engine perkins 2200 series

KENR6907May 2008

Systems OperationTesting and Adjusting2206-E13 Industrial EngineTGB (Engine)TGD (Engine)TGF (Engine)

This document has been printed from SPI². Not for Resale

Important Safety InformationMost accidents that involve product operation, maintenance and repair are caused by failure toobserve basic safety rules or precautions. An accident can often be avoided by recognizing potentiallyhazardous situations before an accident occurs. A person must be alert to potential hazards. Thisperson should also have the necessary training, skills and tools to perform these functions properly.

Improper operation, lubrication, maintenance or repair of this product can be dangerous andcould result in injury or death.

Do not operate or perform any lubrication, maintenance or repair on this product, until you haveread and understood the operation, lubrication, maintenance and repair information.

Safety precautions and warnings are provided in this manual and on the product. If these hazardwarnings are not heeded, bodily injury or death could occur to you or to other persons.

The hazards are identified by the “Safety Alert Symbol” and followed by a “Signal Word” such as“DANGER”, “WARNING” or “CAUTION”. The Safety Alert “WARNING” label is shown below.

The meaning of this safety alert symbol is as follows:

Attention! Become Alert! Your Safety is Involved.

The message that appears under the warning explains the hazard and can be either written orpictorially presented.

Operations that may cause product damage are identified by “NOTICE” labels on the product and inthis publication.

Perkins cannot anticipate every possible circumstance that might involve a potential hazard. Thewarnings in this publication and on the product are, therefore, not all inclusive. If a tool, procedure,work method or operating technique that is not specifically recommended by Perkins is used,you must satisfy yourself that it is safe for you and for others. You should also ensure that theproduct will not be damaged or be made unsafe by the operation, lubrication, maintenance orrepair procedures that you choose.

The information, specifications, and illustrations in this publication are on the basis of information thatwas available at the time that the publication was written. The specifications, torques, pressures,measurements, adjustments, illustrations, and other items can change at any time. These changes canaffect the service that is given to the product. Obtain the complete and most current information beforeyou start any job. Perkins dealers or Perkins distributors have the most current information available.

When replacement parts are required for thisproduct Perkins recommends using Perkins replacement parts.Failure to heed this warning can lead to prema-ture failures, product damage, personal injury ordeath.


KENR6907 3Table of Contents

Table of Contents

Systems Operation Section

General Information ................................................ 4Electronic Control System Components ................. 6Fuel System ........................................................... 8Air Inlet and Exhaust System ............................... 12Lubrication System .............................................. 14Cooling System .................................................... 15Basic Engine ......................................................... 18Electrical System ................................................. 19

Testing and Adjusting Section

Testing and AdjustingBelt Tension Chart ................................................ 23

Fuel SystemFuel System - Inspect ........................................... 24Air in Fuel - Test .................................................... 24Electronic Unit Injector - Adjust ............................. 25Electronic Unit Injector - Test ................................ 26Finding Top Center Position for No. 1 Piston ........ 26Fuel Quality - Test ................................................. 27Fuel System - Prime ............................................. 28Fuel System Pressure - Test ................................. 29Gear Group (Front) - Time .................................... 30

Air Inlet and Exhaust SystemAir Inlet and Exhaust System - Inspect ................. 31Turbocharger - Inspect .......................................... 32Exhaust Temperature - Test .................................. 34Engine Crankcase Pressure (Blowby) - Test ........ 34Engine Valve Lash - Inspect/Adjust ...................... 35

Lubrication SystemEngine Oil Pressure - Test .................................... 37Excessive Bearing Wear - Inspect ........................ 39Excessive Engine Oil Consumption - Inspect ....... 39Increased Engine Oil Temperature - Inspect ........ 40

Cooling SystemCooling System - Check (Overheating) ................ 41Cooling System - Inspect ...................................... 42Cooling System - Test ........................................... 43Water Temperature Regulator - Test ..................... 45Water Pump - Test ................................................ 46

Basic EnginePiston Ring Groove - Inspect ................................ 47Connecting Rod Bearings - Inspect ...................... 47Main Bearings - Inspect ........................................ 47Cylinder Block - Inspect ........................................ 47Cylinder Liner Projection - Inspect ........................ 48Flywheel - Inspect ................................................. 50Flywheel Housing - Inspect ................................... 51Vibration Damper - Check .................................... 53

Electrical SystemBattery - Test ......................................................... 54

Charging System - Test ........................................ 54Electric Starting System - Test .............................. 54

Index Section

Index ..................................................................... 55


4 KENR6907Systems Operation Section

Systems Operation Sectioni02769236

General Information

The following model views show the 2206-13 Enginefeatures. Due to individual applications, your enginemay appear different from the illustrations.

g01405969Illustration 1Typical example

Left side engine view(1) Connection for the breather(2) Electronic control module (ECM)(3) Fuel priming pump

(4) Secondary fuel filter(5) Primary fuel filter(6) Fuel pump

(7) Crankshaft damper(8) Oil filler


KENR6907 5Systems Operation Section

g01405970Illustration 2Typical exampleRight side engine view

(9) Water temperature regulator housing(10) Alternator(11) Water pump

(12) Turbocharger(13) Oil filter(14) Oil drain plug

(15) Oil cooler(16) Exhaust manifold

Starting the EngineThe Electronic Control Module (ECM) willautomatically provide the correct amount of fuel thatis necessary to start the engine. If the engine failsto start in 30 seconds, the starter switch should bereleased. The starting motor should be allowed tocool for 30 seconds before being used again.

Cold Mode OperationThe ECM will set the cold start strategy when thecoolant temperature is below 20 °C (68 °F).

Cold mode operation will be deactivated when any ofthe following conditions have been met:

• Coolant temperature reaches 20 °C (68 °F).

• The engine has been running for twelve minutes.

Cold mode operation varies the fuel injection amountfor white smoke cleanup. Cold mode operation alsovaries the timing for white smoke cleanup. Theengine operating temperature is usually reachedbefore the walk-around inspection is completed.



i02769284

Electronic Control SystemComponents

g01402324Illustration 3(1) Engine coolant temperature sensor(2) Intake manifold pressure sensor(3) Intake manifold air temperature sensor

(4) Atmospheric pressure sensor(5) Secondary position sensor (Camshaft)(6) Engine oil pressure sensor

(7) Fuel temperature sensor(8) Primary position sensor (Crankshaft)(9) Electronic control module (ECM)

The electronic control system is integrally designedinto the engine’s fuel system and the engine’s airinlet and exhaust system in order to electronicallycontrol the fuel delivery and the injection timing. Theelectronic control system provides increased timingcontrol and fuel air ratio control in comparison toconventional mechanical engines. Injection timingis achieved by precise control of injector firing time,and engine rpm is controlled by adjusting the firingduration. The Electronic Control Module (ECM)energizes the solenoid in the unit injector in order tostart the injection of fuel. Also, the ECM de-energizesthe unit injector solenoids in order to stop injectionof fuel. Refer to Systems Operation, Testing andAdjusting, “Fuel System” for a complete explanationof the fuel injection process.

The engine uses the following types of electroniccomponents:

• Inputs

• Controls

• Outputs

An input component is one that sends an electricalsignal to the ECM. The signal that is sent varies inone of the following ways:

• Voltage

• Frequency



• Pulse width

The variation of the signal is in response to a changein some specific system of the equipment. TheECM sees the input sensor signal as informationabout the condition, environment, or operation of theequipment.

A electronic control module (ECM) receives theinput signals. Electronic circuits inside the controlcomponent evaluate the signals from the inputcomponents. These electronic circuits also supplyelectrical energy to the output components of thesystem. The electrical energy that is supplied tothe output components is based on predeterminedcombinations of input signal values.

An output component is one that is operated by acontrol module. The output component receiveselectrical energy from the control component. Theoutput component uses that electrical energy in oneof two ways. The output component can use thatelectrical energy in order to perform work. The outputcomponent can use that electrical energy in order toprovide information.



i02769330

Fuel System

g01282152Illustration 4

Fuel system schematic(1) Fuel return line(2) Electronic unit injectors(3) Fuel gallery(4) Fuel priming pump

(5) Fuel cooler(6) Fuel tank(7) Secondary fuel filter(8) Primary fuel filter

(9) Fuel transfer pump(10) Fuel temperature sensor

The fuel supply circuit is a conventional design forengines with electronic unit injection. A fuel tank (6)is used to store the fuel prior to use by the engine. Aprimary fuel filter/water separator (8) is placed intothe fuel supply circuit in order to remove large debrisfrom the fuel. This debris may have entered thefuel tank during fueling. The debris may have alsoentered the fuel tank through the vent for the fueltank. The primary filter element also separates waterfrom the fuel. The water is collected in the bowl at thebottom of the primary fuel filter/water separator.

Note: The inlet fuel temperature to the fuel transferpump must not exceed 79 °C (175 °F) when theengine has reached normal operating temperature.Fuel temperatures above 79 °C (175 °F) will reducethe life of the fuel transfer pump check valves. Thefuel efficiency and the engine power output arereduced when the fuel temperature increases from30 °C (86 °F) to 70 °C (158 °F).



Fuel from the tank (6) flows to the fuel filter base.The fuel filter base contains the primary fuel filterand the secondary fuel filter. The fuel flows throughcored passages in the fuel filter base. The fuelpriming pump (4) is mounted on the fuel filter base.The fuel priming pump is used in order to manuallypump the fuel into the fuel system after the system,or parts of the system have been drained. The fuelpriming pump is used in order to refill the fuel systemafter air has been introduced into the system. Formore information on priming the fuel system, referto Systems Operation, Testing and Adjusting, “FuelSystem - Prime”.

As the fuel flows through cored passages in the fuelfilter base, the fuel is directed into the primary fuelfilter (8). Fuel flows out of the fuel filter and returnsto the passages in the fuel filter base. Prior to exitingthe fuel filter base, the fuel temperature is sampledby the fuel temperature sensor (10). The signalsthat are generated by the sensors are used by theengine control in order to monitor the condition of theengine’s components.

The fuel flows from the fuel filter base to the fueltransfer pump (9). The fuel transfer pump (9) is a geartype pump with fixed clearances. The fuel transferpump (9) incorporates an internal relief valve thatprotects the fuel system from extreme pressure. Inthe case of extreme pressure, fuel is redirected backto the inlet of the fuel transfer pump (9). An outletcheck valve is used in order to prevent pressurizedfuel leakage back through the pump. The fuel transferpump (9) is located in the front of the engine. The fueltransfer pump (9) is driven by the front gear train.

The fuel flows from the fuel transfer pump (9) to thesecondary fuel filter (7). The fuel is filtered in orderto remove small abrasive particles that will causepremature wear to fuel system components. The fuelflows from the secondary fuel filter (7) to the fuel filterbase.

The fuel is then directed from the fuel filter basethrough the fuel return line (1) to fuel manifold (3) thatruns the length of the cylinder head. A continuousflow of fuel is supplied to the electronic unit injectors(2) in order to perform the following tasks:

• Supply fuel for injection

• Remove excessive heat from the injectors.

• Remove air that may accumulate in the fuelsystem.

The fuel exits the fuel gallery and returns to the fuelfilter base. A pressure regulating valve is located inthe fuel filter base. The pressure regulating valveregulates the pressure for the fuel system. A sufficientamount of back pressure is maintained in the systemin order to ensure a continuous availability of fuel tothe electronic unit injectors. The fuel flows from thefuel filter base to the fuel cooler (5). The fuel flowsfrom the fuel cooler (5) back to the tank (6).

Fuel System Electronic ControlCircuit

g00451841Illustration 5Electronic governor(1) Signals to the electronic unit injectors(2) Fuel injection control(3) Fuel position(4) Electronic governor(5) Desired rpm(6) Coolant temperature(7) TC for No. 1 cylinder(8) FRC fuel position(9) Rated fuel position(10) FCR maps(11) Torque maps(12) Engine speed/timing sensor(13) Engine speed/timing signals’ interpreter(14) Engine rpm(15) Coolant temperature sensor(16) Boost pressure sensor(17) Boost pressure

The injection pump, the fuel lines, and the nozzlesthat are used in the traditional Perkins diesel engineshave been replaced with an electronically controlled,mechanically actuated electronic unit injector in eachcylinder. A solenoid on each injector controls theamount of fuel that is delivered by the injector. AnElectronic Control Module (ECM) sends a signal toeach injector solenoid in order to provide completecontrol of the engine.



Fuel Injection

The ECM controls the amount of fuel that is injectedby varying the signals that are sent to the injectors.The ECM sends a high voltage signal to the solenoidin order to energize the solenoid. The injectorswill inject fuel only while the injector solenoid isenergized. By controlling the timing and the durationof the voltage signal, the ECM can control injectiontiming and the amount of fuel that is injected.

The ECM sets certain limits on the amount of fuel thatcan be injected. “FRC” is a limit which controls theamount of air and of fuel for the purpose of emissioncontrol. This limit is based on the boost pressure.When the ECM senses a higher boost pressure, theECM increases the “FRC” limit. “Rated Fuel Pos” isa limit that is based on the horsepower rating of theengine. This is similar to the rack stops and to thetorque spring on a mechanically governed engine.“Rated Fuel Pos” provides horsepower and torquecurves for a specific engine family and for a specificengine rating. All of these limits are programmedinto the ECM by the factory. These limits are notprogrammable by the service technician.

Injection timing depends on three factors: the enginespeed (rpm), the engine load, and the operationalconditions of the engine. The ECM determines thetop center position of No. 1 cylinder from the signalthat is provided by the engine speed/timing sensor.The ECM decides when the injection should occurrelative to the top center position. The ECM thenprovides the signal to the electronic unit injector atthe desired time.

Electronic Unit Injector Mechanism


Typical examples of Electronic Unit Injector fuel systems.(1) Adjusting nut(2) Rocker arm assembly(3) Unit injector(4) Pushrod

The unit injector pressurizes the fuel. The correctamount of fuel is then injected into the cylinder blockat precise times. The ECM determines the injectiontiming and the amount of fuel that is delivered. Theunit injector is operated by a camshaft lobe and arocker arm. The camshaft has three camshaft lobesfor each cylinder. Two lobes operate the inlet andexhaust valves, and the other lobe operates theunit injector mechanism. Force is transferred fromthe unit injector lobe on the camshaft through thelifter to the pushrod (4). The force of the pushrodis transferred through rocker arm assembly (2) andto the top of the unit injector. The adjusting nut (1)allows setting of the unit injector adjustment. Refer toSystems Operation/Testing and Adjusting, “ElectronicUnit Injector - Adjust” for the correct setting of theunit injector adjustment.



Electronic Unit Injector

g00984466Illustration 7Electronic unit injector(1) Spring(2) Solenoid connection to the Electronic Control Module (ECM)(3) Solenoid valve assembly(4) Plunger assembly(5) Barrel(6) Seal(7) Seal(8) Spring(9) Spacer(10) Body(11) Check valve

Fuel at low pressure from the fuel supply manifoldenters the electronic unit injector at the fill portthrough drilled passages in the cylinder head.

As the electronic unit injector mechanism transfersthe force to the top of the electronic unit injector,spring (1) is compressed and plunger (4) is drivendownward. This action displaces fuel through thevalve in solenoid valve assembly (3), and into thereturn manifold to the fuel tank. As the plunger travelsdownward, the passage in barrel (5) is closed by theoutside diameter of the plunger. The passages withinbody (10) and along check valve (11) to the injectortip already contain fuel for injection. After the passagein the plunger barrel is closed, the injector is ready forinjection at any time. The start of injection relies onthe software in the Electronic Control Module (ECM).

When the solenoid valve assembly is energizedfrom a signal across solenoid connection (2), thevalve closes and fuel pressure is elevated in theinjector tip. Injection begins at 34500 ± 1900 kPa(5000 ± 275 psi) as the force of spring (8) abovespacer (9) is overcome. The check valve beginsto lift from the valve seat. The pressure continuesto rise as the plunger cycles through a full stroke.After the correct amount of fuel has been dischargedinto the cylinder, the ECM removes the signal to thesolenoid connection. The solenoid valve assemblyis de-energized and the valve in the solenoid valveassembly is opened. The high pressure fuel is thendumped through the spill port and into the fuel returnmanifold. The fuel is then returned to the fuel tank.The check valve in the injector tip seats as thepressure in the tip decreases.

The duration of injection meters the fuel that isconsumed during the fuel injection process. Injectionduration is controlled by the governor logic that isprogrammed into the ECM.

As the camshaft lobe rotates past the point ofmaximum lobe lift, the force on top of the electronicunit injector is removed and the spring for the injectormechanism is allowed to expand. The plunger returnsto the original position. This uncovers the fuel supplypassage into the plunger barrel in order to refill theinjector pump body. The fuel at low pressure is againallowed to circulate through the fuel injector body.After circulating through the fuel injector body, thefuel flows out of the spill port. This continues until thesolenoid valve assembly is re-energized for anotherinjection cycle.



i02769479

Air Inlet and Exhaust System


Air inlet and exhaust system schematic(1) Inlet to the engine(2) Aftercooler core(3) Inlet air line(4) Exhaust outlet from turbocharger(5) Turbine side of turbocharger(6) Compressor side of turbocharger(7) Air cleaner

The engine components of the air inlet and exhaustsystem control the quality of air and the amount ofair that is available for combustion. The componentsof the air inlet and exhaust system are the followingcomponents:

• Air cleaner

• Turbocharger

• Aftercooler

• Cylinder head

• Valves and valve system components

• Piston and cylinder

• Exhaust manifold

The turbocharger compressor wheel pulls inlet airthrough the air cleaner and into the air inlet. The airis compressed and this causes the air to become hot.The air flows through aftercooler core (2) and thetemperature of the compressed air lowers. This helpsto provide increased horsepower output. Aftercoolercore (2) is a separate cooler core that is mounted infront of the engine radiator. The engine fan causesambient air to move across both cores. This cools theturbocharged inlet air and the engine coolant.

Air is forced from the aftercooler into inlet manifold(1). The air flow from the inlet port into the cylindersis controlled by inlet valves.

g00615497Illustration 9Air inlet and exhaust system(2) Aftercooler core(4) Exhaust outlet(5) Turbine side of turbocharger(6) Compressor side of turbocharger(8) Exhaust manifold(9) Exhaust valve(10) Inlet valve(11) Air inlet

Each cylinder has two inlet valves (10) and twoexhaust valves (9) in the cylinder head. The inletvalves open on the inlet stroke. When the inlet valvesopen, compressed air from the inlet port within theinlet manifold is pushed into the cylinder. The inletvalves close when the piston begins the compressionstroke. The air in the cylinder is compressed and thefuel is injected into the cylinder when the piston isnear the top of the compression stroke. Combustionbegins when the fuel mixes with the air. The force ofcombustion pushes the piston on the power stroke.The exhaust valves open and the exhaust gasesare pushed through the exhaust port into exhaustmanifold (8). After the piston finishes the exhauststroke, the exhaust valves close and the cycle beginsagain.

Exhaust gases from the exhaust manifold flowinto the turbine side of turbocharger (5). The hightemperature exhaust gases cause the turbochargerturbine wheel to turn. The turbine wheel is connectedto the shaft that drives the compressor wheel.Exhaust gases from the turbocharger pass throughexhaust outlet (4), through a muffler, and through anexhaust stack.



Turbocharger


Turbocharger(4) Air inlet(5) Compressor housing(6) Compressor wheel(7) Bearing(8) Oil inlet port(9) Bearing(10) Turbine housing(11) Turbine wheel(12) Exhaust outlet(13) Oil outlet port(14) Exhaust inlet

Turbocharger (3) is mounted to exhaust manifold (2)of the engine. All of the exhaust gases go from theexhaust manifold through the turbocharger.

The exhaust gases enter the turbocharger and theturbine wheel is turned. Because the turbochargerturbine wheel is connected by a shaft to theturbocharger compressor wheel, the turbine wheeland the compressor wheel turn at very high speeds.The rotation of the compressor wheel pulls cleanair through the compressor housing air inlet. Theaction of the compressor wheel blades causes acompression of the inlet air. This compression allowsa larger amount of air to enter the engine. With moreair in the engine, the engine is able to burn more fuel.The overall effect is an increase in power.

Bearing (7) and bearing (9) in the turbocharger useengine oil that is under pressure for lubrication. Thelubrication for the bearings flows through oil inlet port(8) and into the inlet port in the center section of theturbocharger cartridge. The oil exits the turbochargerthrough oil outlet port (13). The oil then returns tothe engine oil pan through the oil drain line for theturbocharger.

Valve System Components

g01086490Illustration 11(1) Rocker arm(2) Pushrod(3) Valve bridge(4) Valve spring(5) Valve(6) Lifter

The valve system components control the flow ofinlet air into the cylinders and out of the cylindersduring engine operation. The valve mechanism alsooperates the fuel injector.

The camshaft must be timed to the crankshaft inorder to get the correct relation between the pistonmovement and the valve movement.

The camshaft has two camshaft lobes for eachcylinder. The lobes operate the inlet and exhaustvalves. As the camshaft turns, lobes on the camshaftcause lifters (6) to move pushrods (2) up and down.Upward movement of the pushrods against rockerarms (1) results in downward movement (opening) ofvalves (5).

Each cylinder has two inlet valves and two exhaustvalves. The valves are actuated at the same time bya valve bridge (3). Valve springs (4) close the valveswhen the lifters move down.



i02843427

Lubrication System

g01417920Illustration 12Lubrication system schematic

(1) Piston cooling jets(2) Main oil gallery in cylinder block(3) Engine pressure sensor(4) Oil flow to valve mechanism(5) Camshaft journals

(6) Oil filter bypass valve(7) Main bearings(8) Signal line(9) Primary engine oil filter(10) Engine oil pump

(11) Oil cooler bypass valve(12) Engine oil cooler(13) Oil pan sump(14) High pressure relief valve(15) Oil pump bypass valve




Right side view of engine(9) Primary engine oil filter(10) Engine oil pump(12) Engine oil cooler

The lubrication system supplies 110 °C (230 °F)filtered oil at approximately 275 kPa (40 psi) at ratedengine operating conditions. Oil pump bypass valve(15) is controlled by the engine oil manifold pressure,rather than the oil pump pressure. The engine oilmanifold pressure is independent of the pressuredrop that is caused by the engine oil filter and theengine oil cooler.

Oil cooler bypass valve (11) maintains the engine oiltemperature to 110 °C (230 °F). High pressure reliefvalve (14), which is located in the filter base, protectsthe filters and other components during cold starts.The opening pressure of the high pressure reliefvalve is 695 kPa (100 psi). The opening pressure ofthe oil filter bypass valve is 170 kPa (25 psi). Engineoil pressure sensor (3) is part of the engine protectionsystem.

The turbocharger cartridge bearings are lubricated bythe oil supply line from the main oil gallery, and the oildrain line returns the oil flow to the sump.

i02769599

Cooling System

Coolant Flow

g01085911Illustration 14Cooling system schematic

(1) Cylinder head(2) Expansion tank(3) Return manifold(4) Cylinder liners(5) Temperature regulator housing(6) Radiator(7) Water pump(8) Engine oil cooler

Note: Use Perkins ELC in an Air to Air AftercoolerSystem. Refer to Operation and MaintenanceManual, “Fluid Recommendations” for furtherinformation. This keeps the temperature range of thecoolant high enough for efficient performance.

The water pump is gear-driven. The water pump islocated on the right hand side of the engine. Thewater pump supplies the coolant for the enginecooling system. The coolant is supplied to thefollowing components:

• Cylinder head (1)

• Cylinder liners (4)

• Engine oil cooler (8)

• Air compressor (not shown)

• Coolant conditioner element (not shown)



g01413806Illustration 15(3) Return manifold(5) Temperature regulator housing

(7) Water pump(8) Engine oil cooler

Water pump (8) pulls the coolant from the bottom ofradiator. The water pump is located on the right handside of the front timing gear housing.

The water pump impeller rotates at 1.17 times theengine speed. The water pump is driven by an idlergear. The idler gear is turned by the crankshaftgear. The water pump shaft is supported by two ballbearings. One ball bearing is located in the waterpump housing. The other ball bearing is located in thefront timing gear housing. The water pump impellerface is open. The impeller is made out of cast iron.The rear cover is an aluminum die casting. The waterpump seal is a cartridge seal that is located on theinlet side of the water pump in order to provide goodwater flow around the seal for cooling.



The coolant is pumped through engine oil cooler(9). The coolant then flows to the supply manifold.The supply manifold, which is located in the cylinderblock, distributes coolant around the upper portionof the cylinder liners. At each cylinder, the coolantflows from the cylinder liner to the cylinder head.The cylinder head is divided into single cylindercooling sections. In the cylinder head, the coolantflows across the center of the cylinder and acrossthe injector seat boss. At the center of the cylinder,the coolant flows around the injector sleeve overthe exhaust port. The coolant then exits into returnmanifold (3). The return manifold collects thecoolant from each cylinder and the return manifolddirects the flow to temperature regulator housing(5). When the coolant temperature regulator isin the closed position, the coolant flows throughthe coolant temperature regulator. This allows thecoolant to flow directly back to the water pump forrecirculation by bypassing the radiator. When thecoolant temperature regulator is in the open position,the coolant is directed through the radiator and backto the water pump inlet.

Supply ManifoldCooling is provided for only the portion of the cylinderliner above the seal in the cylinder block. The coolantenters the cylinder block at each cylinder throughslits in the supply manifold. The supply manifold isan integral casting in the cylinder block. The coolantflows around the circumference of the cylinder linerand into the cylinder head through a single drilledpassage for each liner. The coolant flow is split ateach cylinder liner so that 60 percent flows aroundthe cylinder liner and the remainder flows directly tothe cylinder head.

Temperature Regulator Housing


Section view of the temperature regulator housing(1) Temperature regulator housing(2) Coolant temperature sensor

The coolant temperature regulator is a full flowbypass type that is used to control the outlettemperature of the coolant. When the engine iscold, the coolant temperature regulator is in theclosed position. This allows the coolant to flowthrough the coolant temperature regulator from thereturn manifold. This allows the coolant to bypassthe radiator. The coolant goes directly to the waterpump for recirculation. As the coolant temperatureincreases, the coolant temperature regulator beginsto open directing some of the coolant to the radiatorand bypassing the remainder to the water pump inlet.At the full operating temperature of the engine, thecoolant temperature regulator moves to the openposition. This allows all the coolant flow to be directedto the radiator. The coolant then goes to the waterpump. This route provides the maximum heat releasefrom the coolant. A vent line is recommended fromthe manifold to the radiator overflow tank in order toprovide venting for the cooling system.



i02773143

Basic Engine

Cylinder BlockThe cylinder block is a unique design with a deepcounterbore that supports the cylinder liner. Thecylinder block also forms the coolant jacket. Twooil manifolds are provided in the cylinder block forengine lubrication. The manifold on the lower rightside of the cylinder block provides oil to the followingcomponents:

• Piston cooling jets

• Crankshaft bearings

• Oil filter base

The manifold on the upper left side of the cylinderblock provides oil to the following components:

• Camshaft bearings

• Valve mechanism

The manifold on the right supplies oil to the manifoldon the left. The oil travels through the cut above thenumber one main bearing and the cut above thenumber four main bearing.


Cylinder liners (1) are seated on a ridge (4) in themiddle of the cylinder wall between the crankcaseand the coolant jacket. The ridge is created by acounterbore in the cylinder block. The cylinder linershave a lip (2) which rests on the ridge. The seals ofthe coolant jacket are located in the upper regionsand middle regions of the cylinder liners. The lowerbarrier uses a D-ring seal (3) that is located above theseating surface of the cylinder liner. The upper barrieris the head gasket which is above the coolant jacket.

The cylinder block has seven main bearings in orderto support the crankshaft. Each main bearing cap isfastened to the cylinder block with two bolts.

Pistons, Rings, and ConnectingRodsThe high compression ratio of the engine requiresthe use of steel one piece pistons.

The pistons have three rings:

• Compression ring

• Intermediate ring

• Oil ring

The rings are located in grooves in the piston. Therings seal the crankcase from the combustion gasesand the rings also provide control of the engineoil. The design of the compression ring is a barrelface with a plasma face coating. The design of theintermediate ring is a tapered shape and a chromefinish. The oil ring is double railed with a coil springexpander. The oil ring has a ground profile and achrome finish.

The connecting rod is a conventional design. Thecap is fastened to the shank by two bolts that arethreaded into the shank. Each side of the small endof the connecting rod is machined at an angle of12 degrees in order to fit within the piston cavity.This allows a larger surface area on the piston, andconnecting rod in order to minimize bearing load.

CrankshaftThe crankshaft converts the linear motion of thepistons into rotational motion. The crankshaft drivesa group of gears (front gear train) on the front of theengine. The front gear train provides power for thefollowing components:

• Camshaft

• Water pump



• Engine oil pump

• Air compressor

• Fuel transfer pump

• Accessory drive

The crankshaft is held in place by seven mainbearings. The oil holes and the oil grooves in theshell of the upper bearing supply oil to the connectingrod bearings. The oil holes for the connecting rodbearings are located at the following main bearingjournals: 2, 3, 5, and 6.

Hydrodynamic seals are used at both ends of thecrankshaft to control oil leakage. The hydrodynamicgrooves in the seal lip move lubrication oil back intothe crankcase as the crankshaft turns. The frontseal is located in the front housing. The rear seal isinstalled in the flywheel housing.

Camshaft


The camshaft has three lobes at each cylinder inorder to operate the unit injector, the exhaust valves,and the inlet valves. Seven bearings support thecamshaft. The camshaft is driven by an idler gearthat is turned by the crankshaft in the front geartrain. Each bearing journal is lubricated from the oilmanifold in the cylinder block. A thrust pin that islocated at the rear of the block positions the camshaftthrough a circumferential groove. The groove ismachined at the rear of the camshaft. Timing of thecamshaft is accomplished by aligning marks on thecrankshaft gear, idler gear, and camshaft gear witheach other.

The injector lobe on the camshaft has a modifiedprofile. The modified profile produces multipleinjections.

Vibration DamperThe force from combustion in the cylinders and fromdriveline components will cause the crankshaft totwist. This is called torsional vibration. If the vibrationis too great, the crankshaft will be damaged. Drivelinecomponents can excite torsional stress. This stresswill cause damage to components. The vibrationdamper limits the torsional vibrations to an acceptableamount in order to prevent damage to the crankshaft.

The viscous vibration damper is installed on the frontof the crankshaft. The viscous vibration damper hasa weight in a case. The space between the weightand the case is filled with a viscous fluid. The weightmoves in the case in order to limit the torsionalvibration.

i02773144

Electrical System

Grounding PracticesCorrect grounding for the machine electrical systemand engine electrical systems is necessary forcorrect machine performance and reliability. Impropergrounding will result in uncontrolled electrical circuitpaths and unreliable electrical circuit paths.

Uncontrolled engine electrical circuit paths can resultin damage to main bearings, crankshaft bearingjournal surfaces, and aluminum components.

To ensure correct functioning of the application andengine electrical systems, an engine-to-frame groundstrap with a direct path to the negative battery postmust be used. This may be provided by way of astarting motor ground, a frame to starting motorground, or a direct frame to engine ground.

An engine-to-frame ground strap must be used inorder to connect the grounding stud of the engineto the frame of the application and to the negativebattery post.




(1) Starting motor to engine block(2) Starting motor to battery negative

The engine must have a wire ground to the battery.

Ground wires or ground straps should be combinedat ground studs that are only for ground use. All ofthe grounds should be tight and free of corrosion.

All of the ground paths must be capable of carryingany likely current faults. An AWG #0 or larger wire isrecommended for the grounding strap to the cylinderhead.

The engine alternator should be battery groundwith a wire size that is capable of managing the fullcharging current of the alternator.

NOTICEWhen boost starting an engine, the instructions in Op-eration and Maintenance Manual, “Engine Starting”should be followed in order to correctly start the en-gine.

This engine is equipped with a 24 volt starting system.Only equal voltage for boost starting should be used.The use of a higher voltage will damage the electricalsystem.

The Electronic Control Module (ECM) must be dis-connected at the “J1/P1” and “J2/P2” locations beforewelding on the application.

The engine has several input components which areelectronic. These components require an operatingvoltage.

Unlike many electronic systems of the past, thisengine is tolerant to common external sources ofelectrical noise. Buzzers that use electrical energycan cause disruptions in the power supply. If buzzersare used anywhere on the machine, the engineelectronics should be powered directly from thebattery system through a dedicated relay. The engineelectronics should not be powered through a commonpower bus with other keyswitch activated devices.

Engine Electrical SystemThe electrical system has the following separatecircuits:

• Charging

• Starting (If equipped)

• Accessories with low amperage

The charging circuit is in operation when the engineis running. An alternator makes electricity for thecharging circuit. A voltage regulator in the circuitcontrols the electrical output in order to keep thebattery at full charge.

The starting circuit is activated only when the startswitch is activated.

Charging System Components

Alternator

The alternator is driven by a belt from the crankshaftpulley. This alternator is a three-phase, self-rectifyingcharging unit, and the regulator is part of thealternator.

The alternator design has no need for slip ringsand the only part that has movement is the rotorassembly. All conductors that carry current arestationary. The following conductors are in the circuit:

• Field winding

• Stator windings

• Six rectifying diodes

• Regulator circuit components



The rotor assembly has many magnetic poles thatlook like fingers with air space between each of theopposite poles. The poles have residual magnetism.The residual magnetism produces a small magneticfield between the poles. As the rotor assemblybegins to turn between the field winding and thestator windings, a small amount of alternating current(AC) is produced. The AC current is produced in thestator windings from the small magnetic field. TheAC current is changed to direct current (DC) whenthe AC current passes through the diodes of therectifier bridge. The current is used for the followingapplications:

• Charging the battery

• Supplying the accessory circuit that has the lowamperage

• Strengthening the magnetic field

The first two applications use the majority of thecurrent. As the DC current increases through thefield windings, the strength of the magnetic field isincreased. As the magnetic field becomes stronger,more AC current is produced in the stator windings.The increased speed of the rotor assembly alsoincreases the current and voltage output of thealternator.

The voltage regulator is a solid-state electronicswitch. The voltage regulator senses the voltage inthe system. The voltage regulator switches ON andOFF many times per second in order to control thefield current for the alternator. The alternator usesthe field current in order to generate the requiredvoltage output.

NOTICENever operate the alternator without the battery in thecircuit. Making or breaking an alternator connectionwith heavy load on the circuit can cause damage tothe regulator.

g00425518Illustration 20Typical alternator components

(1) Regulator(2) Roller bearing(3) Stator winding(4) Ball bearing(5) Rectifier bridge(6) Field winding(7) Rotor assembly(8) Fan

Starting System Components

Starting Solenoid

g00317613Illustration 21Typical starting solenoid



g00425521Illustration 22Typical starting motor components

(1) Field(2) Solenoid(3) Clutch(4) Pinion(5) Commutator(6) Brush assembly(7) Armature

The starting solenoid (2) is an electromagnetic switchthat performs the following basic operations:

• The starting solenoid (2) closes the high currentstarting motor circuit with a low current start switchcircuit.

• The starting solenoid (2) engages the pinion of thestarting motor (4) with the ring gear.

Solenoid (2) has windings (one or two sets) arounda hollow cylinder. A plunger that is spring loaded isinside the cylinder. The plunger can move forwardand backward. When the start switch is closed andelectricity is sent through the windings, a magneticfield (1) is made. The magnetic field (1) pulls theplunger forward in the cylinder. This moves the shiftlever in order to engage the pinion drive gear with thering gear. The front end of the plunger then makescontact across the battery and motor terminals ofsolenoid (2). Next, the starting motor begins to turnthe flywheel of the engine.

When the start switch is opened, current no longerflows through the windings. The spring now pushesthe plunger back to the original position. At the sametime, the spring moves the pinion gear away fromthe flywheel.

When two sets of solenoid windings are used, thewindings are called the hold-in winding and thepull-in winding. Both sets of windings have the samenumber of turns around the cylinder, but the pull-inwinding uses a wire with a larger diameter. The wirewith a larger diameter produces a greater magneticfield (1). When the start switch is closed, part of thecurrent flows from the battery through the hold-inwindings. The rest of the current flows through thepull-in windings to the motor terminal. The currentthen flows through the motor to ground. Solenoid(2)is fully activated when the connection across thebattery and the motor terminal is complete. Whensolenoid (2) is fully activated, the current is shutoff through the pull-in windings. At this point, onlythe smaller hold-in windings are in operation. Thehold-in windings operate for the duration of time thatis required in order to start the engine. Solenoid (2)will now draw less current from the battery, and theheat that is generated by solenoid (2) will be kept atan acceptable level.


KENR6907 23Testing and Adjusting Section

Testing and AdjustingSection

Testing and Adjustingi02773145

Belt Tension Chart

Table 1

Required Tools

Tool Part Number Part Description Qty

A - Belt Tension Gauge 1

Table 2

Fan Drive Belt Tension Chart

Gauge ReadingSize of Belt Top Width of Belt

Initial Belt Tension(1) Used Belt Tension(2)

5 VX 16 mm (0.629 inch) 868 N (195 lb) 800 N (180 lb)

Measure the tension of the belt that is farthest from the engine.(1) Initial Belt Tension refers to a new belt.(2) Used Belt Tension refers to a belt that has been in operation for 30 minutes or more at the rated speed.

Install Tooling (A) at the center of the longest freelength of belt and check the tension on the belt.Check and adjust the tension on the tightest belt.To adjust the belt tension, refer to Disassembly andAssembly, “Belt Tightener - Install”.

Note: When the belts are replaced, always replacethe belts as a set.

Table 3

Alternator Belt Tension Chart

Gauge ReadingSize of Belt Top Width of Belt

Initial Belt Tension(1) Used Belt Tension(2)

3 VX 9.7 mm (0.381 inch) 400 N (89.9240 lb) 267 N (60.0243 lb)

Measure the tension of the belt that is farthest from the engine.(1) Initial Belt Tension refers to a new belt.(2) Used Belt Tension refers to a belt that has been in operation for 30 minutes or more at the rated speed.

Install Tooling (A) at the center of the longest freelength of belt and check the tension on the belt.Check and adjust the tension on the tightest belt.To adjust the belt tension, refer to Disassembly andAssembly, “Alternator - Install”.


24 KENR6907Testing and Adjusting Section

Fuel Systemi02773147

Fuel System - Inspect

A problem with the components that send fuel tothe engine can cause low fuel pressure. This candecrease engine performance.

1. Check the fuel level in the fuel tank. Ensure thatthe vent in the fuel cap is not filled with dirt.

2. Check all fuel lines for fuel leakage. The fuel linesmust be free from restrictions and faulty bends.Verify that the fuel return line is not collapsed.

3. Install a new fuel filter.

4. Cut the old filter open with a suitable filter cutter.Inspect the filter for excess contamination.Determine the source of the contamination. Makethe necessary repairs.

5. Service the primary fuel filter (if equipped).

6. Operate the hand priming pump (if equipped).If excessive resistance is felt, inspect the fuelpressure regulating valve. If uneven resistanceis felt, test for air in the fuel. Refer to SystemsOperation, Testing and Adjusting, “Air in Fuel -Test” for more information.

7. Remove any air that may be in the fuel system.Refer to Systems Operation, Testing andAdjusting, “Fuel System - Prime”.

i02773148

Air in Fuel - Test

This procedure checks for air in the fuel. Thisprocedure also assists in finding the source of the air.

1. Examine the fuel system for leaks. Ensure thatthe fuel line fittings are properly tightened. Checkthe fuel level in the fuel tank. Air can enter thefuel system on the suction side between the fueltransfer pump and the fuel tank.

2. Install a suitable fuel flow tube with a visual sightgauge in the fuel return line. When possible, installthe sight gauge in a straight section of the fuel linethat is at least 304.8 mm (12 inches) long. Do notinstall the sight gauge near the following devicesthat create turbulence:

• Elbows

• Relief valves

• Check valves

Observe the fuel flow during engine cranking.Look for air bubbles in the fuel. If there is no fuelin the sight gauge, prime the fuel system. Refer toSystem Operation, Testing and Adjusting, “FuelSystem - Prime” for more information. If the enginestarts, check for air in the fuel at varying enginespeeds. When possible, operate the engine underthe conditions which have been suspect of air inthe fuel.


(1) A steady stream of small bubbles with a diameter ofapproximately 1.60 mm (0.063 inch) is an acceptable amountof air in the fuel.

(2) Bubbles with a diameter of approximately 6.35 mm (0.250 inch)are also acceptable if there is two seconds to three secondsintervals between bubbles.

(3) Excessive air bubbles in the fuel are not acceptable.

3. If excessive air is seen in the sight gauge in thefuel return line, install a second sight gauge atthe inlet to the fuel transfer pump. If a secondsight gauge is not available, move the sight gaugefrom the fuel return line and install the sight gaugeat the inlet to the fuel transfer pump. Observethe fuel flow during engine cranking. Look for airbubbles in the fuel. If the engine starts, check forair in the fuel at varying engine speeds.

If excessive air is not seen at the inlet to the fueltransfer pump, the air is entering the system afterthe fuel transfer pump. Proceed to Step 6.



If excessive air is seen at the inlet to the fueltransfer pump, air is entering through the suctionside of the fuel system.

To avoid personal injury, always wear eye and faceprotection when using pressurized air.

4. Pressurize the fuel tank to the recommendationsof the OEM in order to avoid damage to the fueltank. Check for leaks in the fuel lines betweenthe fuel tank and the fuel transfer pump. Repairany leaks that are found. Check the fuel pressurein order to ensure that the fuel transfer pump isoperating properly. For information about checkingthe fuel pressure, see System Operation, Testingand Adjusting, “Fuel System Pressure - Test”.

5. If the source of the air is not found, disconnectthe supply line from the fuel tank and connect anexternal fuel supply to the inlet of the fuel transferpump. If this corrects the problem, repair the fueltank or the stand pipe in the fuel tank.

6. If the injector sleeve is worn or damaged,combustion gases may be leaking into the fuelsystem. Also, if the O-rings on the injector sleevesare worn, missing, or damaged, combustion gasesmay leak into the fuel system.

i02799187

Electronic Unit Injector - Adjust

g01126970Illustration 24Injector Mechanism(1) Rocker arm(2) Adjustment screw(3) Locknut

Follow the procedure in order to adjust your electronicunit injectors:

1. Put the No. 1 piston at the top center positionon the compression stroke. Refer to SystemsOperation/Testing and Adjusting, “Finding TopCenter Position for No. 1 Piston”.

a. Cylinder 3, 5, and 6 can be adjusted withcylinder 1 at TC compression stroke.

b. Loosen the jam nut.

c. Turn the adjustment screw until the screwmakes contact with the electronic unit injector.

d. Turn the adjustment screw through 180degrees in a clockwise direction.

e. Tighten the jam nut to a torque of 55 ± 10 N·m(41 ± 7 lb ft).

2. Rotate the engine in the normal operating directionby 360 degrees. Cylinder 1 will now be on TCexhaust stroke.

a. Cylinder 1, 2, and 4 can be adjusted withcylinder 1 at TC exhaust stroke.

b. Loosen the jam nut.



c. Turn the adjustment screw until the screwmakes contact with the electronic unit injector.

d. Turn the adjustment screw through 180degrees in a clockwise direction.

e. Tighten the jam nut to a torque of 55 ± 10 N·m(41 ± 7 lb ft).

i02773150

Electronic Unit Injector - Test

This procedure assists in identifying the cause foran injector misfiring. Perform this procedure onlyafter performing the Cylinder Cutout Test. Refer toTroubleshooting for more information.

1. Check for air in the fuel, if this procedure hasnot already been performed. Refer to SystemsOperation, Testing and Adjusting, “Air in Fuel -Test”.

Electrical shock hazard. The electronic unit injec-tor system uses 90-120 volts.

2. Remove the valve cover and look for brokenparts. Repair any broken parts or replace anybroken parts that are found. Inspect all wiring tothe solenoids. Look for loose connections. Alsolook for frayed wires or broken wires. Ensurethat the connector for the unit injector solenoidis properly connected. Perform a pull test oneach of the wires. Refer to Troubleshooting,“Electrical Connectors - Inspect”. Inspect the postsof the solenoid for arcing. If arcing or evidenceof arcing is found, remove the cap assembly.Refer to Disassembly and Assembly, “ElectronicUnit Injector - Remove”. Clean the connectingposts. Reinstall the cap assembly and tightenthe solenoid nuts to a torque of 2.5 ± 0.25 N·m(22 ± 2 lb in). Refer to Disassembly and Assembly,“Electronic Unit Injector - Install”.

3. Check the valve lash setting for the cylinder of thesuspect unit injector. Refer to Systems Operation,Testing and Adjusting, “Engine Valve Lash -Inspect/Adjust”.

4. Ensure that the bolt that holds the unit injector istightened to the proper torque. If necessary, loosenthe bolt that holds the unit injector and tighten thebolt to a torque of 55 ± 10 N·m (40.6 ± 7.4 lb ft).

5. Remove the suspect unit injector and check theunit injector for signs of exposure to coolant. Referto Disassembly and Assembly, “Electronic UnitInjector - Remove”. Exposure to coolant will causerust to form on the injector. If the unit injectorshows signs of exposure to coolant, remove theinjector sleeve and inspect the injector sleeve.Refer to Disassembly and Assembly, “ElectronicUnit Injector Sleeve - Remove”. Replace theinjector sleeve if the injector sleeve is damaged.Check the unit injector for an excessive browndiscoloration that extends beyond the injector tip. Ifexcessive discoloration is found, check the qualityof the fuel. Refer to Systems Operation, Testingand Adjusting, “Fuel Quality - Test”. Replace theseals on the injector and reinstall the injector.Refer to Disassembly and Assembly, “ElectronicUnit Injector - Install”. Also refer to Disassemblyand Assembly, “Electronic Unit Injector Sleeve -Install”.

6. If the problem is not resolved, replace the suspectinjector with a new injector.

i02793631

Finding Top Center Positionfor No. 1 Piston

Table 4

Required Tools


A CH11148 Engine turning tool 1

B CVT0015 Adapter 1

C 27610286 Timing pin 1




(1) Flywheel housing(2) Timing hole plug(3) Cover bolt(4) Cover

1. Remove two bolts (3) and remove cover (4) fromflywheel housing (1) in order to open the turninghole.

2. Insert Tooling (B) into the timing hole (2).The timing hole is located approximately127 to 152 mm (5.0 to 6.0 inch) above the turninghole for Tooling (A) in the flywheel housing. UseTooling (A) in order to turn the engine flywheel.Turn the flywheel in the direction of enginerotation. The direction of engine rotation iscounterclockwise, as the engine is viewed fromthe flywheel end. Turn the flywheel until Tooling(C) engages with the hole in the flywheel.

Note: If the flywheel is turned beyond the point ofengagement, the flywheel must be turned in thedirection that is reverse of normal engine rotation.Turn the flywheel by approximately 30 degrees. Thenturn the flywheel in the direction of normal rotationuntil Tooling (C) engages with the hole in the flywheel.This procedure removes the play from the gearswhen the No. 1 piston is at the top center position.

3. Remove the valve mechanism cover from theengine.

4. The inlet and exhaust valves for the No. 1cylinder are fully closed if No. 1 piston is on thecompression stroke and the rocker arms can bemoved by hand. If the rocker arms cannot bemoved and the valves are slightly open, the No. 1piston is on the exhaust stroke.

Note: When the actual stroke position is identified,and the other stroke position is needed, removeTooling (C) from the hole in the flywheel. Then turnthe flywheel by 360 degrees in the direction of normalengine rotation and reinstall Tooling (C) into the holein the flywheel.

Note: Never turn the engine by the crankshaftvibration damper. The crankshaft vibration damper isa precision part. Major engine failure may be causedby damage to the crankshaft vibration damper.

i02773153

Fuel Quality - Test

Ensure that all adjustments and repairs are performedby authorized personnel that have had the correcttraining.

Use the following procedure to test for problemsregarding fuel quality:

1. Determine if water and/or contaminants arepresent in the fuel. Check the water separator (ifequipped). If a water separator is not present,proceed to Step 2. Drain the water separator, ifnecessary. A full fuel tank minimizes the potentialfor overnight condensation.

Note: A water separator can appear to be full of fuelwhen the water separator is actually full of water.

2. Determine if contaminants are present in thefuel. Remove a sample of fuel from the bottomof the fuel tank. Visually inspect the fuel samplefor contaminants. The color of the fuel is notnecessarily an indication of fuel quality. However,fuel that is black, brown, and/or similar to sludgecan be an indication of the growth of bacteria oroil contamination. In cold temperatures, cloudyfuel indicates that the fuel may not be suitable foroperating conditions.

Refer to Operation and Maintenance Manual,“Fluid Recommendations” for more information.



3. If fuel quality is still suspected as a possiblecause to problems regarding engine performance,disconnect the fuel inlet line, and temporarilyoperate the engine from a separate source offuel that is known to be good. This will determineif the problem is caused by fuel quality. If fuelquality is determined to be the problem, drain thefuel system and replace the fuel filters. Engineperformance can be affected by the followingcharacteristics:

• Cetane number of the fuel

• Air in the fuel

• Other fuel characteristics

i02788192

Fuel System - Prime

NOTICEUse a suitable container to catch any fuel that mightspill. Clean up any spilled fuel immediately.

NOTICEDo not allow dirt to enter the fuel system. Thoroughlyclean the area around a fuel system component thatwill be disconnected. Fit a suitable cover over discon-nected fuel system component.

Note: This procedure is most common when theengine has run out of fuel.

1. Turn the ignition switch to the “OFF” position.

2. Fill the fuel tank(s) with clean diesel fuel.


Typical example

3. Loosen the union of the pipe for the fuel(1).

Note: Do not remove the union completely. Open theunion enough to allow the air that is trapped in thecylinder head to be purged from the fuel system.

4. Unlock and operate the hand priming pump (2).Use a suitable container to collect excess fuel.

5. Tighten the union of the pipe for the fuel (1).

6. Operate the hand priming pump until a strongpressure is felt on the pump. Push the primingpump plunger inward. Tighten the plunger by handand start the engine.

NOTICEDo not crank the engine continuously for more than30 seconds. Allow the starting motor to cool for 30seconds before cranking the engine again.

7. If the engine will not start, allow the starting motorto cool for 30 seconds. Repeat steps 3 to 6 inorder to operate the engine.

8. Continue to eliminate air from the fuel system ifthese events occur:



• The engine starts, but the engine does not runevenly.

• The engine starts, but the engine continues tomisfire or smoke.

9. Run the engine with no load until the engine runssmoothly.

i02788197

Fuel System Pressure - Test

Low Fuel PressureLow fuel pressure can cause low power. Low fuelpressure can also cause cavitation of the fuelwhich can damage the fuel injectors. The followingconditions can cause low fuel pressure:

• Plugged fuel filters

• Debris in the check valves for the fuel primingpump

• Debris in the pressure regulating valve

• Partially open check valve

• Sticking or worn fuel pressure regulating valve inthe fuel transfer pump

• Severe wear on return fuel pressure regulatingvalve in the fuel filter base

• Worn gears in the fuel transfer pump

• Pinched fuel lines or undersized fuel lines

• Old fuel lines that have a reduced interior diameterthat was caused by swelling

• Fuel lines with deteriorating interior surfaces

• Pinched fuel line fittings or undersized fuel linefittings

• Debris in the fuel tank, fuel lines, or fuel systemcomponents that create restrictions

High Fuel PressureExcessive fuel pressure can cause fuel filter gasketsto rupture. The following conditions can cause highfuel pressure:

• Plugged orifices in the fuel pressure regulatingvalve

• Stuck fuel pressure regulating valve in the fueltransfer pump

• Pinched fuel return line

Checking Fuel PressureTable 5

Required Tools


A - Pressure Gauge 1


To check the fuel transfer pump pressure, removethe hose assembly (1). Install a pressure gauge, andstart the engine.

Fuel Pressure ReadingsThe typical fuel pressure of the engine at operatingtemperature can vary. When the engine is underload, the fuel pressure can be 550 kPa (80 psi).

The performance of the unit injector deteriorateswhen the fuel pressure drops below 241 kPa (35 psi).Low power complaints and erratic operation canoccur in this situation. Check for a plugged fuel filteror air in the fuel lines as possible causes for thesecomplaints before replacing fuel system components.



i02788237

Gear Group (Front) - Time

g01126079Illustration 28Front Gear Group(1) Camshaft gear and timing reference ring(2) Timing marks(3) Idler gear(4) Crankshaft gear

The basis for correct fuel injection timing and valvemechanism operation is determined by the timingreference ring and the alignment of the front geargroup. The timing reference ring is located on the endof the camshaft. The timing reference ring is used tomeasure crankshaft rotation. During installation ofthe front gear, timing marks (2) on idler gear (3) mustbe in alignment with the timing marks on crankshaftgear (4) and the timing marks on camshaft gear (1).

Refer to Disassembly and Assembly, “Gear Group(Front) - Remove” and Disassembly and Assembly,“Gear Group (Front) - Install”.

Note: If timing reference ring (1) is installed backwardthe engine will not start.

Check for proper alignment of the camshaft gear andtiming reference ring (1) on the camshaft assembly.Inspect the key between the timing reference ringand the camshaft gear. Check the teeth on the timingring. The teeth should not be defaced. The teethshould have sharp clean edges and the teeth shouldbe free of contaminants.

Note: The electronic injection timing must becalibrated after reassembly of the front gear train.Refer to Troubleshooting, “Engine Speed/TimingSensor - Calibrate”.



Air Inlet and ExhaustSystem

i02788810

Air Inlet and Exhaust System- Inspect

A general visual inspection should be made to the airinlet and exhaust system. Make sure that there areno signs of leaks in the system.

Table 6

Required Tools


A - Differential PressureGauge 1

Air Inlet RestrictionThere will be a reduction in the performance of theengine if there is a restriction in the air inlet system.

1. Inspect the engine air cleaner inlet and ductingin order to ensure that the passageway is notblocked or collapsed.

2. Inspect the engine air cleaner element. Replacea dirty engine air cleaner element with a cleanengine air cleaner element.

3. Check for dirt tracks on the clean side of theengine air cleaner element. If dirt tracks areobserved, contaminants are flowing past theengine air cleaner element and/or the seal for theengine air cleaner element.

Hot engine components can cause injury fromburns. Before performing maintenance on theengine, allow the engine and the components tocool.

Making contact with a running engine can causeburns from hot parts and can cause injury fromrotating parts.

When working on an engine that is running, avoidcontact with hot parts and rotating parts.

4. Use Tooling (A) for this test.




Air inlet piping(1) Air Cleaner (2) Test location (3) Turbocharger

a. Connect the vacuum port of the differentialpressure gauge to test location (2). Testlocation (2) may be located anywhere along theair inlet piping after air cleaner (1) but beforeturbocharger (3).

b. Leave the pressure port of the differentialpressure gauge open to the atmosphere.

c. Start the engine. Run the engine at full load.

d. Record the value.

e. Compare the result from step 4.d to theappropriate values that follow.

The air flow through a used engine air cleanermay have a restriction. The air flow through aplugged engine air cleaner will be restricted to somemagnitude. In either case, the restriction must not bemore than the following amount:

Maximum restriction ........ 6.2 kPa (25 in of H2O)

The air flow through a new engine air cleaner elementmust not have a restriction of more than the followingamount:

Maximum restriction ........ 3.7 kPa (15 in of H2O)

i02788812

Turbocharger - Inspect

Hot engine components can cause injury fromburns. Before performing maintenance on theengine, allow the engine and the components tocool.

Personal injury can result from rotating and mov-ing parts.

Stay clear of all rotating and moving parts.

Never attempt adjustments while the machine ismoving or the engine is running unless otherwisespecified.

The machine must be parked on a level surfaceand the engine stopped.



NOTICEKeep all parts clean from contaminants.

Contaminants may cause rapid wear and shortenedcomponent life.

NOTICECare must be taken to ensure that fluids are containedduring performance of inspection, maintenance, test-ing, adjusting and repair of the product. Be prepared tocollect the fluid with suitable containers before open-ing any compartment or disassembling any compo-nent containing fluids.

Dispose of all fluids according to local regulations andmandates.

Before you begin inspection of the turbocharger,be sure that the inlet air restriction is within thespecifications for your engine. Be sure that theexhaust system restriction is within the specificationsfor your engine. Refer to Systems Operation, Testingand Adjusting, “Air Inlet and Exhaust System -Inspect”.

The condition of the turbocharger will have definiteeffects on engine performance. Use the followinginspections and procedures to determine thecondition of the turbocharger.

• Inspection of the Compressor and the CompressorHousing

• Inspection of the Turbine Wheel and the TurbineHousing

Inspection of the Compressor andthe Compressor HousingRemove air piping from the compressor inlet.

1. Inspect the compressor wheel for damage from aforeign object. If there is damage, determine thesource of the foreign object. As required, cleanthe inlet system and repair the intake system.Replace the turbocharger. If there is no damage,go to Step 3.

2. Clean the compressor wheel and clean thecompressor housing if you find buildup of foreignmaterial. If there is no buildup of foreign material,go to Step 3.

3. Turn the rotating assembly by hand. While youturn the assembly, push the assembly sideways .The assembly should turn freely. The compressorwheel should not rub the compressor housing.Replace the turbocharger if the compressor wheelrubs the compressor wheel housing. If there is norubbing or scraping, go to Step 4.

4. Inspect the compressor and the compressorwheel housing for oil leakage. An oil leak fromthe compressor may deposit oil in the aftercooler.Drain and clean the aftercooler if you find oil inthe aftercooler.

a. Check the oil level in the crankcase. If the oillevel is too high, adjust the oil level.

b. Inspect the air cleaner element for restriction. Ifrestriction is found, correct the problem.

c. Inspect the engine crankcase breather. Cleanthe engine crankcase breather or replacethe engine crankcase breather if the enginecrankcase breather is plugged.

d. Remove the oil drain line for the turbocharger.Inspect the drain opening. Inspect the oil drainline. Inspect the area between the bearings ofthe rotating assembly shaft. Look for oil sludge.Inspect the oil drain hole for oil sludge. Inspectthe oil drain line for oil sludge in the drainline. If necessary, clean the rotating assemblyshaft. If necessary, clean the oil drain hole. Ifnecessary, clean the oil drain line.

e. If Steps 4.a through 4.d did not reveal thesource of the oil leakage, the turbocharger hasinternal damage. Replace the turbocharger.

Inspection of the Turbine Wheeland the Turbine HousingRemove the air piping from the turbine housing.

g00763164Illustration 30Typical example(1) Turbine Housing(2) Turbine Wheel(3) Turbocharger



1. Inspect the turbine for damage by a foreign object.If there is damage, determine the source of theforeign object. Replace turbocharger (3). If thereis no damage, go to Step 2.

2. Inspect turbine wheel (2) for buildup of carbon andother foreign material. Inspect turbine housing (1)for buildup of carbon and foreign material. Cleanturbine wheel (2) and clean turbine housing (1) ifyou find buildup of carbon or foreign material. Ifthere is no buildup of carbon or foreign material,go to Step 3.

3. Turn the rotating assembly by hand. While youturn the assembly, push the assembly sideways.The assembly should turn freely. Turbine wheel (2)should not rub turbine wheel housing (1). Replaceturbocharger (3) if turbine wheel (2) rubs turbinehousing (1). If there is no rubbing or scraping, goto Step 4.

4. Inspect the turbine and turbine housing (1) for oilleakage. Inspect the turbine and turbine housing(1) for oil coking. Some oil coking may be cleaned.Heavy oil coking may require replacement ofthe turbocharger. If the oil is coming from theturbocharger center housing go to Step 4.a.

a. Remove the oil drain line for the turbocharger.Inspect the drain opening. Inspect the areabetween the bearings of the rotating assemblyshaft. Look for oil sludge. Inspect the oil drainhole for oil sludge. Inspect the oil drain linefor oil sludge. If necessary, clean the rotatingassembly shaft. If necessary, clean the drainopening. If necessary, clean the drain line.

b. If crankcase pressure is high, or if the oil drainis restricted, pressure in the center housingmay be greater than the pressure of turbinehousing (1). Oil flow may be forced in the wrongdirection and the oil may not drain. Check thecrankcase pressure and correct any problems.

c. If the oil drain line is damaged, replace the oildrain line.

d. Check the routing of the oil drain line. Eliminateany sharp restrictive bends. Make sure thatthe oil drain line is not too close to the engineexhaust manifold.

e. If Steps 4.a through 4.d did not reveal thesource of the oil leakage, turbocharger (3) hasinternal damage. Replace turbocharger (3).

i02788813

Exhaust Temperature - Test

Table 7

Required Tools


A - Infrared Thermometer 1

When the engine runs, the temperature of an exhaustmanifold port can indicate the condition of a fuelinjection nozzle.

A low temperature indicates that no fuel is flowing tothe cylinder. An inoperative fuel injection nozzle ora problem with the fuel injection pump could causethis low temperature.

A very high temperature can indicate that too muchfuel is flowing to the cylinder. A malfunctioningfuel injection nozzle could cause this very hightemperature.

Use Tooling (A) to check exhaust temperature.

i02788814

Engine Crankcase Pressure(Blowby) - Test

Table 8

Required Tools

ToolPart

Number Part Name Quantity


Damaged pistons or rings can cause too muchpressure in the crankcase. This condition will causethe engine to run rough. There will be more than thenormal amount of fumes (blowby) rising from thecrankcase breather. The breather can then becomerestricted in a very short time, causing oil leakageat gaskets and seals that would not normally haveleakage. Blowby can also be caused by worn valveguides or by a failed turbocharger seal.

Install Tooling (A) to the most convenient location onthe output tube for the crankcase breather or thebreather hose. The pressure for the engine blowbyshould be 0.25 kPa (1 inch of H2O).



Note: Do not use the data alone to determine if theengine should be overhauled. Other indicators suchas high oil consumption, low power, hard starting,and excessive fuel consumption must be considered.

After a new engine is used for a short time, theblowby can decrease as the rings are seated. Newengines should be checked for blowby during allmaintenance checks. As the piston rings and cylinderwalls wear, the blowby will gradually increase.

The blowby on a worn engine may be two times ormore than the blowby of a new engine and mayindicate the need for an overhaul.

i02788818

Engine Valve Lash -Inspect/Adjust

To prevent possible injury, do not use the starterto turn the flywheel.

Hot engine components can cause burns. Allowadditional time for the engine to cool before mea-suring valve clearance.

This engine uses high voltage to control the fuelinjectors.

Disconnect electronic fuel injector enable circuitconnector to prevent personal injury.

Do not come in contact with the fuel injector ter-minals while the engine is running.

Note: Valve lash is measured between the rockerarm and the valve bridge. All measurements andadjustments must be made with the engine stoppedand the valves fully closed.

Valve Lash CheckAn adjustment is NOT NECESSARY if themeasurement of the valve lash is in the acceptablerange in Table 9.

Table 9

Inlet Valves Exhaust Valves

Valve Lash(StoppedEngine)

0.38 ± 0.08 mm(0.015 ± 0.003

inch)

0.64 ± 0.08 mm(0.025 ± 0.003 inch)

TCCompression

Stroke1-2-4 1-3-5

TC ExhaustStroke(1) 3-5-6 2-4-6

Firing Order 1-5-3-6-2-4(2)

(1) 360° from TC compression stroke(2) The No. 1 cylinder is at the front of the engine.

If the measurement is not within this range, anadjustment is necessary. Refer to “Valve LashAdjustment” for the proper procedure.

Valve Lash Adjustment


Cylinder and valve location

(A) Exhaust valves(B) Inlet valves

Use the following procedure to adjust the valve lash:

1. Put the No. 1 piston at the top center positionon the compression stroke. Refer to SystemsOperation, Testing and Adjusting, “Finding TopCenter Position for No. 1 Piston”.

Table 10

CompressionStroke for No.1 Piston

Inlet Valves Exhaust Valves

Valve Lash0.38 ± 0.08 mm(0.015 ± 0.003

inch)

0.64 ± 0.08 mm(0.025 ± 0.003

inch)

Cylinders 1-2-4 1-3-5

2. Adjust the valve lash according to Table 10.



a. Lightly tap the rocker arm with a soft mallet.This will ensure that the lifter roller seatsagainst the camshaft’s base circle.

b. Loosen the adjustment locknut.

c. Place the appropriate feeler gauge betweenrocker arm and the valve bridge. Then, turnthe adjustment screw in a clockwise direction.Slide the feeler gauge between the rocker armand the valve bridge. Continue turning theadjustment screw until a slight drag is felt onthe feeler gauge. Remove the feeler gauge.

d. Tighten the adjustment locknut to a torqueof 30 ± 7 N·m (22 ± 5 lb ft). Do not allowthe adjustment screw to turn while you aretightening the adjustment locknut. Recheckthe valve lash after tightening the adjustmentlocknut.

Note: If necessary, adjust the electronic unit injectorson cylinders 3, 5 and 6. Refer to Systems Operation,Testing and Adjusting, “Electronic Unit Injector -Adjust” for the correct procedure.

3. Remove the timing pin. Turn the flywheel by 360degrees in the direction of engine rotation. Thiswill put the No. 6 piston at the top center positionon the compression stroke. Install the timing pin.

Table 11

CompressionStroke for No.6

PistonInlet Valves Exhaust Valves

Valve Lash0.38 ± 0.08 mm(0.015 ± 0.003

inch)

0.64 ± 0.08 mm(0.025 ± 0.003

inch)

Cylinders 3-5-6 2-4-6

4. Adjust the valve lash according to Table 11.

a. Lightly tap the rocker arm with a soft mallet.This will ensure that the lifter roller seatsagainst the camshaft’s base circle.

b. Loosen the adjustment locknut.

c. Place the appropriate feeler gauge betweenrocker arm and the valve bridge. Then, turnthe adjustment screw in a clockwise direction.Slide the feeler gauge between the rocker armand the valve bridge. Continue turning theadjustment screw until a slight drag is felt onthe feeler gauge. Remove the feeler gauge.

d. Tighten the adjustment locknut to a torqueof 30 ± 7 N·m (22 ± 5 lb ft). Do not allowthe adjustment screw to turn while you aretightening the adjustment locknut. Recheckthe valve lash after tightening the adjustmentlocknut.

5. Remove the timing bolt from the flywheel after alladjustments to the valve lash have been made.Reinstall the timing cover.

Refer to Systems Operation, Testing and Adjusting,“Electronic Unit Injector - Adjust”.



Lubrication Systemi02788819

Engine Oil Pressure - Test

The engine oil pressure may be checkedelectronically by using the electronic service tool.The engine oil pressure can be measured with theelectronic service tool. Refer to Troubleshooting forinformation on the use of the electronic service tool.

Measuring Engine Oil Pressure

Work carefully around an engine that is running.Engine parts that are hot, or parts that are moving,can cause personal injury.





Table 12

Required Tools

ToolPart

Number Part Name Quantity


Tool (A) measures the oil pressure in the system.


Oil gallery plug(1) Plug

1. Install Tool (A) into the oil gallery plugs (1).

Note: Engine oil pressure to the camshaft and mainbearings should be checked on each side of thecylinder block at oil gallery plugs (1).

2. Start the engine. Refer to Operation andMaintenance Manual, “Fluid Recommendations”for the correct engine oil.

3. Record the value of the engine oil pressure whenthe engine is at operating temperature 100 °C(212 °F).

The minimum engine oil pressure should beapproximately 275 to 414 kPa (40 to 59 psi).

4. Compare the recorded engine oil pressure withthe oil pressure indicators on the instrument paneland the engine oil pressure that is displayed onthe electronic service tool.

5. An engine oil pressure indicator that has a defector an engine oil pressure sensor that has a defectcan give a false indication of a low oil pressure ora high oil pressure. If there is a notable differencebetween the engine oil pressure readings makenecessary repairs.

6. If low engine oil pressure is determined, refer to“Reasons for Low Engine Oil Pressure”.



7. If high engine oil pressure is determined, refer to“Reason for High Engine Oil Pressure”.

Reasons for Low Engine OilPressure





• Engine oil level is low. Refer to Step 1.

• Engine oil is contaminated. Refer to Step 2.

• The engine oil bypass valves are open. Refer toStep 3.

• The engine lubrication system is open. Refer toStep 4.

• The oil pickup tube has a leak or a restricted inletscreen. Refer to Step 5.

• The engine oil pump is faulty. Refer to Step 6.

• Engine Bearings have excessive clearance. Referto Step 7.

1. Check the engine oil level in the crankcase. Theoil level can possibly be too far below the oil pumpsupply tube. This will cause the oil pump not tohave the ability to supply enough lubrication to theengine components. If the engine oil level is lowadd engine oil in order to obtain the correct engineoil level. Refer to Operation and MaintenanceManual, “Fluid Recommendations” for the correctengine oil.

2. Engine oil that is contaminated with fuel orcoolant will cause low engine oil pressure. Highengine oil level in the crankcase can be anindication of contamination. Determine the reasonfor contamination of the engine oil and makethe necessary repairs. Replace the engine oilwith the approved grade of engine oil. Referto Operation and Maintenance Manual, “FluidRecommendations” for the correct engine oil.

NOTICEPerkins oil filters are manufactured to Perkins speci-fications. Use of an oil filter that is not recommendedby Perkins could result in severe damage to the en-gine bearings, crankshaft, etc., as a result of the largerwaste particles from unfiltered oil entering the enginelubricating system. Only use oil filters recommendedby Perkins.

3. If the engine oil bypass valves are held in theopen position, a reduction in the oil pressure canbe the result. This may be due to debris in theengine oil. If the engine oil bypass valves arestuck in the open position, remove each engineoil bypass valve and clean each bypass valvein order to correct this problem. You must alsoclean each bypass valve bore. Install new engineoil filters. New engine oil filters will prevent moredebris from causing this problem. For informationon the repair of the engine oil bypass valves, referto Disassembly and Assembly, “Engine Oil FilterBase - Disassemble”.

4. An oil line or an oil passage that is open, broken,or disconnected will cause low engine oil pressure.An open lubrication system could be caused bya piston cooling jet that is missing or damaged.Determine the reason for an open lubricationsystem of the engine and make the necessaryrepairs.

Note: The piston cooling jets direct engine oil towardthe bottom of the piston in order to cool the piston.This also provides lubrication for the piston pin.Breakage, a restriction or incorrect installation of thepiston cooling jets will cause seizure of the piston.

5. The inlet screen of the oil pickup tube for theengine oil pump can have a restriction. Thisrestriction will cause cavitation and a loss ofengine oil pressure. Check the inlet screen onthe oil pickup tube and remove any material thatmay be restricting engine oil flow. Low engine oilpressure may also be the result of the oil pickuptube that is drawing in air. Check the joints of theoil pickup tube for cracks or a damaged O-ringseal. Remove the engine oil pan in order to gainaccess to the oil pickup tube and the oil screen.Refer to Disassembly and Assembly, “Engine OilPan - Remove and Install” for more information.



6. Check the following problems that may occur tothe engine oil pump.

a. Air leakage in the supply side of the oil pumpwill also cause cavitation and loss of oilpressure. Check the supply side of the oil pumpand make necessary repairs. For informationon the repair of the engine oil pump, refer toDisassembly and Assembly, “Engine Oil Pump- Remove”.

b. Oil pump gears that have too much wear willcause a reduction in oil pressure. Repair theengine oil pump. For information on the repairof the engine oil pump, refer to Disassemblyand Assembly, “Engine Oil Pump - Remove”.

7. Excessive clearance at engine bearings willcause low engine oil pressure. Check theengine components that have excessive bearingclearance and make the necessary repairs.

Reason for High Engine OilPressure





Engine oil pressure will be high if the engine oilbypass valves become stuck in the closed positionand the engine oil flow is restricted. Foreign matterin the engine oil system could be the cause for therestriction of the oil flow and the movement of theengine oil bypass valves. If the engine oil bypassvalves are stuck in the closed position, removeeach bypass valve and clean each bypass valve inorder to correct this problem. You must also cleaneach bypass valve bore. Install new engine oilfilters. New engine oil filters will prevent more debrisfrom causing this problem. For information on therepair of the engine oil filter bypass valve, refer toDisassembly and Assembly, “Engine Oil Filter Base -Disassemble”.

NOTICEPerkins oil filters are manufactured to Perkins speci-fications. Use of an oil filter that is not recommendedby Perkins could result in severe damage to the en-gine bearings, crankshaft, etc., as a result of the largerwaste particles from unfiltered oil entering the enginelubricating system. Only use oil filters recommendedby Perkins.

i02788840

Excessive Bearing Wear -Inspect

When some components of the engine show bearingwear in a short time, the cause can be a restriction inan oil passage.

An engine oil pressure indicator may show that thereis enough oil pressure, but a component is worndue to a lack of lubrication. In such a case, look atthe passage for the oil supply to the component.A restriction in an oil supply passage will not allowenough lubrication to reach a component. This willresult in early wear.

i02788843

Excessive Engine OilConsumption - Inspect

Engine Oil Leaks on the Outside ofthe EngineCheck for leakage at the seals at each end of thecrankshaft. Look for leakage at the gasket for theengine oil pan and all lubrication system connections.Look for any engine oil that may be leaking fromthe crankcase breather. This can be caused bycombustion gas leakage around the pistons. A dirtycrankcase breather will cause high pressure in thecrankcase. A dirty crankcase breather will cause thegaskets and the seals to leak.

Engine Oil Leaks into theCombustion Area of the CylindersEngine oil that is leaking into the combustion area ofthe cylinders can be the cause of blue smoke. Thereare several possible ways for engine oil to leak intothe combustion area of the cylinders:

• Leaks between worn valve guides and valve stems



• Worn components or damaged components(pistons, piston rings, or dirty return holes for theengine oil)

• Incorrect installation of the compression ring and/orthe intermediate ring

• Leaks past the seal rings in the turbocharger shaft

• Overfilling of the crankcase

• Wrong dipstick or guide tube

Excessive consumption of engine oil can alsoresult if engine oil with the wrong viscosity is used.Engine oil with a thin viscosity can be caused by fuelleakage into the crankcase or by increased enginetemperature.

i02788844

Increased Engine OilTemperature - Inspect

If the oil temperature is high, then check for arestriction in the oil passages of the oil cooler. Arestriction in the oil cooler will not cause low oilpressure in the engine.

Determine if the oil cooler bypass valve is held in theopen position. This condition will allow the oil to passthrough the valve instead of the oil cooler. The oiltemperature will increase.

Refer to Operation and Maintenance Manual, “RefillCapacities” for the correct lubricating oil.



Cooling Systemi02788847

Cooling System - Check(Overheating)

Above normal coolant temperatures can be causedby many conditions. Use the following procedureto determine the cause of above normal coolanttemperatures:

Personal injury can result from escaping fluid un-der pressure.

If a pressure indication is shown on the indicator,push the release valve in order to relieve pressurebefore removing any hose from the radiator.

1. Check the coolant level in the cooling system.Refer to Operation and Maintenance Manual,“Cooling System Coolant Level - Check”. If thecoolant level is too low, air will get into the coolingsystem. Air in the cooling system will cause areduction in coolant flow and bubbles in thecoolant. Air bubbles will keep coolant away fromthe engine parts, which will prevent the transfer ofheat to the coolant. Low coolant level is caused byleaks or incorrectly filling the radiator.

2. Check the mixture of antifreeze and water. Referto Operation and Maintenance Manual, “FluidRecommendations”. If the coolant mixture isincorrect, drain the system. Put the correct mixtureof water, antifreeze and coolant conditioner in thecooling system.

3. Check for air in the cooling system. Air can enterthe cooling system in different ways. The mostcommon causes of air in the cooling systemare not filling the cooling system correctly andcombustion gas leakage into the cooling system.Combustion gas can get into the system throughinside cracks, a damaged cylinder head, or adamaged cylinder head gasket. Air in the coolingsystem causes a reduction in coolant flow andbubbles in the coolant. Air bubbles keep coolantaway from the engine parts, which prevents thetransfer of heat to the coolant.

4. Check the water temperature gauge. A watertemperature gauge which does not work correctlywill not show the correct temperature. Referto Systems Operation, Testing and Adjusting,“Cooling System - Inspect”.

5. Check the sending unit. In some conditions, thetemperature sensor in the engine sends signals toa sending unit. The sending unit converts thesesignals to an electrical impulse which is used by amounted gauge. If the sending unit malfunctions,the gauge can show an incorrect reading. Also ifthe electric wire breaks or if the electric wire shortsout, the gauge can show an incorrect reading.

6. Check the radiator.

a. Check the radiator for a restriction to coolantflow. Check the radiator for debris, dirt, ordeposits on the inside of the radiator core.Debris, dirt, or deposits will restrict the flow ofcoolant through the radiator.

b. Check for debris or damage between the finsof the radiator core. Debris between the finsof the radiator core restricts air flow throughthe radiator core. Refer to Systems Operation,Testing and Adjusting, “Cooling System -Inspect”.

c. Ensure that the radiator size is adequate forthe application. An undersized radiator doesnot have enough area for the effective releaseof heat. This may cause the engine to runat a temperature that is higher than normal.The normal temperature is dependent on theambient temperature.

7. Check the filler cap. A pressure drop in theradiator can cause the boiling point to be lower.This can cause the cooling system to boil. Referto Systems Operation, Testing and Adjusting,“Cooling System - Test”.

8. Check the fan and/or the fan shroud.

a. The fan must be large enough to send airthrough most of the area of the radiator core.Ensure that the size of the fan and the positionof the fan are adequate for the application.

b. The fan shroud must be the proper size andthe fan shroud must be positioned correctly.Ensure that the size of the fan shroud and theposition of the fan shroud are adequate for theapplication.

9. If the fan is belt driven, check for loose drive belts.A loose fan drive belt will cause a reduction in theair flow across the radiator. Check the fan drivebelt for proper belt tension. Adjust the tension ofthe fan drive belt, if necessary. Refer to SystemsOperation, Testing and Adjusting, “Belt TensionChart”.



10.Check the cooling system hoses and clamps.Damaged hoses with leaks can normally be seen.Hoses that have no visual leaks can soften duringoperation. The soft areas of the hose can becomekinked or crushed during operation. These areasof the hose can cause a restriction in the coolantflow. Hoses become soft and/or get cracksafter a period of time. The inside of a hose candeteriorate, and the loose particles of the hosecan cause a restriction of the coolant flow. Referto Operation and Maintenance Manual, “Hosesand Clamps - Inspect/Replace”.

11.Check for a restriction in the air inlet system.A restriction of the air that is coming into theengine can cause high cylinder temperatures.High cylinder temperatures cause higher thannormal temperatures in the cooling system. Referto Systems Operation, Testing and Adjusting, “AirInlet and Exhaust System - Inspect”.

a. If the measured restriction is higher than themaximum permissible restriction, remove theforeign material from the engine air cleanerelement or install a new engine air cleanerelement. Refer to Operation and MaintenanceManual, “Engine Air Cleaner Element -Clean/Replace”.

b. Check for a restriction in the air inlet systemagain.

c. If the measured restriction is still higher thanthe maximum permissible restriction, check theair inlet piping for a restriction.

12.Check for a restriction in the exhaust system.A restriction of the air that is coming out of theengine can cause high cylinder temperatures.

a. Make a visual inspection of the exhaust system.Check for damage to exhaust piping or for adamaged muffler. If no damage is found, checkthe exhaust system for a restriction. Refer toSystems Operation, Testing and Adjusting, “AirInlet and Exhaust System - Inspect”.

b. If the measured restriction is higher than themaximum permissible restriction, there is arestriction in the exhaust system. Repair theexhaust system, as required.

13.Check the shunt line, if the shunt system isused. The shunt line must be submerged in theexpansion tank. A restriction of the shunt linefrom the radiator top tank to the engine waterpump inlet will cause a reduction in water pumpefficiency. A reduction in water pump efficiencywill result in low coolant flow and overheating.

14.Check the water temperature regulator. A watertemperature regulator that does not open, ora water temperature regulator that only openspart of the way can cause overheating. Refer toSystems Operation, Testing and Adjusting, “WaterTemperature Regulator - Test”.

15.Check the water pump. A water pump with adamaged impeller does not pump enough coolantfor correct engine cooling. Remove the waterpump and check for damage to the impeller. Referto Systems Operation, Testing and Adjusting,“Water Pump - Test”.

16.Check the air flow through the enginecompartment. The air flow through the radiatorcomes out of the engine compartment. Ensurethat the filters, air conditioner, and similar itemsare not installed in a way that prevents the freeflow of air through the engine compartment.

17.Check the aftercooler. A restriction of air flowthrough the air to air aftercooler (if equipped) cancause overheating. Check for debris or depositswhich would prevent the free flow of air throughthe aftercooler.

18.Consider high outside temperatures. Whenoutside temperatures are too high for the ratingof the cooling system, there is not enough of atemperature difference between the outside airand coolant temperatures.

19.Consider high altitude operation. The coolingcapacity of the cooling system goes down asthe engine is operated at higher altitudes. Apressurized cooling system that is large enough tokeep the coolant from boiling must be used.

i02788851

Cooling System - Inspect

Cooling systems that are not regularly inspected arethe cause for increased engine temperatures. Makea visual inspection of the cooling system before anytests are performed.





1. Check the coolant level in the cooling system.Refer to Operation and Maintenance Manual,“Cooling System Coolant Level - Check”.

2. Check the quality of the coolant. The coolantshould have the following properties:

• Color that is similar to new coolant

• Odor that is similar to new coolant

• Free from dirt and debris

If the coolant does not have these properties,drain the system and flush the system. Refillthe cooling system with the correct mixture ofwater, antifreeze, and coolant conditioner. Referto Operation and Maintenance Manual, “FluidRecommendations”.

3. Look for leaks in the system.

Note: A small amount of coolant leakage acrossthe surface of the water pump seals is normal. Thisleakage is required in order to provide lubrication forthis type of seal. A hole is provided in the water pumphousing in order to allow this coolant/seal lubricantto drain from the pump housing. Intermittent leakageof small amounts of coolant from this hole is not anindication of water pump seal failure.

4. Ensure that the air flow through the radiator doesnot have a restriction. Look for bent core finsbetween the folded cores of the radiator. Also, lookfor debris between the folded cores of the radiator.

5. Inspect the drive belts for the fan.

6. Check for damage to the fan blades.

7. Look for air or combustion gas in the coolingsystem.

8. Inspect the filler cap, and check the surface thatseals the filler cap. This surface must be clean.

i02788878

Cooling System - Test

This engine has a pressure type cooling system. Apressure type cooling system has two advantages.The cooling system can be operated in a safe mannerat a temperature higher than the normal boiling point(steam) of water.

This type of system prevents cavitation in the waterpump. Cavitation is the forming of low pressurebubbles in liquids that are caused by mechanicalforces. It is difficult to create a pocket of air in thistype of cooling system.

g00921815Illustration 33Boiling point of water

Remember that temperature and pressure worktogether. When a diagnosis is made of a coolingsystem problem, temperature and pressure must bechecked. Cooling system pressure will have an effecton the cooling system temperature. For an example,refer to Illustration 33. This will show the effect ofpressure on the boiling point (steam) of water. Thiswill also show the effect of height above sea level.

Personal injury can result from hot coolant, steamand alkali.

At operating temperature, engine coolant is hotand under pressure. The radiator and all linesto heaters or the engine contain hot coolant orsteam. Any contact can cause severe burns.

Remove filler cap slowly to relieve pressure onlywhen engine is stopped and radiator cap is coolenough to touch with your bare hand.

Cooling SystemConditioner contains alkali. Avoidcontact with skin and eyes.

The coolant level must be to the correct level in orderto check the coolant system. The engine must becold and the engine must not be running.

After the engine is cool, loosen the pressure capin order to relieve the pressure out of the coolingsystem. Then remove the pressure cap.

The level of the coolant should not be more than13 mm (0.5 inch) from the bottom of the filler pipe. Ifthe cooling system is equipped with a sight glass,the coolant should be to the proper level in the sightglass.



Checking the Filler CapTable 13

Required Tools


A GE50031 Pressurizing Pump 1

One cause for a pressure loss in the cooling systemcan be a damaged seal on the radiator filler cap.

g01096114Illustration 34Typical schematic of filler cap

(1) Sealing surface of both filler cap and radiator





To check for the amount of pressure that opens thefiller cap, use the following procedure:

1. After the engine cools, carefully loosen the fillercap. Slowly release the pressure from the coolingsystem. Then, remove the filler cap.

Carefully inspect the filler cap. Look for anydamage to the seals and to the sealing surface.Inspect the following components for any foreignsubstances:

• Filler cap

• Seal

• Surface for seal

Remove any deposits that are found on theseitems, and remove any material that is found onthese items.

2. Install the filler cap onto Tooling (A).

3. Look at the gauge for the exact pressure thatopens the filler cap.

4. Compare the gauge reading with the openingpressure that is listed on the filler cap.

5. If the filler cap is damaged, replace the filler cap.

Testing The Radiator And CoolingSystem For LeaksTable 14

Required Tools


A GE50031 Pressurizing Pump 1

Use the following procedure in order to check thecooling system for leaks:





1. After the engine is cool, loosen the filler cap slowlyand allow pressure out of the cooling system.Then remove the filler cap from the radiator.

2. Ensure that the coolant level is above the top ofthe radiator core.

3. Install Tooling (A) onto the radiator.

4. Take the pressure reading on the gauge to 20 kPa(3 psi) more than the pressure on the filler cap.



5. Check the radiator for leakage on the outside.

6. Check all connection points for leakage, andcheck the hoses for leakage.

The cooling system does not have leakage only if thefollowing conditions exist:.

• You do not observe any outside leakage.

• The reading remains steady after five minutes.

The inside of the cooling system has leakage only ifthe following conditions exist:

• The reading on the gauge goes down.

• You do NOT observe any outside leakage.

Make any repairs, as required.

Test For The Water TemperatureGaugeTable 15

Required Tools


A - Thermometer 1





Check the accuracy of the water temperatureindicator or water temperature sensor if you findeither of the following conditions:

• The engine runs at a temperature that is too hot,but a normal temperature is indicated. A loss ofcoolant is found.

• The engine runs at a normal temperature, but ahot temperature is indicated. No loss of coolant isfound.

Coolant temperature can also be read on the displayscreens of the Electronic Service Tool.

g01096115Illustration 35Typical example(1) Water manifold assembly

Remove a plug from water manifold assembly (1).Install Tooling (A) in the open port:

A temperature indicator of known accuracy can alsobe used to make this check.

Start the engine. Run the engine until the temperaturereaches the desired range according to the testthermometer. If necessary, place a cover over part ofthe radiator in order to cause a restriction of the airflow. The reading on the water temperature indicatorshould agree with the test thermometer within thetolerance range of the water temperature indicator.

i02788898

Water Temperature Regulator- Test



1. Remove the water temperature regulator from theengine.



2. Heat water in a suitable container until thetemperature is 98 °C (208 °F).

3. Hang the water temperature regulator in thecontainer of water. The water temperatureregulator must be below the surface of the waterand away from the sides and the bottom of thecontainer.

4. Keep the water at the correct temperature for tenminutes.

5. After ten minutes, remove the water temperatureregulator. Ensure that the water temperatureregulator is open.

Replace the water temperature regulator if thewater temperature regulator is not open at thespecified temperature. Refer to Specifications,“Water Temperature Regulator”.

i02788939

Water Pump - Test

Table 16

Required Tools


A GE50033 Pressure Gauge 1




Typical example(1) Port(2) Water manifold

Perform the following procedure in order to determineif the water pump is operating correctly:

1. Remove one plug from port (1).

2. Install Tooling (A) in port (1).

3. Start the engine. Run the engine until thecoolant is at operating temperature. Refer toSpecifications, “Water Temperature Regulator” forfurther information.

4. Note the water pump pressure. The water pumppressure should be 100 to 125 kPa (15 to 18 psi).



Basic Enginei02788973

Piston Ring Groove - Inspect

Inspect the Piston and the PistonRings1. Check the piston for wear and other damage.

2. Check that the piston rings are free to move in thegrooves and that the rings are not broken.

Inspect the Clearance of the PistonRing1. Remove the piston rings and clean the groovesand the piston rings.

2. Fit new piston rings in the piston grooves.

3. Check the clearance for the piston ring by placinga suitable feeler gauge between the piston grooveand the top of piston ring. Refer to Specifications,“Piston and Rings” for the dimensions.

Inspect the Piston Ring End Gap1. Clean all carbon from the top of the cylinder bores.

2. Place each piston ring in the cylinder bore justbelow the cylinder ring ridge.

3. Use a suitable feeler gauge to measure pistonring end gap. Refer to Specifications, “Piston andRings” for the dimensions.

Note: The coil spring must be removed from the oilcontrol ring before the gap of the oil control ring ismeasured.

i02799220

Connecting Rod Bearings -Inspect

The connecting rod bearings fit tightly in the bore inthe rod. If the bearing joints are worn, check the boresize. This can be an indication of wear because ofa loose fit.

Connecting rod bearings are available with smallerinside diameters than the original size bearings.These bearings are for crankshafts that have beenground.

If necessary, replace the connecting rod bearings.Refer to Disassembly and Assembly, “ConnectingRod Bearings - Remove” and Disassembly andAssembly, “Connecting Rod Bearings - Install” for thecorrect procedure.

i02801041

Main Bearings - Inspect

Main bearings are available with smaller insidediameters than the original size bearings. Thesebearings are for crankshafts that have been ground.

If necessary, replace the main bearings. Referto Disassembly and Assembly, “Crankshaft MainBearings - Remove and Install” for the correctprocedure.

i02801042

Cylinder Block - Inspect

1. Clean all of the coolant passages and the oilpassages.

2. Check the cylinder block for cracks and damage.

3. The top deck of the cylinder block must not bemachined. This will affect the depth of the cylinderliner flange and the piston height above thecylinder block.

4. Check the front camshaft bearing for wear. Referto Specifications, “Camshaft Bearings” for thecorrect specification of the camshaft bearing. If anew bearing is needed, use a suitable adapter topress the bearing out of the bore. Ensure that theoil hole in the new bearing faces the front of theblock. The oil hole in the bearing must be alignedwith the oil hole in the cylinder block. The bearingmust be aligned with the face of the recess.



i02846965

Cylinder Liner Projection -Inspect

Table 17

Required Tools


A - Clamp bolt (M16 x 2mm) 6

B GE50006 Clamp washer 6

C GE50007 Clamp washer 6

D GE50002 Cylinder linerprojection tool 1

1. Clean the cylinder liner flange and the cylinderblock surface. Remove any nicks on the top of thecylinder block (1).

2. Install the cylinder liners to the cylinder blockwithout seals or bands. Ensure that the cylinderliners are installed to the original positions.


3. Install Tooling (B) and Tooling (C) to Tooling (A).Install Tooling (A) around the liner (2). Refer toillustration 37.

4. Tighten the clamp bolts to a torque of 14 N·m(10 lb ft).

5. Use Tooling (D) to measure the cylinder linerprojection at "A", "B", "C" and "D". Refer toillustration 38.

6. Record the measurements for the cylinder.

7. Repeat steps 3 to 6 for each cylinder.

8. Add the four readings for each cylinder. Divide thesum by four in order to find the average.

Table 18

Specifications

Liner Projection 0.06 to 0.18 mm( 0.0024 to 0.0071 inch)

Maximum Variation inEach Liner 0.050 mm (0.0020 inch)

Maximum AverageVariation BetweenAdjacent Liners

0.08 mm (0.0031 inch)

Maximum VariationBetween All 6 Liners 0.100 mm (0.0040 inch)

9. If a liner does not meet the recommended cylinderliner projection specification, check the followingparts:

• The depth of the cylinder block bore should be100.00 ± 0.03 mm (3.937 ± 0.001 inch).

• The liner flange should be 100.12 ± 0.03 mm(3.942 ± 0.001 inch).

If the dimensions for the liner flange do notmatch the specifications, replace the liner. Thenrepeat the liner projection measurements. If thedimensions for the depth of the cylinder blockbore do not match the specifications, replace thecylinder block. Then repeat the liner projectionmeasurements.



i02801049

Flywheel - Inspect

Face Runout (Axial Eccentricity) ofthe FlywheelTable 19

Required Tools


21825617 Dial Gauge 1A

- Holder 1


1. Install Tooling (A). Refer to illustration 39. Alwaysput a force on the crankshaft in the same directionbefore the dial indicator is read. This will removeany crankshaft end clearance.

2. Set the dial indicator to read 0.0 mm (0.00 inch).

3. Turn the flywheel at intervals of 45 degrees andread the dial indicator.

4. Take the measurements at all four points. Thedifference between the lower measurements andthe higher measurements that are performed atall four points must not be more than 0.15 mm(0.006 inch), which is the maximum permissibleface runout (axial eccentricity) of the flywheel.

Bore Runout (Radial Eccentricity)of the FlywheelTable 20

Required Tools



- Magnetic Base 1


1. Install Tooling (A). Refer to illustration 40.

2. Set the dial indicator to read 0.0 mm (0.00 inch).

3. Turn the flywheel at intervals of 45 degrees andread the dial indicator.

4. Take the measurements at all four points. Thedifference between the lower measurements andthe higher measurements that are performed atall four points must not be more than 0.15 mm(0.006 inch) for the maximum permissible facerunout (radial eccentricity) of the flywheel.



g00286058Illustration 41Flywheel clutch pilot bearing bore

5. To find the runout (eccentricity) of the pilot bearingbore, use the preceding procedure.

6. The runout (eccentricity) of the bore for the pilotbearing in the flywheel must not exceed 0.13 mm(0.005 inch).

i02801085

Flywheel Housing - Inspect

Table 21

Required Tools



- Holder

Face Runout (Axial Eccentricity) ofthe Flywheel Housing


Typical example

If you use any other method except the method thatis given here, always remember that the bearingclearance must be removed in order to receive thecorrect measurements.

1. Install Tooling (A) to the flywheel so the anvil of thedial indicator will contact the face of the flywheelhousing. Refer to illustration 42.

2. Use a rubber mallet and tap the crankshaft towardthe rear before the dial indicator is read at eachpoint.

g00285932Illustration 43Checking face runout of the flywheel housing

3. Turn the flywheel while the dial indicator is set at0.0 mm (0.00 inch) at location (A). Read the dialindicator at locations (B), (C) and (D).

4. The difference between the lower measurementsand the higher measurements that are performedat all four points must not be more than 0.38 mm(0.015 inch), which is the maximum permissibleface runout (axial eccentricity) of the flywheelhousing.

Bore Runout (Radial Eccentricity)of the Flywheel Housing


Typical example



1. Install Tooling (A) to the flywheel so the anvil of thedial indicator will contact the bore of the flywheelhousing. Refer to illustration 44.

g00285932Illustration 45Checking bore runout of the flywheel housing


2. While the dial indicator is in the position at location(C) adjust the dial indicator to 0.0 mm (0.00 inch).Push the crankshaft upward against the top ofthe bearing. Refer to Illustration 46. Write themeasurement for bearing clearance on line 1 incolumn (C).

Note: Write the measurements for the dial indicatorwith the correct notations. This notation is necessaryfor making the calculations in the chart correctly.

3. Divide the measurement from Step 2 by two. Writethis number on line 1 in columns (B) and (D).

4. Turn the flywheel in order to put the dial indicatorat position (A). Adjust the dial indicator to 0.0 mm(0.00 inch).

5. Turn the flywheel counterclockwise in order toput the dial indicator at position (B). Write themeasurements in the chart.

6. Turn the flywheel counterclockwise in order toput the dial indicator at position (C). Write themeasurement in the chart.

7. Turn the flywheel counterclockwise in order toput the dial indicator at position (D). Write themeasurement in the chart.

8. Add the lines together in each column.

9. Subtract the smaller number from the largernumber in column B and column D. Place thisnumber on line III. The result is the horizontaleccentricity (out of round). Line III in column C isthe vertical eccentricity.

g00286046Illustration 47Graph for total eccentricity

(1) Total vertical eccentricity(2) Total horizontal eccentricity(3) Acceptable value(4) Unacceptable value

10. Find the intersection of the eccentricity lines(vertical and horizontal) in Illustration 47.

11. If the point of the intersection is in the “Acceptable”range, the bore is in alignment. If the point ofintersection is in the “Not acceptable” range, theflywheel housing must be changed.



i02801086

Vibration Damper - Check


(1) Vibration damper(2) Crankshaft pulley(1) Spacer for the pulley(4) Bolts

Damage to the vibration damper or failure of thevibration damper will increase vibrations. This willresult in damage to the crankshaft.

Replace the damper if any of the following conditionsexist:

• The damper is dented, cracked, or fluid is leakingfrom the damper.

• The paint on the damper is discolored fromexcessive heat.

• The damper is bent.

• The bolt holes are worn or there is a loose fit forthe bolts.

• The engine has had a crankshaft failure due totorsional forces.

NOTICEInspect the viscous vibration damper for signs of leak-ing and for signs of damage to the case. Either ofthese conditions can cause the weight to contact thecase. This contact can affect damper operation.



Electrical Systemi02801089

Battery - Test

Most of the tests of the electrical system can be doneon the engine. The wiring insulation must be in goodcondition. The wire and cable connections must beclean, and both components must be tight.

Never disconnect any charging unit circuit or bat-tery circuit cable from the battery when the charg-ing unit is operated. A spark can cause an explo-sion from the flammable vapor mixture of hydro-gen and oxygen that is released from the elec-trolyte through the battery outlets. Injury to per-sonnel can be the result.

The battery circuit is an electrical load on the chargingunit. The load is variable because of the condition ofthe charge in the battery.

NOTICEThe charging unit will be damaged if the connectionsbetween the battery and the charging unit are brokenwhile the battery is being charged. Damage occursbecause the load from the battery is lost and becausethere is an increase in charging voltage. High voltagewill damage the charging unit, the regulator, and otherelectrical components.

i02813962

Charging System - Test

Note: This procedure is only applicable if a chargingsystem is installed.

The condition of charge in the battery at each regularinspection will indicate whether the charging systemoperates correctly. An adjustment is necessary whenthe battery is constantly in a low condition of chargeor a large amount of water is needed.

Test the charging unit and the voltage regulator onthe engine. Use wiring and components that are apermanent part of the system. This testing will give anindication of needed repair. After repairs are made,perform a test in order to prove that the units havebeen repaired to the original condition of operation.

To check for correct output of the alternator, refer toSpecifications.

Before the start of on-engine testing, the chargingsystem and the battery must be checked accordingto the following steps.

1. The battery must be at least 75 percent (1.225 SpGr) of the full charge. The battery must be heldtightly in place. The battery holder must not puttoo much stress on the battery.

2. Cables between the battery, the starter, and theengine ground must be the correct size. Wiresand cables must be free of corrosion. Wires andcables must have cable support clamps in order toprevent stress on battery connections (terminals).

3. Leads, junctions, switches, and panel instrumentsthat have direct relation to the charging circuitprovide correct circuit control.

4. Inspect the drive components for the charging unitin order to be sure that the components are free ofgrease and oil. Be sure that the drive componentshave the ability to operate the charging unit.

i02801092

Electric Starting System - Test

Most of the tests of the electrical system can bedone on the engine. The wiring insulation must bein good condition. The wire and cable connectionsmust be clean, and both components must be tight.The battery must be fully charged. If the on-enginetest shows a defect in a component, remove thecomponent for more testing.

The starting system consists of the following fourcomponents:

• Keyswitch

• Start relay

• Starting motor solenoid

• Starting motor

Trouble with the starting system could be causedby the battery or by charging system problems. Ifthe battery is suspect, refer to Troubleshooting,“Battery”. If the starting system is suspect, refer toTroubleshooting, “Engine Will Not Crank”.


KENR6907 55Index Section

Index

A

Air in Fuel - Test..................................................... 24Air Inlet and Exhaust System .......................... 12, 31Turbocharger ..................................................... 13Valve System Components................................ 13

Air Inlet and Exhaust System - Inspect.................. 31Air Inlet Restriction............................................. 31

B

Basic Engine.................................................... 18, 47Camshaft............................................................ 19Crankshaft.......................................................... 18Cylinder Block .................................................... 18Pistons, Rings, and Connecting Rods ............... 18Vibration Damper ............................................... 19

Battery - Test ......................................................... 54Belt Tension Chart ................................................. 23

C

Charging System - Test ......................................... 54Connecting Rod Bearings - Inspect....................... 47Cooling System ............................................... 15, 41Coolant Flow...................................................... 15Supply Manifold ................................................. 17Temperature Regulator Housing ........................ 17

Cooling System - Check (Overheating) ................. 41Cooling System - Inspect....................................... 42Cooling System - Test............................................ 43Checking the Filler Cap...................................... 44Test For The Water Temperature Gauge ........... 45Testing The Radiator And Cooling System ForLeaks................................................................ 44

Cylinder Block - Inspect......................................... 47Cylinder Liner Projection - Inspect......................... 48

E

Electric Starting System - Test............................... 54Electrical System............................................. 19, 54Charging System Components .......................... 20Engine Electrical System ................................... 20Grounding Practices .......................................... 19Starting System Components ............................ 21

Electronic Control System Components.................. 6Electronic Unit Injector - Adjust ............................. 25Electronic Unit Injector - Test................................. 26Engine Crankcase Pressure (Blowby) - Test ......... 34Engine Oil Pressure - Test..................................... 37Measuring Engine Oil Pressure ......................... 37Reason for High Engine Oil Pressure ................ 39Reasons for Low Engine Oil Pressure ............... 38

Engine Valve Lash - Inspect/Adjust ....................... 35Valve Lash Adjustment ...................................... 35Valve Lash Check .............................................. 35

Excessive Bearing Wear - Inspect......................... 39Excessive Engine Oil Consumption - Inspect........ 39Engine Oil Leaks into the Combustion Area of theCylinders .......................................................... 39Engine Oil Leaks on the Outside of the Engine.. 39

Exhaust Temperature - Test................................... 34

F

Finding Top Center Position for No. 1 Piston......... 26Flywheel - Inspect.................................................. 50Bore Runout (Radial Eccentricity) of theFlywheel ........................................................... 50Face Runout (Axial Eccentricity) of theFlywheel ........................................................... 50

Flywheel Housing - Inspect ................................... 51Bore Runout (Radial Eccentricity) of the FlywheelHousing............................................................ 51Face Runout (Axial Eccentricity) of the FlywheelHousing............................................................ 51

Fuel Quality - Test.................................................. 27Fuel System....................................................... 8, 24Electronic Unit Injector ........................................ 11Electronic Unit Injector Mechanism.................... 10Fuel System Electronic Control Circuit ................ 9

Fuel System - Inspect............................................ 24Fuel System - Prime.............................................. 28Fuel System Pressure - Test ................................. 29Checking Fuel Pressure..................................... 29Fuel Pressure Readings .................................... 29High Fuel Pressure ............................................ 29Low Fuel Pressure ............................................. 29

G

Gear Group (Front) - Time..................................... 30General Information................................................. 4Cold Mode Operation........................................... 5Starting the Engine .............................................. 5

I

Important Safety Information ................................... 2Increased Engine Oil Temperature - Inspect ......... 40

L

Lubrication System.......................................... 14, 37

M

Main Bearings - Inspect......................................... 47


P

Piston Ring Groove - Inspect................................. 47Inspect the Clearance of the Piston Ring........... 47Inspect the Piston and the Piston Rings ............ 47Inspect the Piston Ring End Gap....................... 47

S

Systems Operation Section ..................................... 4

T

Table of Contents..................................................... 3Testing and Adjusting ............................................ 23Testing and Adjusting Section ............................... 23Turbocharger - Inspect .......................................... 32Inspection of the Compressor and the CompressorHousing............................................................ 33Inspection of the Turbine Wheel and the TurbineHousing............................................................ 33

V

Vibration Damper - Check ..................................... 53

W

Water Pump - Test................................................. 46Water Temperature Regulator - Test ..................... 45

©2008 Perkins Engines Company LimitedAll Rights Reserved Printed in U. K.This document has been printed from SPI². Not for Resale

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