specifications 6 4 Operating Limitations 7 5 Dimensions 9 6 Denomination Of Cylinders 10 7 Engine Mount 12 8 Controls 14 9 Instruments 15 10 Electrical Equipment 18 11 Fuel Supply System 21 12 Air Intake System 23 13 Exhaust System 24 14 Cooling Systems 25 15 Propeller Selection 26 16 Auxiliary Units 27 17 Appendix Wiring Diagrams 28 18 Appendix B Supplemantay Information 29 19 Appendix C Jabiru Engine Installation Tips 30 20 Appendix D 33 21 Typical Installation Jabiru Engine 35 meo Te ST T TT T WGatewayMibraryMilesvengine manuals 2200 engine manualsWHydraulic LiftersWorking copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual
18. OUI Figure 4 Engine Mount Point Locations The correct installation is shown below in Figure 4 0 ToT LT a Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine PIN ENGINE MOUN BREAK A 88 l SHARP CORNERS N e 60 41 5 DETAIL REAR ENGINE MOUNT PLATE Nowa RIN SINIC AIIN m ENGINE MOUN V ENGINE MOUNT W ASSY 12 E 0 PSJED 07 MOUNT BUSH FIR WASHER ENGINE MOUNT 9467073 1 Figure 5 Engine Mount Assembly Corrections of the engine alignment may be made using spacers under the rubber cushions The maximum spacer thickness on any one mount is 3mm T TT T eae Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty S Installation Manual Jabiru 2200 Aircraft Engine 8 Controls This section comprises of the mechanical controls and electrical switches 8 1 Throttle and Choke Provisions for the connection of the throttle and choke are made on the carburettor Note Sin
19. ST OR INTAKE SIDE OF THE HEAD EXHAUST INTAKE EXHAUS INTAKE 4 1 6 CYLINDER ENGINE 2 2CYLINDERENGINE 2 FIRING ORDER 1 4 5 2 3 6 FIRING ORDER 1 2 gt 4 CYLINDER ENGINE FIRING ORDER 1 3 4 2 8 CYLINDER ENGINE FIRING ORDER 1 5 8 3 2 6 7 4 E DIMENSIONS THIS DRAWING IS COPYRIGHT AND MUST NOT BE poe 29 9 05 PO SCALE COPIFD WITHOUT THE CONSENT OF LTD NTS 565 DATE UMTS DS d DWG No N A JABIRU ENGINE DISTRIBUTOR CYLINDER 4A266A0D 1 MATERIAL MAP ALL ENGINES SHEET 1 or A4 Figure 3 Distributor Cylinder Map Te ST T TT T eae a Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copiesHL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 7 Engine Mount The design of the engine mount must not only take into account the structural loadings but must make allowances for accessibility of components and the removal of equipment located at the rear of the engine The engine has four engine mounting points located at the rear of the engine refer to figure 1 0 from which the engine is to be mounted An optional bed mount may be fitted POINTS 7 ENGINE MOUN 7 ENGINE M
20. T UL PUMP FUSE CN IGN 2 STARTER MASTER GN GN 2 STARTER MASTER Gh GN 2 STARTER MASTER D REGULATOR ER MAIN BUS 654321 C33 Cy ry ry rs TED 5 1110 7 pooooooQoc Figure 8 Wiring Details meo Te ST T TT T Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 18 Appendix Supplemantay Information 18 1 Recommended Propeller e Fixed pitch wooden propellers Maximum propeller diameter 1727mm 68 18 2 Equipment The following equipment is included in the engine approval Carburettor 1 x Bing constant Pressure carburettor type 94 40 Main jet is Bing 220 Needle jet 276 Idle jet 45 e Fuel Pump Mechanical Jabiru P N PG10332N e Ignition System Jabiru dual magneto high voltage transistorised contactless P N 10522 e Spark Plugs NGK D9EA e Alternator Integrated Jabiru permanent magnet single phase alternator P N 4532064 4535064 with regulator rectifier P No 10652 e Starter Jabiru 12V 1 5 kW engagement via reducti
21. _Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty me 2 Installation Manual Jabiru 2200 Aircraft Engine G Clamp with swivel removed Deep long reach socket 1 BOLT MOUNT CUSHION MALE 3 MOUNT CUSHION FEMALE 4 ENGINE MOUNT WASHER ENT REAR ENGINE MOUNT PLATE ft ENGINE MOUNT PIN W ENGINE MOUNT W ASSY 26 2 26 REF REI A Figure 16 Lower Engine Mount Detail gt LT L L sea Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty eta Ine 2200 Aircraft Engi Iru Jab 01 72259 OL 514 wisi SUAN W3L 1108 Installation Manual laver NI SNOLLVTIVISNI 3NI9N3 00 0022 NUlgvr NOILVYUNSIANOD LNNOW X 8 WN LL 30090 14 NI SNOILVTIV LSNI ANIDNA 0088 0022 a18voriddv NOILVYUNSIANOD LNNOW IH 8 WN LL 30080 ASSY M LINNON 3NION3 3 NI SNOISNAWIG
22. ack Oil Pressure Gauge Negative to Earth Red Oil Pressure Gauge Positive to Instrument White Oil Pressure Gauge Sensor S to Oil Pressure Sensor Fwd Top Eng 9 1 4 Cylinder Head Temperature Gauge The Cylinder Head Temperature Gauge uses a thermocouple An audit must be done to establish the hottest cylinder and the thermocouple probe should be fitted under the exhaust TT LI Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty 7 gt Installation Manual Jabiru 2200 Aircraft Engine spark plug on that cylinder Note that number 4 head runs hottest in normal tractor installations Jabiru Part No PI10732N is the recommended gauge 9 1 4 1 Cylinder Head Temperature Wiring Loom and sensor is supplied with the instrument These must be installed as per directions If cable is too long it must be looped as many times as necessary and strapped behind the instrument panel DO NOT CUT TO LENGTH Ensure that wire is not chaffing on the fibreglass air duct or cooing fins No power connection is required 9 1 4 2 CHT Sender Temperature of the cold junction for best results should be around 50 C Ensure cold junction is furthest from the thermo couple probe as possible 9 1 5 Exhaust Gas Temperature Gauge An optional Exhaust Gas Temperature Gauge can be fitt
23. ative Earth 10 2 Regulator The regulator has been selected to match the voltage and current of the integral alternator Only Jabiru Part No 10652 should be used The regulator output voltage is 14 volts 0 8 volt Recommended wiring of regulator is positive and negative of the regulator directly to the battery A 20A fuse or circuit breaker may be used between the regulator amp battery 10 3 Ignition The ignition unit has dual breakerless transistorised ignition with the magnets mounted on the flywheel and the coils mounted on the alternator mount plate The current from the coils flows to the distributor from where it is distributed to the spark plugs See also Regulator Wiring at Page 12 e The ignition is turned off by grounding the coils via the ignition switches The ignition is timed to 25 BTDC e The temperature limit for the ignition coils is 70 C This should be checked by the installer It is recommended that pipes of 12mm dia be fitted to the top rear of each air duct directing air onto the coils for cooling purposes e Coil gaps are set at 0 25mm to 0 30mm 0 010 to 0 012 10 3 1 Transistorised Ignition 1 Wiring No 1 Switch Upper to Left Transistorised Ignition No 1 Switch Lower to Earth Switch Open for Ignition ON closed for Ignition OFF oT 2 T T T paene Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Man
24. be or Jabiru produced adaptor Air vent for the carburettor bowl must be routed to the filtered side of the air box e Engines must be fitted with an oil cooler e Engines work best at RPM quoted Extended operation of the engine at other speeds may result in reduced performance or engine damage Engines fitted with coarser or finer pitched props will cause variation from figures quoted and could cause excessive fuel consumption and higher than normal CHT s e Engines are jetted to a standard and must not be changed without discussion with Jabiru Aircraft or local representative All figures given at sea level and at summer temp of around 25 20 3 Normal Operation Data Idle Hot 900 950 RPM Take Off Power 2800 RPM 60 x 44 Propeller 2900 RPM 60 x 42 Propeller Full Power S amp L 3200 RPM 60 x 44 Propeller 3300 RPM 60 x 42 Propeller Cruise At 75 Power 2750 2850 RPM Oil Pressure 226 525 kPa 32 psi 76 psi Oil Temperature 70 C 100 C 158 F 212 F normal operation 118 C 244 F Max Cruise CHT 180 C 356 F Max Climb CHT 200 C 392 F EGT 650 C 750 C 1202 F 1382 F Mechanical Fuel Pump Pressure 3 Ibs 20 kPa eo ont warn zo ZE WGatewayMibraryMilesvengine Dem engine manualsWydraulic LiftersWorking copiesWHL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 P Jabiru Aircraft pty eta GG N
25. ce a pressure compensating carburettor is used there is no mixture control 8 2 Master Switch Ignition Switches and Starter Button The switches are connected as shown by the circuit diagram on Page 10 REVISION Dated March 2006 Page 14 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 9 Instruments 9 1 Electronic Tachometer The tachometer picks up on 2 metal tabs attached to the inside of the flywheel Pickup is of induction sender type 9 1 1 Tachometer Wiring Tachometer Negative 3 to Earth Tachometer Positive 4 to Instrument Tachometer to Red Wire tachometer pick up Tachometer to Black Wire tachometer pick up 9 1 2 Oil Temperature Gauge The Oil Temperature Gauge uses an electric probe mounted in the base of the sump Jabiru Part No 10752 is recommended 9 1 2 1 Oil Temperature Wiring Black Oil Temperature Gauge Negative to Earth Red Oil Temperature Gauge Positive to Instrument White Oil Temperature Gauge Sensor S to Oil Temperature Sensor Lower Left Eng Sump 9 1 3 Oil Pressure Gauge An electric oil pressure sender is fitted to the engine for an Oil Pressure Gauge Jabiru Part PI10762N is the recommended gauge 9 1 3 1 Oil Pressure Wiring Bl
26. cseveecneeeeceaeceeesecaeeseceevsecsaeeeesaecaeseecseeaeesaeensaesateneeaeeetents 39 Figure 17 Engine Mount Detail 41 Figure T9 Fuel Connections General Ren 41 Figure 18 Fuel Connection i Rue Ie e ER HERI EO HEC 41 Eiv re20 Oil Collector Bottles 42 Figure 21 Hot Air Plumbing Incorrect 43 Figure 22 Hot Air Plumbing Correct dayiuqawqaysaytakayaayaapaytaqhayawasaspawaayashayashaphayaaahapayssqa 43 Figure 24 SCAT Hose e e re 44 Figure 23 Typical Hot Air Mixer Box 46 Figure 26 Control Connections to Carburettor 46 Figure 27 Balance Tube Detail 11 47 Figure 29 Carburettor Balance Tube Nipple eee tette teet dte rite 47 Figure Oil FemperatireS6HsOf sc ceret ertet P RE n Eie ieri aide eae 48 Figure 32 Oil Pressure SENSON x Lettere UE Pe Hr ee te euet Dedi eo re ies tot uqaqa qasa 4
27. ct as possible no tight bends and air taken from outside the cowl Current air filter is RAF 17 Repco ToT LT TE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt 22 gt Installation Manual Jabiru 2200 Aircraft Engine 13 Exhaust System An exhaust system is provided with the engine Both Pusher and Tractor systems are available Muffler Volume Capacity 3 litres Back pressure at Takeoff Performance Max 0 2 bar 2 9 psi Readings taken 70mm from muffler flange connections Only complete mufflers supplied with Jabiru Aircraft are welded all others require tail pipes to be welded to the muffler body NOTE Drilled ends of pipes go inside muffler cavity The tail pipes go completely through the muffler body and are welded on both top and bottom When fitting the muffler one or more of the exhaust pipes can be loosened at the connection to the cylinder head to allow easy fit of the muffler They then must be tightened Exhaust Gas Temperature EGT Nominal 650 750 1202 F 1382 F measured 100mm from the exhaust manifold flange ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM
28. de suggested figures Appendix C Carburettor tuning must not be altered other than with advice from Jabiru Aircraft If in doubt contact Jabiru Aircraft or our local representative 11 5 Fuel Lines Fuel lines are nominally 6mm bore All hoses forward of the firewall require fire resistant sheathing and those between moving sections such as between engine and firewall should be flexible Hoses must be changed every two years though if there are visible signs of degradation such as cracking or hardening the hose should be changed immediately ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty Me gt Installation Manual Jabiru 2200 Aircraft Engine 12 Air Intake System 12 1 SCAT HOSE Remove at each 50 hourly inspection one end of each scat hose Inspect for holes leaks and condition of helical wound in a wire former Replace if any signs of corrosion is evident 12 2 Air Filter e The induction system must not cause positive RAM induction pressure as this will have an unpredictable affect the fuel air mixture supplied to the engine e The filter must be capable of supplying 250 kg hr 550 pph of air e The filter may have to be changed at regular intervals if the engine is to be used in a dusty environment Air flow should be as dire
29. ed The probe should be positioned 100mm from the port flange on the exhaust pipe of a convenient cylinder Jabiru Part No PI0325N is the recommended gauge LT pre Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine ER NDI SE TACHO gt ARTMEN OM NGINE SE 10 FUS RING REVISION Dated March 2006 Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine Figure 6 Wiring Diagram 10 Electrical Equipment 10 1 Alternator The alternator fitted to the Jabiru 2200 engine is a single phase permanently excited with a regulator The rotor is mounted on the flywheel with the stator mounted on the alternator mount plate at the back of the engine The alternator mount plate is also the mount for the ignition coils and the vacuum pump Specifications Power Max 120W Continuous Note The electrical system is Neg
30. h Negative to Earth Bus 10 6 3 Master Wiring Red Starter Solenoid to Main Fuse 6 2 T L T T osea Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt Installation Manual Jabiru 2200 Aircraft Engine Red Main Fuse to Master Switch Lower Red Master Switch Upper to Main Bus Red Main Bus to Red on Regulator 10 6 4 Fuel Pump Wiring Red Main Bus to Fuel Pump Fuse Red Fuel Pump Fuse to Fuel Pump Switch Lower Red Fuel Pump Switch Upper to fuel Pump Red Wire Black Fuel Pump Black Wire to Earth Bus 10 6 5 Regulator Pale Blue No Coding Pale Blue Wire Regulator plug to one Alternator Wire Pale Blue No Coding Pale Blue Wire Regulator plug to the other Alt Wire Black Black Wire Regulator Plug to Earth Red 10 g Positive to Red Wire Reg Plug Yellow 16g Positive to Yellow Wire Reg Plug Green Not connected can power a charging light Regulator Plug Pale Blue Black Pale Blue Green Yellow Red Figure 7 Regulator Plug ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty eta GG N gt Installation Manual Jabiru 2200 Aircraft Engine 11 Fuel Supply
31. ich is supplied as a complete kit The probe is mounted in a fitting which is welded to an T DET Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty Me 2 Installation Manual Jabiru 2200 Aircraft Engine exhaust pipe Note that this fitting is not standard The installation of the fitting is best done at the time of order though if required the exhaust pipe may be returned to Jabiru and the fitting added Note that in this case it will normally take around 2 weeks before the pipe is returned to you The fitting is welded to the pipe 100mm down from the exhaust manifold mounting plate w The Tachometer sensor used is a 6 35 x 22 mm analogue magnetic pick up and is fitted to a bracket on the alternator housing Refer to photo below The sensor picks up on 2 tags fitted behind the flywheel C 5 N in E gt 3 4 4 LS lt Figure 30 Sensor Installation LL TET Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copiesHL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 PM
32. ng SCAT hose to the carburettor intake system that some form of fiberglass tube or specially manufactured Cobra Head made by Jabiru Aircraft be used This will prevent air turbulence in front of the 2 sense holes on the intake of the carby Turbulence next to these sense holes can cause the engine to run out of tune or roughly at certain revs e 6 TE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt 22 gt Installation Manual Jabiru 2200 Aircraft Engine 20 Appendix D Normal Engine Figures The following information is intended to allow an assessment of the engine s performance when installed in a known airframe with a known propeller 20 1 Known Airframe Engine Details e Jabiru SP 2 Seater e Propeller 60 x 42 1525mm x 1067mm or e 60 x 44 1525mm x 1118mm 20 2 Reference Information e Figures given are approximate guide only e Engines installed in other aircraft with different prop loads elevation and fuel types will differ from the Jabiru airframe e Poor installations will result in poor performance air inlet junctions from outside the cowl to the carburettor inlet must be free of edges ledges and tight bends e Carburettor inlet must have protection to the scat hose attachment short glass tu
33. nsor used in Jabiru aircraft is a J type thermocouple located under the rear spark plug of No 4 cylinder The VDO 310 980 Cylinder Head Temperature Gauge Kit is compatible with this sensor and is installed as standard equipment in Jabiru Aircraft Note that to ensure an accurate temperature reading it is important to have the cold junction for the CHT the plug between the stiff thermocouple wires and the normal plastic insulated gauge wires located away from the heat of the engine Refer to Figure at the beginning of the engine installation section above DIT T TT TE Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copiesHL Installation Manual 2200 Rev 0 Print Date 3 8 2006 1 56 00 PM 2 sr __ Installation Manual Jabiru 2200 Aircraft Engine Jabiru Aircraft pty pt Oil temperature sensor Figure 28 Oil Temperature Sensor t The Oil Temperature Sensor used is a VDO 320 028 which is located in the bottom of the sump as shown in photo Wire WK is normally not used but can be used to power a low oil pressure warning light Oil pressure sender Connect wire G to gauge Figure 29 Oil Pressure Sensor u The oil pressure sensor is located at the base of the oil filter and this can be seen in photo The sensor used is VDO 360 001 v The exhaust gas probe used on Jabiru engines is a VDO 310 306 Pyrometer wh
34. on gear and flywheel Nippon Denso type P No 4933023 The following optional equipment may be driven by or fitted to the engine subject to the type number being included in the approved Jabiru Aircraft Pty Ltd engine specification Vacuum Pump Tempest 212CW or equivalent vacuum pump fitted to the alternator mounting plate and directly coupled to the crankshaft The drive pad is dry amp The pad and spline are SAE Standard ToT LT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt Installation Manual Jabiru 2200 Aircraft Engine 19 Appendix C Jabiru Engine Installation Tips 19 1 Prop For optimal performance Jabiru engines require 2800 2900 RPM at take off and 3200 in the air straight and level This may vary with aircraft and prop type but variation beyond these limits will affect tuning and in extreme cases may result in damage to the engine Carby tuning must not be altered other than with advice from Jabiru Aircraft If in doubt contact Jabiru Aircraft or our local representative 19 2 Ensure gauge is reading correctly While large errors will be obvious smaller errors are harder to pick and it is recommended to check the gauge reading with another instrument such as a hand held optical prop tach 19 3
35. or to deflect overflowing fuel from the exhaust system is supplied as standard equipment on the engine Because idle adjustments cannot accurately be made on the dynamometer where every engine is run before delivery some adjustment of the 7mm idle set screw may be required A hot idle of around 900RPM is desirable Fitting an earth strap from carby to crankcase is recommended to eliminate possible radio interference 11 4 1 Carburettor Tuning Late in 2004 Jabiru Aircraft introduced a new system of needles and jets to the 2200 engine The new configuration lowers fuel consumption and is now standard Details of the configuration are given below TT Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt gt Installation Manual Jabiru 2200 Aircraft Engine Idle Jet Bing Jet size 45 Idle Air Bleed Size increased to 1 6mm diameter Idle Mixture Screw Typically Out 1 Turn Needle Jet Bing Jet size 276 Main Jet Bing Jet size 220 Needle Jabiru Needle P No 4A138A0D Note that the needle used is a proprietary item developed by Jabiru specifically for use on the 2200 engine From S N 2161 main jet 225 needle jet 280 Engine tuning may be significantly affected by extreme ranges of climate or propellers which incur RPM values outsi
36. raft Engine 19 6 Fuel Pump Ensure boost pump is not capable of more than 3 Ib 20 kPa pressure 19 7 Oil Expel inhibiting oil from cylinders and pressure up wind engine on starter until a the oil pressure gauge shows a reading before first start e Ensure correct run in type oil is used for the first 25 30 hours to ensure proper ring bedding in e Once past the initial 25 30 hours ensure the oil used meets the specifications given above e Oil coolers are mandatory unless operating in very cold ambient temperatures Refer to Oil Cooling section above for allowable oil operating temperature ranges Do not overfill the engine this may result in high oil temperatures 19 8 Fuel e Avgas 100LL e MOGAS above 95 Octane RON e Ensure a suitable fuel filter is used e Ensure the fuel tank is properly vented 19 9 Oil Overflow Use a small collector bottle to catch engine oil venting 19 10 Heads Valves See section on early operation e Check Head bolt tensions at regular intervals 19 11 Additives No Oil or fuel additives should be used Use of oil or fuel additives will void warranty 19 12 Temperature e Refer to correct temperature operation of the engine 19 13 Connections terminal oil pressure sender is connected to gauge W terminal on oil pressure sender can be connected to a warning light Regulator should be connected as per instructions above Oil
37. rburettor p Fit throttle cable to carburetor Note that Jabiru Aircraft kits come with a throttle cable cut to length and with the correct end fitting attached Engines used in firewall forward kits will be supplied with a length of throttle cable with no end the builder must cut the cable to length and fit the carburettor end fitting 5 16 washers are used on the cable end fitting one washer either side of cable end fitting to align cable Use R clip to assemble q Fit choke cable to carburettor Use an R clip to assemble Note that the fuel line from the fuel pump to the carburettor passes between the choke and throttle cables Choke cable not shown on Figure above ToT LT DE WGatewayNibraryMilesvengine manuals2200 engine manuals LiftersWorking Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty mm Installation Manual Jabiru 2200 Aircraft Engine Balance tube connecting filtered side of air mixer box to nipple on carburettor Figure 26 Balance Tube Detail 1 r Connect the fuel balance tube from the nipple on the carburettor to a fitting on the filtered air side of the air mixer box Note The balance tube must be connected to ensure proper mixture control Balance tube nipple Figure 27 Carburettor Balance Tube Nipple s Fit cylinder head temperature CHT sensor The CHT se
38. si e Minimum 5 kPa 0 75 psi WARNING When using auto fuels ensure all components of the fuel delivery system are cooled to prevent fuel vaporization 45 Oil 4 5 1 Specifications Aero Oil W Multigrade 15W 50 or equivalent Lubricant complying with MIL L 22851C or Lycoming Spec 301F or Teledyne Continental Spec MHF 24B 4 5 2 Oil Temperature e Minimum for Take off Power 50 C 122 F e Maximum 118 C 244 F e Continuous 80 C 100 C 176 F 212 F EI T L at Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N Installation Manual Jabiru 2200 Aircraft Engine 4 5 3 Pressure e Normal Operations Min 220 kPa 32 psi Max 525 kPa 76 psi e Idle Min 80 kPa 12 psi e Starting amp Warm Up Max 525 kPa 76 psi Te ST T TT T eae a WGatewayMibraryMilesvengine manuals 2200 engine manualsWHydraulic LiftersWorking copies HL Installation Manual 2200 Rev 0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty gt 22 2 Installation Manual Jabiru 2200 Aircraft Engine 5 Dimensions 2200 JABIRU ENGINE
39. temp terminal connects to gauge per instructions included with gauge T TT 9a Gateway library files engine_manuals 2200_engine_manuals Hydraulic_Lifters Working copies HL_Installation_Manual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine CHT sensor ring under spark plug connects to gauge EGT optional connects to gauge Fuel hoses oil hoses as required Hoses must be protected by fire sleeve Throttle choke connected amp movement adjusted Carburettor heat arrangement working Correct scat hoses and directions Run hose from sump vent pipe to collection bottle 19 14 Contact e Check for contact of engine cooler or ducts on cowl Any contact will cause excessive vibration amp if the oil cooler is rubbing it will eventually fail amp leak 19 15 Warranty Damage caused by overheating due to poor installation techniques would not be covered under warranty Operation of the engine on non approved oils and fuel will likewise not be covered 19 16 Performance e Overall performance of engine and airframe depends on correct installation and prop match 19 17 Coils e When installing new ignition coils the output leads go in the directon of prop rotation RHS coil output lead is up LHS coil output lead goes down See 24 19 18 Induction t is strongly recommended that when connecti
40. ual_2200_Rev_0 doc Print Date 3 8 2006 1 56 00 PM Jabiru Aircraft pty GG N gt Installation Manual Jabiru 2200 Aircraft Engine 10 3 2 Transistorised Ignition 2 Wiring No 2 Switch Upper to Right Transistorised Ignition No 2 Switch Lower to Earth Switch Open for Ignition ON closed for Ignition OFF 10 4 Starter Motor The starter is mounted on the top of the engine and drives the ring gear on the flywheel The motor is activated by engaging the starter button the master switch has to be ON which trips the solenoid hence current flows from the battery to the motor The cable from Battery to starter should be minimum 16mm copper 10 4 1 Starter Wiring Starter Button Switch lower to Main Bus Starter Button Switch upper to Start Solenoid through Grommet 10 5 Battery The battery should be of a light weight 12V 20 Ah type able to accept a charging voltage up to 14 V 0 8V and a 10 Input 10 5 1 Battery Cables Black Starter Motor Mount Engine Rear to Battery Negative Red Battery Positive to Starter Solenoid Red Starter Solenoid Switched to Starter Motor Part of 10 6 Additional Wiring Information 10 6 1 Engine Hourmeter Wiring Red Hourmeter Positive to Positive Black Oil Pressure Switch to Engine Sump Bolt Black Hourmeter to Oil Pressure Switch Fwd Eng Left 10 6 2 Earth Wiring Black Battery Earth Negative to Firewall Earth Engine Bay Black Battery Eart
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