COPERTINA FUIF511 27D Repair Manual N45 And N67 ENT Tier3 P2D32N003E Feb06

User Manual: FUIF511-27D

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NEF TIER 3 SERIES
Industrial application
N45
N45 ENT
N67
N67 ENT
Technical and Repair manual
Publication edited by
Iveco Motors
Iveco SpA
PowerTrain
Mkt. Advertising & Promotion
Viale dell’Industria, 15/17
20010 Pregnana Milanese
Milano (Italy)
Print P2D32N003GB -1
st Ed. 02.2006
This publication describes the characteristics, data and correct
methods for repair operations on each component of the ve-
hicle.
If the instructions provided are followed and the specified
equipment is used, correct repair operations in the pro-
grammed time will be ensured, safeguarding against possible
accidents.
Before starting to perform whatever type of repair, ensure that
all accident prevention equipment is available and efficient.
All protections specified by safety regulations, i.e.: goggles,
helmet, gloves, boot, etc. must be checked and worn.
All machining, lifting and conveying equipment should be in-
spected before use.
The data contained in this publication was correct at the time
of going to press but due to possible modifications made by
the Manufacturer for reasons of a technical or commercial na-
ture or for adaptation to the legal requirements of the differ-
ent countries, some changes may have occurred.
No part of this publication, including the pictures, may be re-
produced in any form or by any means.
B.U. TECHNICAL PUBLISHING
Iveco Technical Publications
Lungo Stura Lazio, 15/19
10156 Turin - Italy
Produced by:
Manuals for repairs are split into Parts and Sections, each one of which is marked by a numeral; the contents of these sections are
indicated in the general table of contents.
The sections dealing with things mechanic introduce the specifications, tightening torque values, tool lists, assembly
detaching/reattaching operations, bench overhauling operations, diagnosis procedures and maintenance schedules.
The sections (or parts) of the electric/electronic system include the descriptions of the electric network and the assembly’s
electronic systems, wiring diagrams, electric features of components, component coding and the diagnosis procedures for the
control units peculiar to the electric system.
The manual uses proper symbols in its descriptions; the purpose of these symbols is to classify contained information. In particular,
there have been defined a set of symbols to classify warnings and a set for assistance operations.
PRELIMINARY REMARKS
General danger
It includes the dangers of above described signals.
Danger of serious damage for the assembly
Failure to comply, both fully or in part, with such prescriptions will involve serious damage to the assembly and may
sometimes cause the warranty to become null and void.
Environment protection
Moreover, it describes the correct actions to be taken to ensure that the assembly is used in such a way so as to protect
the environment as much as possible.
Danger for persons
Missing or incomplete observance of these prescriptions can cause serious danger for persons’ safety.
SYMBOLS - WARNINGS
It indicates an additional explanation for a piece of information.
!
NOTE
3
NEF TIER 3 ENGINES
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GENERAL WARNINGS
Warnings shown cannot be representative of all danger situations possibly occurring. Therefore, it is suggested to contact
immediate superiors where a danger situation occurs which is not described.
Use both specific and general-purpose toolings according to the prescriptions contained in respective use and
maintenance handbooks. Check use state and suitability of tools not subjected to regular check.
The manual handling of loads must be assessed in advance because it also depends, besidesweight,onitssizeandon
the path.
Handling by mechanical means must be with hoisters proper as for weight as well as for shape and volume. Hoisters,
ropes and hooks used must contain clear indications on maximum carrying capacity acceptable. The use of said means
is compulsorily permitted to authorised personnel only. Stay duly clear of the load, and, anyhow, never under it.
In disassembling operations, always observe provided prescriptions; prevent mechanical parts being taken out from
accidentally striking workshop personnel.
Workshop jobs performed in pairs must always be performed in maximum safety; avoid operations which could be
dangerous for the co-operator because of lack of visibility or of his/her not correct position.
Keep personnel not authorised to operations clear of working area.
You shall get familiar with the operating and safety instructions for the assembly prior to operating on the latter. Strictly
follow all the safety indications found on the assembly.
Do not leave the running assembly unattended when making repairs.
When carrying out work on the assembly lifted off the ground, verify that the assembly is firmly placed on its supporting
stands, and that the manual/automatic safety devices have been actuated in the event that the assembly is to be lifted
by means of a hoist.
When you have to operate on assemblies powered by natural gas, follow the instructions contained in the document,
as well as all the specific safety standards provided for.
Only remove radiator cap when the engine is cold by cautiously unscrewing it in order to let system residual pressure
out.
Inflammable fuel and all inflammable fluids and liquids must be handled with care, according to what contained on harmful
materials 12-point cards. Refuelling must be performed outdoors with the engine off, avoiding lit cigarettes, free flames
or sparks in order to prevent sudden fires/bursts. Adequately store inflammable, corrosive and polluting fluids and liquids
according to what provided by regulations in force. Compulsorily avoid to use food containers to store harmful liquids.
Avoid to drill or bore pressurised containers, and throw cloths impregnated with inflammable substances into suitable
containers.
Worn out, damaged or consumable parts must be replaced by IVECO Motors original spares.
During workshop activity, always keep the work place clean; timely clear or clean floors from accidental liquid or oil spots.
Electric sockets and electric equipment necessary to perform repair interventions must meet safety rules.
!
4NEF TIER 3 ENGINES
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GENERAL
W
ARNINGS
Clean the assemblies and carefully verify that they are intact prior to overhauling. Tidy up detached or disassembled
parts with their securing elements (screws, nuts, etc.) into special containers.
Check for the integrity of the parts which prevent screws from being unscrewed: broken washers, dowels, clips, etc.
Self-locking nuts with an insert made of nylon must always be replaced.
Avoid contact of rubber parts with diesel oil, petrol or other not compatible substances.
Before washing under pressure mechanical parts, protect electric connectors, and central units, if present.
Tightening screws and nuts must always be according to prescriptions; IVECO Motors commercial and assistance
network is available to give all clarifications necessary to perform repair interventions not provided in this document.
Before welding:
-Disconnect all electronic central units, take power cable off battery positive terminal (connect it to chassis bonding)
and detach connectors.
-Remove paint by using proper solvents or paint removers and clean relevant surfices with soap and water.
-Await about 15 minutes before welding.
-Equip with suitable fire resistant protections to protect hoses or other components where fluids or other materials
flow which may catch fire easily on welding.
Should the vehicle be subjected to temperatures exceeding 80°C (dryer ovens), disassemble drive electronic central
units.
The disposal of all liquids and fluids must be performed with full observance of specific rules in force.
Put on, where required by the intervention, garments and protections provided in accident prevention rules; contact
with moving parts can cause serious injuries. Use suitable, preferably tight-fitted garments, and avoid to use jewels,
scarves, etc.
Do not leave the engine in motion at workshop locations not provided with a pipe to scavenge exhaust gas outside.
Avoid to breathe fumes coming from heating or from paint welding because they can cause damages to health; operate
outdoors or in suitably ventilated areas. Put on proper inspirator if paint powder is present.
Avoid contact with hot water or steam coming from the engine, radiator and pipings because they could cause serious
burns. Avoid direct contact with liquids and fluids present in vehicle systems; where an accidental contact has occurred,
refer to 12-point cards for provisions to make.
5
NEF TIER 3 ENGINES
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GENERAL
W
ARNINGS ON THE ELECTRIC S
Y
STEM
To start up the engine, do not use fast chargers. Start up must only be performed with either separate batteries or special
truck.
A wrong polarisation of supply voltage in drive electronic central units (for instance, a wrong polarisation of batteries)
can cause them to be destroyed.
Disconnect the batteries from the system during their recharging with an external apparatus.
On connecting, only screw up connector (temperature sensors, pressure sensors etc.) nuts at prescribed tightening
torque.
Before disconnecting the junction connector from an electronic central unit, isolate the system.
Do not directly supply electronic central units servo components at nominal vehicle voltage.
Cables must be arranged such as to result to be parallel to reference plane, i.e. as close as possible to chassis/body
structure.
Once the intervention on the electric system has been completed, recover connectors and wiring harnesses according
to original arrangement.
Ifaninterventionhastobemadeontheelectric/electronicsystem, disconnect batteries from the system; in this case,
always disconnect, as a first one, the chassis bonding cable from batteries negative terminal.
Before connecting the batteries to the system, make sure that the system is well isolated.
Disconnect the external recharging apparatus from the public utility network before taking apparatus pins off battery
terminals.
Do not cause sparks to be generated in checking if the circuit is energised.
Do not use a test lamp in checking circuit continuity, but only use proper control apparatuses.
Make sure that the electronic devices wiring harnesses (length, lead type, location, strapping, connection to screening
braiding, bonding, etc.) comply with IVECO Motors system and are carefully recovered after repair or maintenance
interventions.
Measurements in drive electronic central units, plugged connections and electric connections to components can only
be made on proper testing lines with special plugs and plug bushes. Never use improper means like wires, screwdrivers,
clips and the like in order to avoid the danger of causing a short circuit, as well as of damaging plugged connections, which
would later cause contact problems.
Connectors present must be seen from cable side. Connectors views contained in the manual are representative of cable
side.
!
NOTE
6NEF TIER 3 ENGINES
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7
NEF TIER 3 ENGINES
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Bonding and screening
Negative leads connected to a system bonded point must be both as short and possible and “star“-connected to each other, trying
then to have their centering tidily and properly made (Figure 1, re. M).
Further, following warnings are to be compulsorily observed for electronic components:
- Electronic central units must be connected to system bonding when they are provided with a metallic shell.
- Electronic central units negative cables must be connected both to a system bonding point such as the dashboard opening
bonding (avoiding “serial“ or “chain“ connections), and to battery negative terminal.
- Analog bonding (sensors), although not connected to battery negative system/terminal bonding, must have optimal isolation.
Consequently, particularly considered must be parasitic resistances in lugs: oxidising, clinching defects, etc.
- Screened circuits braiding must only electrically contact the end towards the central unit entered by the signal (Figure 2).
- If junction connectors are present, unscreened section d, near them, must be as short as possible (Figure 2).
- Cables must be arranged such as to result to be parallel to reference plane, i.e. as close as possible to chassis/body structure.
1. NEGATIVE CABLES STARCONNECTION TO SYSTEM BONDING M
2. SCREENING THROUGH METALLIC BRAIDING OF A CABLE TO AN ELECTRONIC COMPONENT — C. CONNECTOR
d. DISTANCE !0
88039
Figure 1
Figure 2
8NEF TIER 3 ENGINES
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OPTIONAL ELECTRICAL AND MECHANICAL PARTS INSTALLATIONS
Assemblies shall be modified and equipped with additions - and their accessories shall be fitted - in accordance with the assembling
directives issued by IVECO Motors.
It is reminded that, especially about the electric system, several electric sockets are provided for as series (or optional) sockets in
order to simplify and normalise the electrical intervention that is care of preparation personnel.
It is absolutely forbidden to make modifications or connections to electric central units wiring harnesses; in particular,
the data interconnection line between central units (CAN line) is to be considered inviolable.
CONVERSIONS BETWEEN THE MAIN UNITS OF MEASUREMENT OF THE
INTERNATIONAL SYSTEM AND MOST USED DERIVED QUANTITIES
Power
1 kW = 1.36 metric HP
1 kW = 1.34 HP
1 metric HP = 0.736 kW
1 metric HP = 0.986 HP
1 HP = 0.746 kW
1 HP = 1.014 metric HP
Torque
1 Nm = 0.1019 kgm
1 kgm = 9.81 Nm
Revolutions per time unit
1 rad/s = 1 rpm x 0.1046
1 rpm = 1 rad/s x 9.5602
Pressure
1bar = 1.02kg/cm
2
1 kg/cm2= 0.981 bar
1 bar = 105Pa
Where accuracy is not particularly needed:
-Nm unit is for the sake of simplicity converted into kgm according to ratio 10:1
1 kgm = 10 Nm;
-bar unit is for the sake of simplicity converted into kg/cm2according to ratio 1:1
1 kg/cm2=1bar.
Temperature
0°C=32°F
1°C = (1 x 1.8 + 32) °F
F4HE engines Part 1
G-Drive Application Engines Part 2
NEF TIER 3 ENGINES
NEF TIER 3 ENGINES 1
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2NEF TIER 3 ENGINES
Base - February 2006 Print P2D32N00GB
Sezione
General specifications 1
Fuel 2
Duty - Industrial application 3
Overhaul and technical specifications 4
Tools 5
Safety prescriptions Appendix
PREFACE TO USER’S GUIDELINE MANUAL
Section 1 describes the NEF engine illustrating its features
and working in general.
Section 2 describes the type of fuel feed.
Section 3 relates to the specific duty and is divided in four sepa-
rate parts:
1. Mechanical part, related to the engine overhaul,
limited to those components with different characteristics
based on the relating specific duty.
2. Electrical part, concerning wiring harness, electrical
and electronic equipment with different characteristics
based on the relating specific duty.
3. Maintenance planning and specific overhaul.
4. Troubleshooting part dedicated to the operators who,
being entitled to provide technical assistance, shall have simple
and direct instructions to identify the cause of the major incon-
veniences.
Sections 4 and 5 illustrate the overhaul operations of the engi-
ne overhaul on stand and the necessary equipment to execute
such operations.
Part 1
F4HE NEF ENGINES
1
F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
2F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Diagrams and symbols have been widely used to give a clearer and more immediate illustration of the subject being dealt with, (see
next page) instead of giving descriptions of some operations or procedures.
Example
Ø 1 = housing for connecting rod small end bush
Ø 2 = housing for connecting rod bearings
α
Tighten to torque
Tighten to torque + angular value
1
2
3
F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
SPECIAL REMARKS
4F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
SYMBOLS - ASSISTANCE OPERATIONS
Removal
Disconnection Intake
Refitting
Connection Exhaust
Removal
Disassembly Operation
Fitting in place
Assembly ρCompression ratio
Tighten to torque Tolerance
Weight difference
α
Tighten to torque + angle value Rolling torque
Press or caulk Rotation
Regulation
Adjustment
Angle
Angular value
Visual inspection
Fitting position check Preload
Measurement
Value to find
Check
Number of revolutions
Equipment Temperature
Surface for machining
Machine finish bar Pressure
Interference
Strained assembly
Oversized
Higher than.
Maximum, peak
Thickness
Clearance
Undersized
Less than.
Minimum
Lubrication
Damp
Grease
Selection
Classes
Oversizing
Sealant
Adhesive
Temperature < 0 °C
Cold
Winter
Air bleeding
Temperature > 0 °C
Hot
Summer
Replacement
Original spare parts
5
F4HE NEF ENGINES
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UPDATING
Section Description Page Date of revision
6F4HE NEF ENGINES
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SECTION 1 - GENERAL SPECIFICATIONS 1
F4AE NEF ENGINES
Print P2D32N003GB Base - February 2006
SECTION 1
General specifications
Page
CORRESPONDENCE BETWEEN TECHNICAL CODE
AND COMMERCIAL CODE 3.............
LUBRICATION 5..........................
-4-cylinder engine version 5.................
-6-cylinder engine version 6.................
OIL VAPOUR RECYCLING 7................
COOLING SYSTEM 8......................
-4-cylinder engine version 8.................
-6-cylinder engine version 9.................
AIR INDUCTION - BOOST DIAGRAM 10.......
-Description 10............................
2SECTION 1 - GENERAL SPECIFICATIONS F4AE NEF ENGINES
Base - February 2006 Print P2D32N00GB
CORRESPONDENCE BETWEEN TECHNICAL CODE AND COMMERCIAL CODE
SECTION 1 - GENERAL SPECIFICATIONS 3
F4AE NEF ENGINES
Print P2D32N003GB Base - February 2006
Technical Code Commercial Code
F4HE9484A*J101 N45 ENT
F4HE9684P*J101 N67 ENT
4SECTION 1 - GENERAL SPECIFICATIONS F4AE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 1
LUBRICATION
Lubrication by forced circulation is achieved through oil rotary
expansion pump (1), placed in the front part of the basement,
driven by the straight-tooth gear splined to the shaft’s bar hold.
From the pan, the lubrication oil flows to the driving shaft, to
the camshaft and to the valve drive.
Lubrication involves the heat exchanger as well, the turbo-
blower and the eventual compressor for any eventual com-
pressed air system. All these components may often vary ac-
cording to the specific duty and will therefore be examined in
the specific section.
Oil recover from the
turbo-blower
To the exchanger
and to the
turbo-blower
LUBRICATION SYSTEM LAYOUT
4-cylinder engines
Routing of oil return by gravity to sump
Routing of oil return by gravity to sump
Introduction of oil
(Demonstration)
4-cylinder engine version
108511
SECTION 1 - GENERAL SPECIFICATIONS 5
F4AE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 2
LUBRICATION SYSTEM LAYOUT
6-cylinder engines
Routing of oil under pressure
Routing of oil return by gravity to sump
Introduction of oil
6-cylinder engine version
Even for the 6 cylinders version lubrication is obtained by
forced circulation and achieved through an oil rotary expan-
sion pump similar to the 4 cylinders’ one.
Also in this case, the components such as the oil exchanger,
the turbo-blower and the eventual compressor are specifically
studied and made out to suit the equipment or the duty for
which the engine has been developed.
Oil recover from the
turbo-blower
To the
exchanger and
to the
turbo-blower
(Demonstration)
108512
6SECTION 1 - GENERAL SPECIFICATIONS F4AE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70484
Figure 3
1. Pre-separator - 2. Exhaust to the outside (temporary) - 3. Filter - 4. Return to engine.
The tappet cover houses the pre-separator (1), whose shape and position determines an increase in oil vapour outlet speed and
condenses a part of vapours at the same time.
Condensate oil returns to the oil sump whereas the residual vapours are ducted, collected and filtered in the blow-by (3).
In the blow-by (3), part of the vapours condense and return to the oil sump whereas the remaining part is put into cycle again
through pipe (2).
Oil condensate
Oil vapours
OIL VAPOUR RECYCLING
SECTION 1 - GENERAL SPECIFICATIONS 7
F4AE NEF ENGINES
Print P2D32N003GB Base - February 2006
COOLING SYSTEM
The engine cooling system, closed circuit forced circulation
type, generally incorporates the following components:
-Expansion tank; placement, shape and dimensions are
subject to change according to the engine’s equipment.
-Radiator, which has the duty to dissipate the heat
subtracted to the engine by the cooling liquid. Also this
component will have specific peculiarities based on the
equipment developed, both for what concerns the
placement and the dimensions.
-Viscous pusher fan, having the duty to increase the heat
dissipating power of the radiator. This component as well
will be specifically equipped based on the engine’s
development.
-Heat exchanger to cool the lubrication oil: even this
component is part of the engine’s specific equipment.
-Centrifugal water pump, placed in the front part of the
engine block.
-Thermostat regulating the circulation of the cooling liquid.
-The circuit may eventually be extended to the
compressor,ifthisisincludedintheequipment.
Figure 4 (Demonstration)
4-cylinder engine version
74194
Expansion tank
Heater
(optional)
Expansion tank
Radiator
Radiator
Water coming out from thermostat
Water recirculating in engine
Water coming into pump
COOLING SYSTEM LAYOUT
4-cylinder engines
8SECTION 1 - GENERAL SPECIFICATIONS F4AE NEF ENGINES
Base - February 2006 Print P2D32N00GB
6-cylinder engine version
The engine cooling system, closed circuit forced circulation
type, is of a similar design as the 4 cylinders engine.
It incorporates necessary components such as the radiator,
the heat exchanger, the expansion tank and some ancillary
components such as the heater or the compressor for the
compressed air.
Such components always vary according to the engine’s equip-
ment and duty.
Figure 5 (Demonstration)
COOLING SYSTEM LAYOUT
6-cylinder engines
108513
Expansion
tank
Heater
(optional)
Expansion tank
Radiator
Radiator
Water coming out from thermostat
Water recirculating in engine
Water coming into pump
SECTION 1 - GENERAL SPECIFICATIONS 9
F4AE NEF ENGINES
Print P2D32N003GB Base - February 2006
74195
Figure 6
AIR INDUCTION - BOOST DIAGRAM
Description
The turbocharger is composed by the following main parts:
one turbine, one transforming valve to regulate the boost
feeding pressure , one main body and one compressor.
During engine working process, the exhaust emissions flow
through the body of the turbine, causing the turbine disk
wheel’s rotation.
The compressor rotor, being connected by shaft to the
turbine disk wheel, rotates as long as this last one rotates,
compressing the drawn air through the air filter.
The above mentioned air is then cooled by the radiator and
flown through the piston induction collector.
The turbocharger is equipped with a transforming valve to
regulate the pressure , that is located on the exhaust collector
before the turbine and connected by piping to the induction
collector.
It’s funchon is to restrict the exhaust of the emissions , releasing
part of them directly to the exhaust tube when the boost
feeding pressure, over the compressor, reaches the
prescribed bar value.
The cooling process and the lubrication of the turbocharger
and of the bearings is made by the oil of the engine.
RADIATOR
AIR FILTRE TURBOCHARGER
EXHAUST
4 Cylinders version
6 Cylinders version
RADIATOR
AIR FILTRE TURBOCHARGER
EXHAUST
10 SECTION 1 - GENERAL SPECIFICATIONS F4AE NEF ENGINES
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SECTION 2 - FUEL 1
F4HE NEF ENGINES
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SECTION 2
Fuel
Page
HIGH PRESSURE ELECTRONIC INJECTION
SYSTEM (COMMON RAIL) 3..............
EDC 7 OPERATION 4......................
WORKING PROCESS 5.....................
FUEL SYSTEM LAYOUT 6...................
MECHANICAL FEEDING PUMP 7............
CP3 HIGH PRESSURE PUMP 8...............
RAIL 12...................................
BOOST GAUGE VALVE 13...................
ELECTRO-INJECTOR 14.....................
-Electro-injector 15.........................
PRESSURE LIMITER FOR FUEL RETURN 16......
2SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 1
1. Connection to Electro-injectors - 2. Sensor monitoring temperature of engine’s cooling liquid - 3. Fuel pressure sensor
cable - 4. Sensor of engine’s oil temperature and pressure -
5. Driving shaft sensor - 6. Electro-injector - 7. Temperature and air pressure sensor -
8. Camshaft sensor - 9. Fuel heater cable and fuel temperature sensor -
10. Pressure gauge cabling - 11. EDC 7 gearbox.
HIGH PRESSURE ELECTRONIC INJECTION
SYSTEM (COMMON RAIL)
Introduction
Extremely high injection pressures are necessary in order to
reduce PARTICULATE emissions.
The common rail system makes it possible to inject fuel at
pressures of up to 1450 - 1600 bar, while the injection preci-
sion obtained by electronic control of the system serves to
optimise operation of the engine while limiting emissions and
fuel consumption.
For engines more powerful than 152 kW, the CRIN2 injec-
tors have DLLA nozzles that work up to a pressure of 1600
bar, whilst for engines less powerful than 152 kW, DSLA
nozzles are fitted which work a pressures up to 1450 bar.
Description of system
The injection system is composed of an electrical part and a
hydraulic part.
Electrical system
The electronic control unit monitors engine control para-
meters by means of the various sensors on the engine.
107851
SECTION 2 - FUEL 3
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
EDC 7 OPERATION
Engine preheating element control
Pre-post heating is activated when even just one of the water,
air or fuel temperature sensors detects a temperature 5°C.
Phase recognition
By means of signals transmitted by the camshaft and
crankshaft sensors, the cylinder into which fuel must be
injected is determined at the time of starting.
Injection control
On the basis of information transmitted by the sensors, the
control unit administrates the pressure regulator and
modifies the pre-injection and main injection mode.
On F4 engines pre-injection is activated at all engine speeds.
Injection pressure closed loop control
On the basis of the engine load, as determined by processing
of data transmitted by the various sensors, the control unit
administrates the regulator to maintain injection pressure at
constantly optimal values.
Pilot and main injection advance control
On the basis of signals transmitted by the various sensors, the
control unit determines the optimum injection point on the
basis of internal mapping.
Idle speed control
The control unit processes signals transmitted by the various
sensors and adjusts the quantity of fuel injected.
It also controls the pressure regulator and modulates
injection duration of the electro-injectors.
Within specific limits, the control unit also monitors battery
voltage.
Overheating protection
If the water temperature reaches 110 °C, the control unit
reduces engine performance.
When the temperature returns below 100 °C, the engine
resumes normal operation, (in some applications, the over
boosting temperature is the reference temperature).
Maximum engine speed limiting
Depending on the application, the control unit memory can
contain appropriate engine speed limits. When the engine
speed surpasses these limits the control unit activates power
reduction strategies by controlling energization time of the
electro-injectors. In some applications the maximum limiting
response consists in stopping the engine.
Cut Off
Fuel cut-off in release phases is managed by the control unit
with the following logical interventions:
-disactivation of the electro-injectors;
-reactivation of electro-injectors immediately prior to
arrival at idle speed;
-control of fuel pressure regulator.
Smoke control under acceleration
With intense load demands, in accordance with signals
received from the air inlet meter and the engine speed
sensor, the control unit manages the pressure regulator and
modulates the activation time of the electro-injectors to
prevent the emission of smoke from the exhaust.
After Run
After the engine is stopped, the control unit microprocessor
saves various parameters to the EEPROM memory, including
the faults log so that they will be available the next time the
engine is started.
Control of working speed in normal operating
conditions
Each time work load varies, the control unit adjusts torque
so as to maintain the engine in maximum power conditions.
If the load causes a reduction in power, the control unit
increases torque i.e. it increases the amount of fuel injected
in order to restore the engine to maximum power.
Recovery strategies
Recovery strategies are characterized by certain differences
as application varies, i.e.
-Control of fuel leaks
In the case of fuel supply problems, the system controls
the engine with suitable constant power values obtained
with a low number of revs and high torque values in
order to inject the maximum quantity of fuel.
-Control of pressure in the rail
When the pressure in the rail exceeds safety values, the
engine reduces power.
-Synchronism problems
In the case of synchronism problems, faulty rev sensors,
the system controls the engine by increasing the number
of revs in order to improve interpretation of the signals.
-Power restrictions as operating temperature increases
When the temperature of the supercharging air rises
above 88 °C, power reduction is started; when a
temperature of 120 °C is reached, performance is
further reduced and is comparable to that of the same
engine if it were aspirated.
-Reduction of power as reference temperature varies
In normal operating conditions, the system knows the
supercharging air, oil and water temperatures.
If the temperature of the engine water is not available,
the system takes the temperature of the oil as reference
and when this reaches the threshold of 103 °C, it starts
to reduce the power available. On reaching 113 °C,
power is reduced to 50%.
4SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 2
1. Electro-injector - 2. Common Rail - 3. Pressure limiting device for fuel return -
4. Common rail pressure relief valve - 5. Pre-filter mounted on the frame - 6. High-pressure pump -
7. Mechanical vane pump - 8. Fuel filter.
The Common Rail system has a special pump that continuously keeps fuel at high pressure, independently from stroke and
cylinder that has to receive the injection and accumulates fuel in a common duct for all injectors.
Therefore, fuel at the injection pressure computed by the ECU is always available at the injectors inlet.
When an injector solenoid valve is energised by the electronic control unit, the injection of fuel directly taken from rail takes
place in the related cylinder.
The hydraulic system is implemented by a low-pressure circuit and a high-pressure circuit.
The high-pressure circuit is composed of the following pipings:
-piping connecting high-pressure pump outlet to rail;
-pipings supplying injectors from rail.
The low-pressure circuit is composed of the following pipings:
-fuel suction piping from tank to prefilter;
-pipings supplying the mechanical supply pump through the control unit heat exchanger, manual priming pump and prefilter;
-pipings supplying the high-pressure pump through the fuel filter.
The fuel draining circuit from rail and from injectors and the high-pressure pump cooling circuit complete the system.
WORKING PROCESS
High Pressure
Low Pressure
Fuel outlet
108607
SECTION 2 - FUEL 5
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
1. High-pressure pump. — 2. Pressure relief valve on high-pressure pump, 5 bars. — 3. Pressure relief valve assembled on fuel
return from injectors, 1.3 to 2 bars. — 4. Rail overpressure valve.—5.CommonRail.—6.Pressuresensor.—7.Injector.—
8. Return piping. — 9. Control unit heat exchanger. — 10. Mechanical priming pump. — 11. Prefilter assembled on chassis. —
12. Fuel tank. — 13. Mechanical supply pump. — 14. Fuel filter. — 15. Pressure regulator. — 16. High-pressure pump cooling
piping. — 17. By-pass valve. — 18. By-pass valve.
FUEL S
Y
STEM LA
Y
OUT
This fuel system is a Common Rail injection with CP3 high
pressure pump and this layout is for 4 cylinder version.
(The 6 cylinder version is similar design as the 4 cylinder en-
gine).
The pressure regulator, placed upstream of the high-pressure
pump, adjusts the fuel flow that is necessary on the low-pres-
sure system. Afterwards, the high-pressure pump takes care
of supplying the rail properly. This arrangement, by pressuris-
ing the necessary fuel only, improves the energetic efficiency
and limits fuel heating in the system.
Function of the pressure relief valve (2), assembled on the
high-pressure pump, is keeping the pressure, at the pressure
regulator inlet, constant at 5 bars, independently from the
efficiency of the fuel filter and of the system set upstream.
The pressure relie
f
al
e(2)in
t
erven
t
ion brings abou
t
a
f
uel
flow increase in the high-pressure pump cooling circuit,
through inlet and drain piping (16) from piping (8).
The pressure relief valve housed on the cylinder head, as-
sembled on injector return (3), limits the fuel return flow
from injectors at a pressure of 1.3 to 2 bars.
Two by-pass valves are placed in parallel with the mechanical
supply pump.
The by-pass valve (18) allows fuel to flow from mechanical
pump outlet to its inlet, when the fuel filter inlet pressure ex-
ceeds the allowed threshold value.
The by-pass valve (17) allows filling the supply system
through the manual priming pump (10).
108608
Figure 3
EXHAUST
SUCTION
SUPPLY SYSTEM FOR HIGH PRESSURE PUMP
(LOW PRESSURE)
HIGH PRESSURE
6SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
MECHANICAL FEEDING PUMP
Gear pump, placed on rear part of the high pressure pump,
whose function is to feed the high pressure pump. It is driven
by the high pressure pump’s shaft.
Figure 4
72592
A- Fuel entry flowing from the tank. B- Fuel exhaust to filter,
I - 2 By-pass valves in close position.
Overpressure condition in Exhaust unit
Figure 5
72593
The by-pass valve (I) is activated in case of overpressure on
B Exhaust unit. The actual pressure, overcoming the
resistance of the valve’s spring (I), connects the exhaust with
the entry through the gallery (2).
Figure 6
Jettison condition
72594
The dump by-pass valve (2) is activated in case, when the
engine is off, it is necessary to fill the feeding system through
the priming pump. In this condition the by pass valve (I) keeps
closed while the dump by-pass valve (2) opens up due to the
pressure effect on the entry unit so the fuel flows to the
exhaust unit B.
!
The mechanical feeding pump cannot be replaced
separately, therefore it must not be disassembled
from the high pressure pump.
Ordinary working condition
SECTION 2 - FUEL 7
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 7
72595
1. Fuel exhaust connector to rail - 2. High pressure pump - 3. Pressure regulating gauge - 4. Driving gear -
5. Connector to fuel entry flowing from filter - 6. Connector to fuel exhaust to filter support - 7. Connector to fuel entry
flowing from engine control module heat exchanger - 8. Connector to fuel exhaust flowing from mechanic pump to filter -
9. Mechanical feeding pump.
CP3 HIGH PRESSURE PUMP
Pump provided with 3 radial pumping elements driven by the
timing system gear, no need of timing. The mechanical
feeding pump driven by the high pressure pump’s shaft is
assembled to the rear side of the high pressure pump.
!
The high pressure pump unit - feeding pump is not subject to overhaul , therefore it must not be disassembled neither
the fixing screws must be tampered.
The only allowed interventions concern control gear and pressure regulator replacement.
8SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70498
Figure 8
Every pumping unit is composed of:
-a piston (5) actuated by a three-lobe element (2) floating
on the pump shaft (6). The element (2), being floating on
a misaligned part of the shaft (6), when the shaft rotates,
does not rotate therewith but is only translated in a
circular movement along a wider radius, with the
resulting alternate actuation of the three pumping
elements;
1. Cylinder. — 2. Three-lobe element. — 3. Cap intake valve. — 4. Ball delivery valve. — 5. Piston. — 6- Pump shaft. —
7. Low-pressure fuel inlet. — 8. Pumping elements supplying fuel ducts.
Sec. B-B
Sec. C-C
-cap intake valve (3);
-ball delivery valve (4).
High pressure pump-inside structure
SECTION 2 - FUEL 9
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 9
Working principle
72597
1. Cylinder. — 2. Three-lobe element. — 3. Cap intake valve. — 4. Ball delivery valve. — 5. Piston. — 6- Pump shaft. —
7. Low-pressure fuel inlet. — 8. Pumping elements supplying fuel ducts.
Sec. D-D
The pumping element (3) is orientated towards the pump’s
camshaft (4). During the intake phase, the pumping element
is fed through the feeding line (5). The quantity of fuel to flow
to the pumping element is determined by the pressure
regulating gauge (7). The pressure regulating gauge,
according to the PWM command received by the engine
control module, stops the fuel flow to the pumping element.
During compression phase of the pumping element, the fuel
achieves the level of pressure determining the opening of the
by-pass valve to common rail (2), feeding it through the
exhaust unit (I).
Sec. B-B
10 SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 10
72601
1. Cylinder. — 2. Three-lobe element. — 3. Cap intake valve.
— 4. Ball delivery valve. — 5. Piston. — 6- Pump shaft. —
7. Low-pressure fuel inlet. — 8. Pumping elements supplying
fuel ducts.
Sec.C-C 72598
Figure 10 shows the fuel runs at low pressure inside the
pump; the following elements are clearly visible: the main
feeding line to the pumping elements (4); the feeding lines to
the pumping elements (1-3-6), the duct lines run for the
pump lubrication (2), the pressure gauge (5), the flow limiting
valve to 5 bar (8) and the fuel exhaust flue (7).
The pump shaft is lubricated by the fuel through the feeding
and recovery lines.
The pressure gauge (5) determines the quantity of fuel to
feed the pumping elements: the fuel in excess flows through
the exhaust gallery (9).
The limiting valve to 5 bar, in addition to recovering fuel
exhaust as a collector has also function to keep the pressure
constant to 5 bar limit at gauge entry.
Figure 11
Sec. A - A
1. Fuel exhaust flue - 2. Fuel exhaust gallery - 3 Fuel
exhaust flowing from pump with connector to high
pressure pipe for common rail.
Figure 11 shows the fuel flow under high pressure running
through the exhaust galleries of the pumping elements.
SECTION 2 - FUEL 11
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 12
Operation
The cylinder is filled through the cap intake valve only if the
supply pressure is suitable to open the delivery valves set on
the pumping elements (about 2 bars).
The amount of fuel supplying the high-pressure pump is
metered by the pressure regulator, placed on the
low-pressure system; the pressure regulator is controlled by
the EDC7 control unit through a PWM signal.
When fuel is sent to a pumping element, the related piston
is moving downwards (suction stroke). When the piston
stroke is reversed, the intake valve closes and the remaining
fuel in the pumping element chamber, not being able to come
out, is compressed above the supply pressure value existing
in the rail.
The thereby-generated pressure makes the exhaust valve
open and the compressed fuel reaches the high-pressure
circuit.
The pumping element compresses the fuel till the top dead
center (delivery stroke) is reached. Afterwards, the pressure
decreases till the exhaust valve is closed.
The pumping element piston goes back towards the bottom
dead center and the remaining fuel is decompressed.
When the pumping element chamber pressure becomes less
than the supply pressure, the intake valve is again opened and
the cycle is repeated.
The delivery valves must always be free in their movements,
free from impurities and oxidation.
The rail delivery pressure is modulated between 250 and
1600 bars by the electronic control unit, through the
pressure regulator solenoid valve.
The pump is lubricated and cooled by the fuel.
The radialjet pump disconnection — reconnection time on
the engine is highly reduced in comparison with traditional
injection pumps, because it does not require setting.
If the pipe between fuel filter and high-pressure pump is to
be removed-refitted, be sure that hands and components are
absolutely clean.
1. Rail — 2. Fuel inlet from high-pressure pump —
3. Overpressure valve - 4. Pressure sensor.
The rail volume is comparatively small to allow a quick
pressurisation at startup, at idle and in case of high flow-rates.
It anyway has enough volume as to minimise system spikes
and the use of plenum chambers caused by injectors
openings and closings and by the high-pressure pump
operation. This function is further enabled by a calibrated
hole being set downstream of the high-pressure pump.
A fuel pressure sensor (4) is screwed to the rail. The signal
sent by this sensor to the electronic control unit is a
feed-back information, depending on which the rail pressure
value is checked and, if necessary, corrected.
RAIL
108609
12 SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70502
Figure 13
70500
BOOST GAUGE VALVE
The boost valve (1750 bars) is assembled to the rail with the purpose to protect the system’s components in case of excessive
increase of pressure within the high pressure system. Pressure limiter.
The valve can be single-stage (as the one showed in the picture) or double-stage with double working limit (1750 bars and 800
bars).
In the second case, when the pressure within the high pressure system reaches 1750 bars, the valve is activated as a single-stage
one to exhaust the fuel and consequently reduce the pressure until reaching safety parameters. Then it provides mechanically
gauging the pressure into rail to aprx. 800 bars. This way the valve enables working of the engine for extended timing at limited
performances, avoiding the fuel’s overheating and preserving the exhaust galleries.
If the above mentioned valve is activated, the engine control module excludes by isolation the pressure gauge and records the
errore code 8.4.
The pump will flow the maximum delivery to the rail.
A Normally, the tapered piston end keeps closed the
discharge towards the tank.
B If the 1750 bar fuel pressure is exceeded in rail, the small
piston is displaced and the excess pressure is discharged
into the tank.
1. Body — 2. Small piston — 3. Stop — 4. Spring — 5. Direct tank discharge — 6. Seat on rail.
AB
SECTION 2 - FUEL 13
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
15
70505
70506
Figure 14
Figure 15
ELECTRO-INJECTOR
The injector is similar as construction to the traditional ones,
apart from the absence of plunger return springs.
The injector can be deemed as composed of two parts:
-actuator — spray nozzle composed of pressure rod (1),
plunger (2) and nozzle (3);
-control solenoid valve composed of coil (4) and pilot
valve (5).
The solenoid valve controls spray nozzle plunger lift.
Injector in rest position
1. Pressure rod — 2. Plunger — 3. Nozzle — 4. Coil 5. Pilot
valve — 6. Ball shutter 7. Control area — 8. Pressure
chamber — 9. Control volume — 10. Control duct —
11. Supply duct — 12. Control fuel outlet — 13. Electric
connection — 14. Spring — 15. High-pressure fuel inlet.
When coil (4) is energised, it makes shutter (6) move
upwards. The control volume (9) fuel flows towards flow
duct (12) making a pressure drop occur in control volume
(9). Simultaneously the fuel pressure into pressure chamber
(8) makes plunger (2) lift, with following fuel injection into the
cylinder.
Injection end
When coil (4) is de-energised, shutter (6) goes back to its
closing position, in order to re-create such a force balance as
to make plunger (2) go back to its closing position and end
the injection.
Injection start
!
The injector cannot be overhauled and therefore it
must not be disassembled.
15
14 SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Electro-injector
The injectors fitted on the NEF TIER 3 engines are the CRIN 2 - BOSCH versions. Depending on the power developed by the
engine (more than or less than 152 kW) different nozzles (1) are fitted (DLLA or DSLA).
Figure 16
108610
1. Jet.
SECTION 2 - FUEL 15
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Jet Powers Pressures
DLLA Up to 152 kW 250 ÷1600 bar
DSLA Lower to 152 kW 250 ÷1450 bar
PRESSURE LIMITER FOR FUEL RETURN
It is housed on the rear of the cylinder head, and adjusts the
pressure of fuel returning from injectors at a pressure 1.3 and
2 bars. By guaranteeing this pressure to the return fuel, the
fuel vapours formation inside injectors is avoided, optimising
fuel spraying and combustion.
70507
Figure 17
ATo tank — BFrom injectors
16 SECTION 2 - FUEL F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 1
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
SECTION 3
Duty-industrial application
Page
GENERAL SPECIFICATIONS 3...............
-Section pictures of complete engine -
common rail version 3....................
-Clearance data - 4 cyl. 4...................
-Clearance data - 6 cyl. 5...................
PART ONE -
MECHANICAL COMPONENTS 7.........
ENGINE OVERHAUL 9.....................
-Preface 9..............................
-Engine setting operations for the assembly
on turning stand 9.......................
-Disassembly of application components 10.....
-Assembly of application components 17.......
-Completion of the engine 29................
-Checks and inspections 30..................
PART TWO -
ELECTRICAL EQUIPMENT 31.............
LOCATION OF THE MAIN ELECTRICAL
COMPONENTS 33.......................
-EDC7 ECU 34...........................
-Cable on engine 35.......................
-Injectors connector (A) 36..................
-Sensors connector (C) 36..................
-Crankshaft sensor 37......................
-Timing sensor 37.........................
-Supercharging air pressure - temperature sensor 38
-Engine oil temperature-pressure sensor 38.....
2SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Page
-Fuel temperature and pressure sensor 39.......
-Electro-injectors 40........................
-Pre-post heating resistance and contactor 41....
-Coolant temperature sensor 42..............
-Fuel temperature sensor 43.................
-High pressure pump - pressure regulator 44....
PART THREE - TESTS - TROUBLESHOOTING 45
TESTS 47.................................
CHECKING THE FUEL SYSTEM 47.............
DESCRIPTION OF TESTS AND CHECKS
THAT CAN BE PERFORMED 47............
-Necessary equipment 47...................
-Low pressure supply test 48.................
-Low-Pressure Pump 49.....................
-Test on the pressure relief valve on the rail 50...
-Test on fuel backflow from the return 51.......
TROUBLESHOOTING 53....................
PART FOUR -
MAINTENANCE PLANNING 55...........
Page
MAINTENANCE PLANNING 57..............
-Recovery 57.............................
-Regular maintenance and inspection planning 57.
-Checks not included in maintenance
planning-daily checks 58....................
MAINTENANCE PROCEDURES 58............
-Checks and inspections 58..................
-Engine oil level check 58................
-Combustion system inspection 59........
-Cooling system inspection 59............
-Lubricating system inspection 59.........
-Inspection of water presence within
fuel filter or pre-filter 59................
-Inspection/replacement of blow-by filter 60.
-Inspection of drive belt tensioning 60......
-Inspection and setting of tappet clearance 60
-Oil motor and filter replacement 61.......
-Fuel filter replacement 62...............
-Alternator belt replacement 62...........
Figure 1
GENERAL SPECIFICATIONS
Section pictures of complete engine - common rail version
The NEF F4HE engines are characterised by four-stroke diesel
cycles supercharged with 4 or 6 cylinders with 4 valves per
cylinder.
They have high pressure injection fuelling (common rail) and
are entirely electronically driven in order to optimise the
working process in accordance to the operation, limiting as
much as possible the pollution emissions and consumption.
The section herein described is composed or four sections:
-Section of mechanical overhaul prescribed in accordance
to the engine’s specific duty, illustrating all necessary
operation to remove and assembly the external
components of the engine, including cylinder heads,
gearbox of the timing system and of the front part cover;
-Electrical section, describing the connections to the
different components of the engine control module and
of the sensors assembled to the engine;
-Diagnosis section;
-Section of preventive maintenance operations, providing
instructions for the execution of the main operations.
!
Data, features and performances are valid only if the
setter fully complies with all the installation
prescriptions provided by Iveco Motors.
Furthermore, the users assembled by the setter shall
always be in conformance to couple, power and
number of turns based on which the engine has been
designed.
108540
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 3
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
!
Data, features and performances are valid only if the technician fully complies with all the installation requirements provided
by Iveco Motors.
Furthermore, the use of the unit after overhaul showd conform to the original specified power and engine rev/min for
which the engine has been designed.
4SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Clearance data - 4 cyl.
F
4
H
E
9
4
8
4
A
Type
F
4
H
E
9
4
8
4
A
ρCompression ratio 16.5 : 1
Max. output kW
(HP)
rpm
104
141
2200
Max. torque Nm
(kgm)
rpm
560
56
1400
Loadless en
g
ine
idling rpm -
Loadless engine
peak rpm -
Bo
r
e
x
s
t
r
oke
Displacement
104 x 132
4485
TURBOCHARGING
Turbocharger type
with intercooler
HOLSET HX27W
bar LUBRICATION Forced by gear pump, relief valve single action
oil filter
Oil pressure (warm engine)
- idling bar
-peakrpm bar
0.7
4.0
COOLING
Water pump control
Thermostat
-startofopening °C
By liquid
Through belt
82.2
15W40 ACEA E3
FILLING
engine sump liters
engine sump + filter liters
5.3
6.3
!
Data, features and performances are valid only if the technician fully complies with all the installation requirements provided
by Iveco Motors.
Furthermore, the use of the unit after overhaul showd conform to the original specified power and engine rev/min for
which the engine has been designed.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 5
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Clearance data - 6 cyl.
F
4
H
E
9
6
8
4
P
Type
F
4
H
E
9
6
8
4
P
ρCompression ratio 17.5 : 1
Max. output kW
(HP)
rpm
175
234
2300
Max. torque Nm
(kgm)
rpm
1020
102
1500
Loadless en
g
ine
idling rpm -
Loadless engine
peak rpm rpm -
Bo
r
e
x
s
t
r
oke
Displacement
104 x 132
6728
TURBOCHARGING
Turbocharger type
with intercooler
HOLSET HX35W
bar
LUBRICATION
Oil pressure (warm engine)
- idling bar
Forced by gear pump, relief valve single action
oil filter
b
a
r
- peak rpm bar 2
4
COOLING
Water pump control
Thermostat
- start of opening ºC
By liquid
Through belt
81 ±2
15W40 ACEA E3
FILLING
engine sump liters
engine sump + filter liters
15
15 + 1
6SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
PART ONE - MECHANICAL COMPONENTS
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 7
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
DIAGNOSI
8SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Disconnect the high pressure fuel pipeline (10, Figure 2) from
the rail diffuser and from the high pressure pump (8) and
disassemble it from the engine block removing the fixing
clamps.
Disconnect the pipeline (7) feeding the mechanic pump that
is combined to the high pressure pump through the
exchanger of the engine control module.
The following information relates to the engine overhaul
operations only for what concerns the different components
customising the engine, according to its specific duties.
In section ”General overhaul”, all the operations of engine
block overhaul have been contemplated. Therefore the
above mentioned section is to be considered as following the
part hereby described.
!
With regard to the engine disassembly operations
from the machine, please apply for Information
consulting the specific manual.
All operations of Engine disassembly operations as
well as overhaul operations must be executed by
qualified technicians provided with the specific
tooling and equipment required.
Figure 2
In order to apply the brackets 99341009 to the engine block
to fix it on to the stand for the overhaul, it is necessary to
perform the following operations on the left hand side of the
engine:
-Using the tool 99360073 disassembly the fuel filter (6)
and remove it from the support (1);
-Disconnect the electrical connection (2) from the
support (1) and the heater’s one (placed on the filter
support as well);
-Disconnect the fuel low pressure pipelines (3-4-5) from
the support (1);
-Disconnect pipeline (9) from the support (1);
-Remove the sustaining support bracket (1) from the
block.
70126
Figure 3
!
Press clamp (1), as shown in Figure B, to disconnect
the low pressure fuel pipes (3 — 4 — 5, Figure 2) from
the corresponding connections.
After disconnecting the pipe, reset the clamp (1) in
locking position (Figure A) to prevent distortions.
!
Because of the high pressure in the pipelines running
from the high pressure pump to the rail and from this
last one to the electro-injectors, it is absolutely
required NOT to:
-disconnect the pipelines when the engine is
working;
-re-use the disassembled pipelines.
Engine setting operations for the assembly on
turning stand
ENGINE OVERHAUL
Preface
108541
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 9
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 4
On the right hand side of the engine:
Remove the screws and remove the oil pipe (1) from the
turbocharger pipe (2) and from the engine block.
Disconnect the oil feed pipeline unlocking the three screws
M12x25. Remove the O-ring from the pipe.
Remove the starter (2) from the flywheel housing (1).
Apply brackets 99361037 to engine block and use them to
secure the engine to the revolving stand 99322205. Remove
sump cap and drain out oil.
Remove the fan from the output shaft pulley.
74166
Figure 5
74168
Figure 6
Disassembly of application components
1. Connections for Electro-injectors - 2. Engine cooling liquid temperature’s sensor - 2. Cable of the fuel pressure sensor -
4. Sensor of engine’s oil temperature and pressure - 5. Driving shaft sensor - 6. Electro-injector - 7. Temperature - air
pressure sensor - 8. Timing system sensor - 9. Cable of fuel heater and fuel temperature’s sensor - 10. Cable of pressure
regulating gauge - 11. EDC 7 gearbox.
1
2
1
2
3
4
5
6
7
8
9
10
11
108542
10 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Disconnect the engine’s cable from the connectors (1.
Figure 6) wiring harness to
Electro-injectors (6); (7) air pressure/temperature sensor; (3)
fuel pressure sensor;
(11) engine control module; (10) high pressure pump sensor;
(8) timing system sensor; (2) Thermostat sensor of engine
cooling liquid’s temperature; (5) sensor of engine’s
revolutions.
Figure 7
Remove the screws (1) and disconnect the rail (2).
Disconnect from the rail (2): the fuel pipe (7) according to
procedures described in Figure 3. Disconnect fuel pipes (5)
from rail (2) and injector manifolds (6).
!
When releasing pipe (6) connections (4) to rail (2),
use the proper wrench to avoid rotation of flow
limiters (3).
74170
Disconnectthepipeline(2)fromthefuelrecover
pressure-limiter, working on the connections as described in
Figure 3.
Unscrew the nut and loosen the clamp tightening the oil
vapour pipe.
Removethepipe(6).
Loosen the screws (3) and disassemble the blow-by filter (4).
Remove on the nuts and tappet cover.
Figure 8
Figure 9
74744
Remove nuts (7) and disconnect the electrical cables from
injectors (8).
Remove screws (1) and disconnect injector wiring support
(2) including the gasket.
Remove screws (5), disconnect air pressure/temperature
sensor (6).
Remove nuts (3) and remove fuel manifolds (4).
!
Disassembled fuel manifolds (4) must not be used
again, replace with new ones during reassembly.
1
2
3
4
5
6
108543
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 11
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 10
Figure 11
70132
Loosen tappet adjustment fastening nuts (1) and unscrew the
adjusters.
Remove the screws (2), remove the rocker assembly (3),
consisting of: bracket (6), rockers (4), shafts (5) and remove
jumpers (7) from valves.
Remove rods (8).
70133
Remove injector fastening screws. Use tool 99342101 (1) to
remove injectors (2) from the cylinder head.
Release on the drive belt tensioner (1) and extract the belt
(2) from the belt pulleys from the water pump ones and from
the belt rebound pulleys;
Disassemble the belt tensioner;
Loosen the screws fixing the alternator to the support and
disassemble it.
Remove the screw (4) holding the fixing clamp of the
turbocharger’s lubricating oil pipeline.
Disconnect the oil pipeline (3) from the supports of the heat
exchanger / oil filter and from the pipe fitting (5) to the
turbine.
Remove the fixing nuts and disassemble the turbocharger (1)
from the exhaust collector (2).
Loosen the screws and disassemble the exhaust collector (2)
from the cylinder head.
Figure 12
Figure 13
108545
108546
12 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
On the opposite side, loosen the fixing screws of the inlet
manifold (1) and disassemble the joint to the air heater (2)
for the cold start.
Figure 14
Figure 15
Remove the screws (2) and disconnect the alternator
support (3).
Use tool 99360076 to remove the oil filter (1).
Figure 16
Hook brackets (1) with suitable lifting chains and remove
cylinder head (2) from block using hoist.
Figure 17
Remove the screws (4) and disconnect the oil
temperature/pressure sensor (3).
Remove the screws (1) and then remove: heat exchanger/oil
filter support (2), intermediate plate (6) and relevant gaskets.
Remove the oil level sensor (5).
Figure 18
Remove the screws (1) and disconnect the ECU (2) including
the heat exchanger.
74174
Figure 19
Unloose the screws (3) and remove the cap (1). Keep the
gasket (4), the power take-off (2) and the second gasket (4).
74176
1
2
1
2
34
108547
74779
108549
108580
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 13
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 20
70145
Remove the nut (1) and disconnect the timing sensor (2).
Remove the nuts (3) and disconnect the high pressure pump
(4) including the feed pump (5).
Figure 21
Remove the screws (3) and disassemble the damping
flywheel (2) and the pulley (1).
Figure 22
Figure 23
Remove the screws (1) and disconnect the water pump (2).
Remove the screw (3) and the roller (4).
Remove the screw (3) and disconnect the engine speed
sensor (4).
Remove the ring sealing the engine’s driving shaft from the
front cover. Use the tool 99340055 (4) to operate on the
front bar hold of the driving shaft. Through the steering holes
of the tool, perforate the inside holding ring (1) with a straight
way drill (diam. 3,5mm) for the depth of 5mm. Fix the tool
to the ring tightening the 6 screws provided with the
equipment. Then proceed removing the ring (2) by tightening
the screw (3).
00900t
Figure 24
00904t
Using the specific tie rod (3) of the tool 99363204 and the
ancillary lever (4), remove the external holding ring (2) from
the front cover (1).
70146
Fit tool 99360339 (2) to the flywheel housing (1) to stop
flywheel (3) rotation.
Loosen the screws (4).
Figure 25
108548
108549
14 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 26
70149
Remove the screws (1) and take out the front cover (2).
!
Take note of screw (1) assembling positions since
they have different lengths.
70151
Remove two opposite screws (1) from the area where the
withdrawal pins will be introduced (2, Figure 29).
Loosen the remaining flywheel fixing screws (3) from the
driving shaft (4).
Remove the flywheel locking tool 99360351.
Figure 27
Remove the screws (1) and disconnect the oil pump (2).
Figure 28
Figure 29
70152
Tighten two screws of medium length into the holes (4) to
sling the flywheel with the hoist.
Throughout the two guide pins (2) previously screw into the
driving shaft holes (3) withdraw the engine flywheel (1) after
slinging it with the hoist.
00903t
Figure 30
Remove the holding ring of the flywheel cover box using the
tool 99340056 (3) to operate on the driving shaft’s back bar
hold (5).
Through the steering holes of the tool, perforate the inside
holding ring with a straight way drill (diam. 3,5mm) for the
depth of 5mm.
Fix the tool 99340056 (3) to the ring tightening the 6 screws
provided with the equipment.(4)
Then proceed removing the ring (1) by tightening the screw
(2).
Using a specific tie rod of the tool 99363204 and an ancillary
lever, remove the external holding ring (2) from the front
cover.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 15
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70153
Remove the screws (2) and take out the rear cover (1).
!
Take note of screw (2) assembling positions since
they have different sizes.
74775
Figure 31
Overturn the engine.
Remove the screws (2), disassemble the plate (3) and
disconnect the oil sump (1).
Figure 32
Remove the screws (1 and 4) and disassemble the oil suction
tube (5). Remove the screws (2) and disassemble the
stiffening plate (3).
70156
Figure 33
Remove the screws (1) and remove the gear (3) from the
camshaft (2).
70157
Figure 34
Remove the screws (2) and disconnect the timing gear case
(1).
!
Take note of screw (2) assembling positions since
they have different sizes.
Figure 35
!
The shape and the dimensions of the oil pan and of
the suction tube may vary according to the duty of
the engine. The relevant pictures of the instructions
are therefore providing an outline of the
intervention to be executed.
However the procedures described are still
applicable.
!
For F4HE0684 engines the stiffening plate (4) has a
single element.
86516
16 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
DIAGRAM FOR TIGHTENING THE REAR TIMING
GEAR CASE FASTENING SCREWS
Refit the case (1) to the engine block.
Screw the fastening screws in the same position found at
removal and tighten them to the following torque values in
the sequence shown in the figure:
ScrewsM12 65to89Nm
Screws M8 20 to 28 Nm
ScrewsM10 42to52Nm
Figure 36
Assembly of application components
LOCTITE 5205 SEALANT APPLICATION AREAS
Clean accurately the timing gear case (1) and the engine
block.
70209
!
Perfect seal is only obtained by cleaning accurately
the surface to seal.
Smear the case with LOCTITE 5205 to obtain a bead
of few mm diameter.
It shall be uniform (no clots), without air bubbles, thin
areas or discontinuities.
Any imperfection shall be corrected as soon as
possible.
Avoid to use excess material to seal the joint.
Excessive sealant could come out from joint sides
and cause lubricant passage clogging.
After applying the sealant, the joint shall be
assembled immediately (10 — 20 minutes).
70210
Figure 37
Figure 38
70211
Use a felt pen to mark the driving gear (1) tooth fitted on the
output shaft (2) having the mark () for timing on the side
surface.
!
Fasten screwing of the two pins to facilitate the
operation of engine driving shaft rotation.
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 17
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 39
Rotate the output shaft (4) and thecamshaft (2) so that when
fitting the driven gear (1) on the camshaft the marks on the
gears (1 and 3) are coinciding.
Figure 40
70213
Tighten the screws (1) fastening gear (2) to camshaft (3) to
the specified torque.
Figure 41
70214
LOCTITE 5205 SEALANT APPLICATION AREAS
!
Perfect seal is only obtained by cleaning accurately
the surface to seal.
Smear the case with LOCTITE 5205 to obtain a bead
of few mm diameter.
It shall be uniform (no clots), without air bubbles, thin
areas or discontinuities.
Any imperfection shall be corrected as soon as
possible.
Avoid to use excess material to seal the joint.
Excessive sealant could come out from joint sides
and cause lubricant passage clogging.
After applying the sealant, the joint shall be
assembled immediately (10 — 20 minutes).
Figure 42
70215
SEQUENCE FOR TIGHTENING THE FLYWHEEL
HOUSING FASTENING SCREWS
Refit the housing (1) to the engine block and screw the
fastening screws in the same position found at removal and
tighten them to the following torque values in the sequence
showninthefigure:
ScrewsM12 75to95Nm
ScrewsM10 44to53Nm
Not available
On engines
F4AE0684H-E
F4HE0684E-F-J
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
108577
18 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 43
70217
!
Where the engine is coupled to a mechanical clutch,
verify that the flywheel nominal thickness of 49,6 ±
0,13 mm.
Check ring gear teeth (2), if breakage or excessive wear is
found remove the ring gear from the engine flywheel (1,
Figure 43) using a suitable hammer and fit the new one,
previously heated to 150°C for 15 to 20 minutes. Chamfering
on ring gear inside diameter shall be facing the engine
flywheel.
Figure 44
Figure 45
Apply tool 99360339 (2) to the flywheel housing to stop
engine flywheel (3) rotation. Tighten the screws (1) fastening
the engine flywheel (3) to the output shaft.
Figure 46
70219
α
!
Tightening to angle is performed using tool
99395216.
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
Apply tool 99346252 part (6) to the rear output shaft tang
(5), secure it by screws (4) and fit the new sealing ring (3).
Position part (1) on part (5), screw nut (2) until completing
sealing ring (3) fitting into flywheel housing (7).
Screw two pins (2) having suitable length into shaft holes (3)
and remove the engine flywheel (1) using proper sling and
hoister.
70152
Figure 47
0901t
Tighten engine flywheel (2) fastening screws (1) in two
stages:
-1st stage, tightening to 30 ±4Nmtorquewith
dynamometric wrench;
-2nd stage, tightening to 60 ±5°angle.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 19
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 48
70220
Fit the oil pump (1).
Tighten the fastening screws (2) to the specified torque.
Figure 49
70221
Apply a new sealing ring (2) to the water pump (1).
Figure 50
Fit the water pump (1).
Tighten the screws (2) to the specified torque.
Figure 51
70223
Remove the sealing ring (2) from the front cover (1), clean
accurately the coupling surfaces and smear them with
LOCTITE 5205.
Clean accurately the front cover (2) surface and refit it.
Tighten the screws (1) to the specified torque.
Figure 52
Apply tool 99346252 part (4) to the front output shaft tang
(6), secure it by screws (5) and fit the new sealing ring (7).
Position part (2) on part (4), screw nut (3) until completing
sealing ring (7) fitting into front cover (1).
00902t
Figure 53
70222
70224
20 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 54
Fit the plate (1), the oil pick up tube (2) and tighten the
fastening screws (3) to the specified torque.
Figure 55
Set the gasket (1) on the oil sump (2).
!
The pictures of the instructions relating to the oil pan
and to thesuction rose may not reflect the actual shape
and dimensions of your engine equipment. However
the procedures described are still applicable.
Figure 56
Fit the oil sump (1) and apply the plate (3) to it.
Tighten the screws (2) to the specified torque.
74775
Figure 57
Assemble the pulley (1) and the damping flywheel (2) to the
driving shaft.
Tighten the fixing screws (3) and clamp them to the couple
68 ±7 Nm.
70230
Fit a new sealing ring on the speed sensor (3).
Fit the speed sensor (3) on the front cover (1) and tighten
the screw (2) to the specified torque.
Figure 58
Figure 59
Fit on the engine block: a new gasket (1), the heat exchanger
(2) a new gasket (3) and the oil filter support (4).
Tighten the screws (5) to the specified torque.
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt. !
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
108553
108548
108576
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 21
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 60
Figure 61
Lubricate the sealing ring (2) with engine oil and set it on the
oil filter (3).
Screw manually to seat the oil filter (3) on the support
connection (1) and then screw again the oil filter (3) by ¾
turn.
Apply a new sealing ring on the oil temperature/pressure
sensor (4) and fit it on the support (1).
Tighten the screws (5) to the specified torque.
Fit a new sealing ring (6) in the engine block seat.
70234
Position the alternator support (1) so that pins (3 and 4) are
set against the engine block.
Tighten the screws (2) to the specified torque.
Refit the alternator (1).
Tighten the screw (2) to the specified torque.
Figure 62
Figure 63
Refit the automatic belt tensioner (2).
Tighten the screw (3) to the specified torque using a wrench,
turn the automatic belt tensioner (2) to fit the belt (1) on
pulleys and guide rollers.
70145
Refit the high pressure pump (6) including the feed pump (5)
and tighten the nuts (3) to the specified torque. Fit the
support (4) with a new sealing ring, the timing sensor (2) with
a new sealing ring and tighten the relevant fastening nut (1)
to the specified torque.
Figure 64
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
108578 108550
108552
22 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 65
Insert the power take-off (2) equipped with the gasket (4),
the cover (I) and its gasket (4).
Tighten the screws (3) to the prescribed matching couple.
74176
Figure 66
Assemble the electronic gearbox (2) equipped with the
exchanger to the engine, fixing it with the screws (1).
In case the rubber buffers are cracked or excessively
deformed, provide replacing them.
74174
Figure 67
Direct the output shaft (4) and the camshaft (2) so that when
fitting the driven gear (1) on the camshaft the marks on the
gears (1 and 3) are coinciding.
Figure 68
Assemble cylinder head (1), tighten the screws (2) in three
following steps, following order and mode shown in the
figure below.
!
The angle tightening is carried out through tool
99395216 (3).
α
70336
Tightening order layout for cylinder head fastening screws:
-1st step pre-tightening with dynamometric wrench:
Screw 12x1.75x130 ( ) 35 ±5Nm
Screw 12x1.75 x 150 ( ) 55 ±5Nm
-2nd step tightening with a 90 ±5°angle
-3rd step tightening with a 90 ±5°angle
A=Frontside
70476
α
Figure 69
A
74779
1
2
3
4
1
2
6-cylinder engine
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 23
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 70
Figure 71
70338
Fit a new sealing ring (2) lubricated with petroleum jelly and
a new sealing washer (3) on injector (1).
70339
Fit injectors (1) on the cylinder head seats, directed so that
the fuel inlet hole (2) is facing the fuel manifold seat (3) side.
Figure 72
70133
Use tool 99342101 (1) to fit the injector (2) into its seat.
Screw injector fastening screws without tightening them.
Figure 73
70337
4-cylinder engine A
α
Cylinder head fastening screws tightening sequence:
-1st stage pre-tightening, with a torque wrench::
Screw 12x1.75x130 ( ) 35 ±5Nm
Screw12x1.75 x 150 ( ) 55 ±5Nm
A = Lato anteriore
-2nd stage tightening with angle 90 ±5°
-3rd stage tightening with angle 90 ±5°
24 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 74
Figure 75
Figure 76
Figure 77
91572
Fit a new sealing ring (3) lubricated with petroleum jelly on
the fuel manifold (2) and fit it into the cylinder head seat so
that the positioning ball (5) is coinciding with the relevant
housing (4).
!
Disassembled fuel manifolds (2) must not be used
again. Replace with new items.
The fuel manifolds (2) for F4HE0684 engines have
2 positioning spheres.
!
During this operation, the injector (1) shall be
moved so that the manifold (2, Figure 72) is properly
inserted into the fuel inlet hole (2, Figure 74).
70342
Use the torque wrench to tighten gradually and alternately
the injector fastening screws (1) to 8.5 ±0.8 Nm torque.
Tighten the fuel manifold (3) fastening nuts (2) to 50 Nm
torque.
Carry out the assembly of the equalisers’ unit , after previous
check of the components.
70343
ROCKER ASSEMBLY COMPONENTS:
1. Screws - 2. Bracket - 3. Shafts - 4. Rockers.
SHAFT-ROCKER MAIN DATA
Check that shaft/rocker coupling surfaces are not showing
excessive wear or damages.
Rocker control rods shall not be distorted; the ball seats in
touch with the rocker adjusting screw and with tappets
(arrows) shall not show seizing or wear; otherwise replace
them. Intake and exhaust valve control rods are identical and
are therefore interchangeable.
32655
Figure 78
Screw the fastening nuts (2, Figure 75) without locking them.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 25
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 79
Figure 80
Figure 81
70345
Fit the rods (2).
Position jumpers (1) on valves with marks ()facingthe
exhaust manifold.
70346
Check that tappet adjusters (1) are loose to prevent their
balking on the rods (2, Figure 79) when refitting the rocker
assembly.
Then refit the rocker assembly consisting of: bracket (5),
rockers (3), shafts (4) and secure them to the cylinder head
by tightening the fastening screws (2) to 36 Nm torque.
70520
Adjust clearance between rockers and valves using setscrew
wrench (1), box wrench (3) and feeler gauge (2).
Clearance shall be as follows:
- intake valves 0.25 ±0.05 mm
- exhaust valves 0.50 ±0.05 mm.
!
On TIER 3 engines, due to the additional lobe for the
INTERNAL E.G.R., it is not possible to use the valve
clearance adjustment procedure that requires
adjusting the clearance of all the valves by positioning
the crankshaft 2 times only.
Each cylinder must be checked by taking it to the
T.D.C. (top dead centre) at the end of compression
and adjusting the clearance of both valves on the
cylinder in question.
26 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 82
Figure 83
Figure 84
Figure 85
Apply to the coupling surface of the intake manifold (1)
equipped with heater (2) a sufficient coat of LOCTITE 5999
and provide tightening the screws to the prescribed matching
couple.
Fit the rail (2) and tighten the screws (1) to the specified
torque, connect the ground cable (3) to the intake manifold
(4) and tighten the fastening nut to the specified torque.
Connect new fuel pipes (1) to rail (3) and injector manifolds
(2).
!
Pipe (7) connections shall be tightened to 20 Nm
torque, using the proper wrench (5) and the torque
wrench 99389833 (4).
Connections (6) shall be tightened by holding the
flow limiting valve hexagon (1) with the proper
wrench.
Connect the fuel pipe (3) to the rail (2) following the
procedure shown in the following figure.
70126
Press the clamp (1) in arrow direction (Figure B) and connect
the pipe to the rail, reset the clamp to the initial locking
position “A”.
!
Check proper fuel pipe connection.
Figure 86
108547
108567
108568
108569
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 27
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70352
Figure 87
Figure 88
Figure 89
Figure 90
Check electrical cable (5) conditions, replace if damaged by
cutting the support (2) clamps and removing the screws (4)
that secure it to connections (3).
Fit a new gasket (1) on the support (2).
Fit the wiring support (2) and tighten the screws (1) to the
specified torque.
Fit a new gasket (2) on the tappet cover (1).
Place the tappet cover on, install the bolts in the correct
position and tighten.
70355
Reconnect the exhaust manifold (2) with new gaskets. Tighten
the fastening screws (1) to the specified torque.
Sling the turbocharger (1) and place it over the manifold after
having first inserted a new gasket.
Connect the oil pipeline (3) to the support of the heat
exchanger /oil filter. Fix the pipe (3) to the pipe fitting on the
turbocharger.
!
Before any assembly operation always verify that the
hole and screw threads have no evidence of wear or
dirt.
Connect the electrical cables (1) to the injectors (3) and use
the torque wrench 99389834 (4) to tighten the fastening
nuts (2) to the specified torque.
Figure 91
108570
108571
108572
28 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
74170
Figure 92
Insert the blow-by filter (4) tightening the screws.
Connect the pipeline (6) and fix the oil vapour recover pipe
through the clamp (5); lock up the nut fixing it to the upper
edge.
Connect the pipeline (2) to the pressure- limiter (1).
1
2
3
4
5
6
Figure 93
1
2
Assemble the starter (2) to the internal part of the flywheel
cover.
Assemble the oil feeding pipe using a new O-ring. Fix with
three M12x25 screws.
Assemble the bracket and the support (1) of the fuel filter (6).
Proceed connecting in sequence the pipelines (9,3,4 and 5)
of the support (1) to the high pressure pump (8).
Connect the pipeline (7) from the high pressure pump to the
engine control module heat exchanger.
Connect the pipeline (10) from the high pressure pump to
the rail diffuser.
Figure 94
70126
All the fuel pipelines are fixed using the clamps shown in the
picture.
For the connection of the pipes, press the clamp (I) following
the arrow’s direction (Figure B) and connect the pipe to the
clamp on the high pressure pump or on the support of the
fuel filter.
Reset the clamp in the initial locking ”A” position.
!
In case the pipes are re-employed, they must keep
the sealing tops at the edges.
Make sure that the fuel pipeline is correctly
connected.
Reconnect the engine harness to all the sensors, the engine
control module and the rail diffuser (see Figure 6)
Figure 95
108541
Completion of the engine
Properly handle the engine holding it by a lifter, remove it
from the rotating shaft, remove the brackets 99341009 and
place it on proper suitable support to carry out the
completion.
Proceed assembling the oil filter.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 29
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
-that there are no water leaks from the connecting
sleeves of engine cooling circuit pipes and cab internal
heating pipes, tighten the clamping collars if required;
-check carefully the connection between the low
pressure fuel pipes and the relevant connectors;
-that there are no oil leaks between the cover and the
cylinder head, between oil sump and engine block,
between heat exchanger oil filter and the relevant
housings and between the different pipes in the
lubricating circuit;
-that there are no fuel leaks from the fuel pipes;
-that there are no air leaks from pneumatic pipes (if
fitted);
-check also proper operation of the warning lights set on
the instrument panel and of the equipment
disconnected when engine was removed.
-Carefully check and bleed the engine cooling equipment
by repeated draining operations.
Checks and inspections
Start the engine and leave it running just above the
idling speed, wait until the coolant reaches the
temperature necessary to open the thermostat and
then check:
!
The following checking inspections must be carried
out after the engine assembly on the vehicle .
30 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
PART TWO - ELECTRICAL EQUIPMENT
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 31
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
32 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 96
The NEF F4HE engines are fully driven by the electronic
engine control module, which is assembled directly to the
engine by means of a heat exchanger enabling its cooling,
utilising rubber buffers to reduce vibration originated by the
engine.
Through the engine control module it is possible to verify the
correct working of the engine. (See part three of the hereby
user’s guide specifically dedicated to diagnostic).
The electrical and electronic components of the engine are
listed here following:
1. Coolant temperature sensor.
2. Electro-injector.
3. RAIL pressure sensor.
4. Air temperature/pressure sensor.
6. Timing sensor.
7. Solenoid valve for pressure regulator.
8. Fuel temperature sensor.
9. EDC electronic control unit.
10. Crankshaft sensor.
11. Engine oil pressure/temperature sensor.
12. Heating element for pre-post heating.
LOCATION OF THE MAIN ELECTRICAL COMPONENTS
108641
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 33
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 97
A - Connector to injectors; B - Connector to chassis (Provide reference of the vehicle to which the engine is assembled);
C - Connector to sensors.
01525t
EDC7 ECU
34 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Figure 98
1. Injectors for cylinders 1-2 - 2 Injectors for cylinders 3-4 - 3. Injectors for cylinders 5-6 - 4. Engine rpm sensor -
5. Timing sensor - 6. Engine oil pressure and temperature sensor - 7. Fuel temperature sensor -
8. Coolant temperature sensor - 9. Air temperature and pressure sensor - 10. Rail temperature and pressure sensor -
11. Pressure regulator - 12. Connector C EDC control unit (signal) - 13. Connector A EDC control unit (power).
Cable on engine
All the components described below refer to the engine cable in question, therefore the connections to the pins are a preliminary
version, in other words at the approval stage.
0051064t
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 35
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Injectors connector (A) Sensors connector (C)
36 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
ECU PIN FUNCTION ECU PIN ECU PIN
1Cylinder 5 injector 1 -
2Cylinder 6 injector 2 -
3Cylinder 4 injector 3 -
4Cylinder 1 injector 4 -
5Cylinder 3 injector 5 -
6Cylinder 2 injector 6 -
7 - 7 -
8 - 8 -
9Pressure regulator 9Timing sensor
10 Pressure regulator 10 Timing sensor
11 Cylinder 2 injector 11 -
12 Cylinder 3 injector 12 Negative for rail temperature and pressure sensor
13 Cylinder 1 injector 13 Positive for rail temperature and pressure sensor
14 Cylinder 4 injector 14 Signal from rail temperature and pressure sensor
15 Cylinder 6 injector 15 Coolant temperature sensor
16 Cylinder 5 injector 16 -
17 -
18 Signal from fuel temperature sensor
19 Engine rpm sensor
20 -
21 -
22 -
23 Engine rpm sensor
24 Negative for engine oil pressure and temperature
sensor
25 Negative for air temperature and pressure sensor
26 Coolant temperature sensor
27 Signal from engine oil pressure sensor
28 Signal from engine oil temperature sensor
29 -
30 -
31 -
32 Positive for engine oil pressure and temperature
sensor
33 Positive for air temperature and pressure sensor
34 Signal from air pressure sensor
35 Negative for fuel temperature sensor
36 Signal from air temperature sensor
Figure 99
Crankshaft sensor
Crankshaft sensor
This is an inductive sensor located at the front left hand side of the engine. The crankshaft sensor produces signals obtained from
a magnetic flux field closing through the openings in a phonic wheel fitted on the crankshaft.
The crankshaft sensor is connected to the control unit on pins 19C - 23C. The sensor impedance is 900 .
50319
Timing sensor
This is an inductive sensor located at the rear left hand side of the engine. The timing sensor generates signals obtained from a
magnetic flux field closing through the holes in the timing gear on the camshaft. The signal generated by this sensor is utilized by
the electronic control unit as an injection phase signal.
Although it is similar to the flywheel sensor, these two devices areNOTinterchangeablebecauseofthe different external shape.
The timing sensor is connected to the control unit on pins 9C - 10C. The sensor impedance
is 900 .
Figure 100
5028850342
Connector Wiring diagram
50320
Timing sensor
312
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 37
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1Signal 19C 10C
2Signal 23C 9C
3Shield
Supercharging air pressure - temperature sensor
This component incorporates a temperature sensor and a pressure sensor.
Mounted on the intake manifold, the sensor measures the maximum flow rate of air supplied, which serves to make an accurate
calculation of the quantity of fuel to be injected in each cycle.
The sensor is connected to the control unit on pins 25C - 36C - 33C - 34C.
The power supply is 5 volt
Voltage at the sensor output is proportional to the detected pressure or temperature.
Pin 25C - 36C Temperature
Pin 33C - 34C Pressure
Engine oil temperature-pressure sensor
This component is analogous to the air temperature-pressure sensor.
The engine oil temperature-pressure sensor is installed on the engine oil filter support in a vertical position.
This sensor measures the engine oil temperature and pressure.
The sensor is connected to the control unit on pins 24C - 28C - 32C - 27C.
The sensor is supplied with 5 Volts. The signal detected is transmitted to the EDC control unit which, in turn, controls the relative
device on the instrument panel (gauge + low pressure warning light).
The oil temperature is not displayed on any gauges - this value is used exclusively by the control unit.
Pin 24C - 28C Temperature
Pin 32C - 27C Pressure
Figure 101
5034450324
Wiring diagram
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1Ground 24C 25C
2NTC signal (temperature) 28C 36C
3+5 V power input 32C 34C
4Signal (pressure) 27C 34C
Fuel temperature and pressure sensor
Mounted on one end of the rail, this sensor measures the internal fuel pressure and informs the control unit of the value (feedback).
The injection pressure value is used as a pressure control feedback signal and to determine the duration of the electrical injection
command.
This sensor is connected to the control unit on pins 12C - 14C- 13C.
The power supply is 5 Volt.
Figure 102
Fuel pressure sensor connector
0051065t
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 39
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Ref. Description ECU pin
1Ground 12C
2Signal 14C
3Power supply 13C
Electro-injectors
The electro-injectors are effectively N.O. solenoid valves.
Each injector is connected to the EDC control unit on connector A.
The impedance of the coil of each injector is 0.56 - 0.57 .
Figure 103
50343
50349
Figure 104
40 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Ref. Description ECU pin
CONNECTOR 1
1
2
3
4
Cylinder 2 injector
Cylinder 2 injector
Cylinder 1 injector
Cylinder 1 injector
11 A
6A
13 A
4A
CONNECTOR 2
1
2
3
4
Cylinder 4 injector
Cylinder 4 injector
Cylinder 3 injector
Cylinder 3 injector
14 A
3A
12 A
5A
CONNECTOR 3
1
2
3
4
Cylinder 6 injector
Cylinder 6 injector
Cylinder 5 injector
Cylinder 5 injector
15 A
2A
1A
16 A
Pre-post heating resistance and contactor
The pre-post heating resistance is located on the intake manifold.
The resistance serves to heat the air in pre / post heating operations. This resistance is powered by a contactor on the left hand
side of the chassis.
The resistance impedance is approximately 0.5 .
Figure 105
Figure 106
003215t
Resistance
002371t
A. Control contactor
The control contactor is connected to the control unit B connector.
The contactor is tripped with water and/or fuel temperature below 5 °C.
The contactor impedance is approximately 15 .
!
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 41
F4HE NEF ENGINES
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Coolant temperature sensor
This is a variable resistance sensor able to read the coolant temperature in order to provide the control unit with an indication
of the thermal status of the engine.
The same signal is utilized by the control unit to drive an instrument panel gauge, if present.
This sensor is connected to the control unit on pins 15C - 26C.
The impedance of the coolant temperature sensor at 20 °C is approximately 2.50 .
Figure 107
107471
42 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Fuel temperature sensor
This sensor is identical to the coolant temperature sensor.
This sensor detects the fuel temperature to provide the control unit with a parameter defining the thermal status of the fuel.
The fuel temperature sensor is connected to the control unit on pins 35C -18C.
The sensor impedance at 20 °C is approximately 2.50 .
Figure 108
1. Fuel temperature sensor - 2. Filter heating resistance.
0051140t
The ECU drives the filter heater contactor at fuel temperature 5°C.
107798107799
Connector
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 43
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1Ground 15C 35C
2Temperature signal 26C 18C
High pressure pump - pressure regulator
Figure 109
A. Pressure regulator.
000912t
The quantity of fuel supplied to the high pressure pump is metered by the pressure regulator on the low pressure system; the
pressure regulator is managed by the EDC7 control unit.
Delivery pressure to the rail is modulated between 250 and 1450 bar by the electronic control unit by controlling the pressure
regulator solenoid valve.
-This component is a N.O. solenoid valve.
-The solenoid is connected to the control unit on pins 9A - 10A.
-The solenoid valve impedance is approximately 3.2 .
44 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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PART THREE - TESTS - TROUBLESHOOTING
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 45
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46 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Figure 110
TESTS
CHECKING THE FUEL SYSTEM
This section analyses the tests for correctly troubleshooting and checking the fuel circuit and the common rail injection system.
The stated procedure can be used in the event of trouble with the engine injection system correlated with error codes 8.x saved
in the control unit, or not accompanied by any error code and the user notices a drop in performance. The following table gives
descriptions of error codes 8.x.
108599
DESCRIPTION OF TESTS AND CHECKS THAT CAN BE PERFORMED
The contemplated tests are:
-Low pressure supply test
-Test on the pressure relief valve on the rail
-Test on fuel backflow from the injector return
Necessary equipment
Use the kit dwg. 99305453 described in the figure.
1. Pressure gauge 1 (0 - 15bar) and standard couplings - 2. Pressure gauge 2 and standard couplings - 3. 2-litre container -
4. Pressure gauge pipes - 5. Graduated container of 100ml - 6. Plug for rail - 7. Closed Voss coupling.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 47
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Error Description
8.1 - Negative deviation of the fuel pressure (actual pressure higher than the objective pressure).
- Positive deviation of the fuel pressure (actual pressure lower than the objective pressure).
- Drop in fuel pressure with vehicle in motion (lack of diesel).
- Drop in fuel pressure with vehicle in motion: downhill with throttle pedal released (lack of diesel).
- Drop in fuel pressure with the engine idling (lack of diesel).
8.2 - Fuel pressure sensor on rail.
8.4 - Backflow valve control (opening the pressure relief valve DBV).
8.5 - Fuel pressure in the rail too high.
- Fuel pressure in the rail too low.
Figure 111
Low pressure supply test
The figure shows the diagram for using the components available in the kit dwg. 99305453.
108600
A. Fuel tank - B. Prefilter - C. Low-pressure pump - D. Fuel delivery circuit -
E. Fuel filter - F. High-pressure pump CP3 - G. High-pressure circuit - H. Common rail -
I. Fuel recirculation circuit - L. Injectors - M1. Pressure gauge 1 fuel filter inlet -
M2. Pressure gauge 2 fuel filter outlet - N. External container.
Figure 112
108601
48 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Figure 113
Low-Pressure Pump
The function of the gear pump is to supply the high-pressure pump CP3. It is driven by the shaft of the high-pressure pump and
is fitted on its rear portion. Under normal operating conditions, the flow of fuel inside the pump is as shown in the figure.
108602
On completing the fuel supply system and with the battery charged to 24.7V, the engine must start within the 20 seconds of
activation of the starter motor, drawing fuel from the external container placed at most 1 metre lower than the engine. If the pump
is not able to draw up fuel in the stated time and therefore start the engine, replace it.
After starting the engine, check the pressure at 1500 rpm:
-OnpressuregaugeM1itmustbebetween6and9bar.
f lower than 6 bar: replace the pump,
if higher than 9 bar: replace the diesel filter.
-On pressure gauge M2 it must be greater than 5 bar:
If lower, replace the diesel filter,
if the trouble persists, check the seals of the couplings of the fuel filter support and of the high-pressure pump inlet.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 49
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Figure 114
Test on the pressure relief valve on the rail
Fitted at one end of the rail, its function is to protect the system’s components if any malfunctioning causes an excessive increase
in the pressure of the high-pressure system.
108603
Disconnect the recirculation pipe (1) of the pressure relief valve and plug it with the Voss coupling of the kit dwg. 99305453. No
diesel must come out of the valve at any engine speed. If the diagnosis system signals fault code 8.4 ”Engine - backflow valve control”,
it means that the EDC control unit has recognised that the valve has opened after a significant change in the pressure of the rail
(greater than 1700bar). Since its opening is to be considered a consequence of the abnormal increase in pressure, the valve is NOT
defective even though a great amount of diesel flows out. Whereas, if the valve seeps diesel without fault code 8.4, then replace
it.
With the overpressure sensor disconnected or with a bundle of defective cables fault code 8.2 is generated and the rail pressure
is set to 710bar (measurable with the diagnosis instrument). Therefore the trouble is to be found in the wiring and it is not necessary
to replace the component.
!
The experience acquired to date shows that the defectiveness is RARELY due to the sensor.
50 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Figure 115
Test on fuel backflow from the return
Permits establishing the operating status of the injectors. The engine speed and power are controlled through the injectors. The
power required by the user, through the accelerator, is converted into the quantity of fuel injected per cycle. In its turn, this is
converted into microseconds of injector opening according to the rail pressure.
108604
Notes:
The injectors may have problems of both a mechanical and an electrical nature; before proceeding with the following analysis, it
is wise to rule out the presence of water in the tank and in the fuel prefilter.
When the EDC warning light comes on occasionally (fault code 8.1) in the phase of acceleration and/or cold start trouble, make
the following checks.
-Possible incorrect tightening of the nut (1) locking the injector duct on the cylinder head. The prescribed torque setting is 50Nm
±5Nm.
Figure 116
108605
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 51
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Figure 117
-Proceed with the injector fuel backflow tests.
Remove the duct (1) from the cylinder head, plug it (2) and fit on the coupled transparent pipe (3).
108606
Make sure first of all that the engine idling speed is as set in the factory. Check the quantities of fuel recirculation from the cylinder
head. The conditions for measuring the quantities of injector return fuel are:
-engine idling and without air compressor or air conditioner working;
-engine at temperature (> 50 °C).
The quantity that flows out must be no greater than 80ml of diesel in one minute. Excessive recirculation (more than 80ml of diesel
a minute) could be caused by:
-incorrect coupling between one or more injectors and the related ”needles”;
-problem of internal leakage of the injector.
To identify the defective injector, follow the method described hereunder. Measure the quantity of fuel flowing out in one minute
from the coupling on the cylinder head by means of a graduated container. After checking that the recirculation is greater than
80ml a minute, plug the rail outlet of one injector (4) at a time by using the rail plug in the kit dwg. 99305453. The defective injector
is the one whose exclusion caused a significant reduction in recirculation. In addition, remember that when changing an injector
it is necessary to change the duct. After identifying the injectors / ducts with a high recirculation, check that the tightness of the
ductsisasdesigned(50Nm±5) and tighten them if they are loose and then check the recirculation values again. If on the other
hand the tightness is correct, remove the pipe and check that the spherical end towards the injector is not out of shape; replace
it if it is and then check the recirculation value again. If the duct is not out of shape either, then replace the injector and duct because
there must be a leak inside the injector. Check the recirculation value again.
52 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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SECTION 3 - DUTY-INDUSTRIAL APPLICATION 53
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ANOMALY POSSIBLE CAUSE
(*) = if available in the equipment
RECOMMENDED TESTS OR
INTERVENTION REMARKS
Low performance at load request.
Possible exessive smoke.
Possible blink-code 8.1
Insufficient fuel level in the tank. Check fuel level. The excessive smoke is due to the fact
that, in case of insufficient fuel feeding, the
engine control module tries to compen-
sate prolonging the injectors working
time.
Fuel tank device partially obstructed by
impurities or deformed because of over-
heating.
Check if the priming pump of the pre-filter
is working correctly.
If the pump plunger is permanently de-
pressed disassemble and check the tank
pick.-up tube. If this is in order, replace the
pre-filter.
Obstructed air filter. Replace the air filter. Solve the cause of the filter’s obstruction.
Excessive fuel blow-by from rail boost
valve.
Check the O Rings and the correct con-
nection of the pipe fittings under the
feeding pump (the lockers must stay out-
side and the fittings must be well locked).
Visually check the low pressure pipeline
integrity.
Unless the leakage is significant, no per-
formance failures will be detected.
To verify O-rings integrity, extract from
the tank the fuel recycling pipeline, seal
the end and activate the priming pump
driving the low pressure circuit.
Excessive fuel blow-by from rail boost
valve.
Disconnect the pipe and visually check if
there are any significant blow-by from the
boost gauge valve; in such case replace
the valve.
The engine suddenly stops (with no previ-
ous problems) and does not start again.
Obstructed fuel filter. Replace the fuel filter. Solve the cause of the filter’s obstruction
(empty and clean the tank and the part of
the circuit over the filter, refill with clean
fuel).
TROUBLESHOOTING
54 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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ANOMALY POSSIBLE CAUSE
(*) = if available in the equipment
RECOMMENDED TESTS OR
INTERVENTION REMARKS
The engine disconnects or does not start. (*)
EDC ”burned” by short circuit on the wir-
ing harness of the friction clutch.
Eliminate the short circuit and replace the
EDC.
Verify that the wire line, close to the
pedal, is not exposed to.
Difficult start and low performance in all
conditions.
Inefficient high pressure pump. After having excluded any other possible
cause, replace the high pressure pump.
Difficult start, low performance and en-
gine running with one cylinder less.
Injector with obstructer or solenoid
(mechanical part) blocked open.
The non-working injector is easily recog-
nisable detecting by feeling the absence of
pulsing within the relevant high pressure
pipe.
In case of low entity blow-by, inficiating
the mechanical working of the injector
but not involving flow limiter activation,
there is no error memorisation in the en-
gine control module.
If the flow limiter is activated. Check error
code memory.
Starting requires in excess of ten seconds,
followed by huge white exhaust fumes,
and a fuel smell.
Injector blocked in open position (with
no return).
The non-working injector is easily recog-
nisable detecting by feeling the absence of
pulsing within the relevant high pressure
pipe.
Usually, whether such symptoms appear,
it is instinctive to give up engine start.
However, by insisting, it is possible to start
the engine.
As a matter of facts, by insisting, if within
the rail the pressure makes the flow li-
miter close up, the engine starts with one
cylinder less and gradually the grade of
fumes reduces and disappears.
Breaking of high pressure pipeline from
pump to rail.
Strange vibrations provoked by slack of
pipe bracket.
Replace the pipeline ensuring the correct
tightening of the anti-vibration bracket
screws.
It is very important, in addition to correct
blocking, to keep the brackets in the orig-
inal position.
Theengineworkswithonecylinderless,
without memorising failure blink codes in
theenginecontrolmodule.
Injector blocked in closed position. Identify the injector that is not working
anymoreandtherelatinghighpressure
filler.
The non-working injector is easily recog-
nisable detecting by feeling the absence of
pulsing within the relevant high pressure
pipe.
PART FOUR - MAINTENANCE PLANNING
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 55
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56 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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MAINTENANCE PLANNING
Recovery
To ensure optimised working conditions, in the following pages we are providing instructions for the overhaul control interventions,
checks and setting operations that must be performed on the engine at due planned dates.
The frequency of the maintenance operations is just an indication since the use of the engine is the main characteristic to determine
and evaluate replacements and checks.
It is not only allowed but recommended that the staff in charge of the maintenance should also carry out the necessary maintenance
and controlling operations even if not being included in the ones listed here below but that may be suggested by common sense
and by the specific conditions in which the engine is run.
Regular maintenance and inspection planning
Checks and periodical inspections
Visualcheckofengine..............................................
Inspectionpresenceofwaterinfuelfilterorpre-filter ......................
Inspectionblow-byfilterelements .....................................
Inspectionofbeltwearstatus .........................................
Inspectionandsettingoftappetclearance ...............................
EDC ............................................................
Replacementofenginesoilandfilter ..................................
Replacementofpre-filter ............................................
Replacementoffuelfilter ............................................
Replacementofblowbyfilter........................................
Replacementofbelt ...............................................
Frequency (hours)
Daily
Daily
-
-
4000
When anomaly occurs
500
1000
500
500
1500
!
The frequency of the maintenance operations is just an indication since the use of the engine is the main characteristic
to determine and evaluate replacements and checks.
The maintenance operations are valid only if the setter fully complies with all the installation prescriptions provided by
Iveco Motors.
Furthermore, the users assembled by the setter shall always be in conformance to couple, power and number of turns
based on which the engine has been designed.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 57
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After engine start and while engine is running, proceed with the following checks and controls:
- check presence of any eventual leakage from the fuel, cooling and lubricating circuits.
- Verify absence of noise or unusual rattle during engine working.
- Verify, using the vehicle devices, the prescribed pressure temperature and other parameters.
- Visual check of fumes (colour of exhaust emissions)
- Visual check of cooling liquid level, in the expansion tank.
Checks not included in maintenance planning-daily checks
It is a good habit to execute, before engine start, a series of simple checks that might represent a valid warranty to avoid inconven-
iences, even serious, during engine running. Such checks are usually up to the operators and to the vehicle’s drivers.
- Level controls and checks of any eventual leakage from the fuel, cooling and lubricating circuits.
- Notify the maintenance if any inconvenience is detected of if any filling is necessary.
MAINTENANCE PROCEDURES
Checks and inspections
Engine oil level check
The check must be executed when the engine is disconnected
and possibly cool.
Thecheckcanbemadeusingthespeciallyprovidedflexible
rod (1) placed on the right hand side of the EDC.
Figure 118
Draw off the rod from its slot and check that the level is within
the etched tags of minimum and maximum level.
Whether it should be difficult to make the evaluation, proceed
cleaning the rod using a clean cloth with no rag grinding and
put it back in its slot. Draw it off again and check the level.
In case the level results being close to the tag showing mini-
mum level, provide filling lubrication of the engine’s compo-
nents.
To provide filling, operate through the upper top (1) or
through the lateral top (2). During filling operation, the tops
must be removed as well as the rod in order to make the oil
flow easier”.
Figure 119
!
The engine oil is highly polluting and harmful.
In case of contact with the skin, rinse well with water
and detergent.
Adequately protect the skin and the eyes, operate in
full compliance with safety regulations.
Disposal must be carried out properly, and in full
compliance with the law and regulations in force.
74174
1
2
108540
58 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
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Combustion system inspection
The check must be executed both when the engine discon-
nected and when it is running.
The check operation consists in examining the fuel pipelines
running from the tank to the pre-filter (if provided in the spe-
cific equipment), to the filter, to the high pressure pump and
to the rail diffuser and from this last one to the head.
Special attention must be paid to the connections on the high
pressure pipelines.
!
Due to the high pressure within the pipelines running
from the high-pressure pump to the rail diffuser and
from this last one to the electro-injectors, special
attention must be aid also in checking presence of any
leakage or blow-by.
Protect the eyes and the skin from any eventual high
pressure jet: these may deeply penetrate under the
skin surface provoking serious poisoning.
Cooling system inspection
The check must be executed both when the engine discon-
nected and when it is running.
Check the pipelines from the engine to the radiator, from the
expansion tank and vice-versa. Find out any blow-by, verify the
status of the pipes specially close to the holding strips.
Verify that the radiator is clean, the correct working of the fan
flywheels, the presence of any leakage from the connectors,
from the manifold and from the radiating unit.
!
Due to the high temperatures achieved by the sys-
tem, do not operate immediately after the engine’s
disconnection, but wait for the time deemed necess-
ary for the cooling.
Protect the eyes and the skin from any eventual high
pressure jet of cooling liquid.
Lubricating system inspection
The check must be executed both when the engine discon-
nected and when it is running.
Verifythepresenceofanyoilleakageorblow-byfromthe
head, from the engine pan of from the heat exchanger.
!
The engine oil is highly polluting and harmful.
In case of contact with the skin, rinse well with water
and detergent.
Adequately protect the skin and the eyes, operate in
full compliance with safety regulations.
Disposal must be carried out properly, and in full
compliance with the law and regulations in force.
Inspection of water presence within fuel filter or pre-filter
!
The components of the common rail system can be
damaged very quickly in presence of water or impur-
ity within the fuel.
Timely proceed operating on the pre-filter (not avail-
able on the engine block) to carry out the drainage of
the water within the feed circuit.
The density of the cooling liquid must be checked any how
every year before winter season and be replaced in any case
every two year.
!
In case of new filling, proceed bleeding system,
through the bleeds on the engine.
If bleeding of the system is not carried out, serious in-
convenience might be caused to the engine due to
the presence of air pockets in the engine’s head.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 59
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Inspection/replacement of blow-by filter
The filter in subject has been developed and equipped for the
collection, filtering and condense of the lubricating oil vapours.
Within the filter unit (1) two cartridge filters are included (2).
Figure 120
Figure 121
The check of the filtering element is carried out by removing
the cover and drawing off the cartridges (2).
Inspection of drive belt tensioning
The drive belt tensioning control is made using an automatic
tensioning device therefore no intervention is required apart
from checking the wear status of the belt itself.
70520
Adjust clearance between rockers and valves using setscrew
wrench (1), box wrench (3) and feeler gauge (2).
Clearance shall be as follows:
- intake valves 0.25 ±0.05 mm
- exhaust valves 0.50 ±0.05 mm.
Inspection and setting of tappet clearance
74188
2
1
!
On TIER 3 engines, due to the additional lobe for the
INTERNAL E.G.R., it is not possible to use the valve
clearance adjustment procedure that requires
adjusting the clearance of all the valves by positioning
the crankshaft 2 times only.
Each cylinder must be checked by taking it to the
T.D.C. (top dead centre) at the end of compression
and adjusting the clearance of both valves on the
cylinder in question.
60 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Oil motor and filter replacement
Due to the several applications, the pan shape and the oil
quantity can change slightly. However, the following oper-
ations are valid for all applications.
We recommend to carry out the oil drainage when the motor
is hot.
-Place a proper container for the oil collecting under the
pan connected with the drain plug.
-Unscrew the plug and then take out the control dipsick
and the inserting plug to ease the downflow of the lubrica-
tion oil.
!
Warning: We recommend to wear proper protec-
tions because of high motor service temperature.
The motor oil reaches very high temperature: you
must always wear protection gloves.
!
The oil motor is very pollutant and harmful.
In case of contact with the skin, wash with much water
and detergent.
Protect properly skin and eyes: operate according to
safety rules.
Dispose of the residual properly following the rules.
-After the complete drainage, screw the plug and carry out
the clean oil filling.
!
Use only the recommended oil or oil having the re-
quested features for the corrrect motor functioning.
In case of topping up, don’t mix oils having different
features.
If you don’t comply with theses rules, the service war-
ranty is no more valid.
-Check the level through the dipsick until when the filling
is next to the maximum level notch indicated on the dip-
sick.
Whereas you replace the lubrication oil, it is necessary to re-
place the filter.
According to the application the filter can be located in differ-
ent positions: the following procedure is a valid guide for all ap-
plications.
-The filter is composed by a support and a filtering car-
tridge. For the cartridge replacement use the
9936076-tool.
!
Warning: the oil filter contains inside a quantity of oil
of about 1 kg.
Place properly a container for the liquid.
Warning: avoid the contact of skin with the motor oil:
in case of contact wash the skin with running water.
The motor oil is very pollutant: it must be disposed
of according to the rules.
-Replace the filtering cartidge with a new one and screw
manually until when the gasket is in contact with the sup-
port.
-Tigthen by means of the 99360076-tool of three fourth
turn.
-Operate the motor for some minutes and check the level
through the dipsick again. If it is necessary, carry out a top-
ping up to compensate the quantity of oil used for the fill-
ing of the filtering cartridge.
SECTION 3 - DUTY-INDUSTRIAL APPLICATION 61
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Fuel filter replacement
According to the applications the filters position and the quan-
tity can change.
However the following operations are valid for all applications.
-Drain the fuel inside the filter by operating the water re-
lease screw. Collect the fuel in a container without impu-
rities.
-Unscrew the cartridge by using the 99360076-tool.
-Collect the eventual fuel inside the filtering cartridge.
-Clean the gasket seat on the support and oil slightly the
gasket on the new filtering cartridge.
-Screw manually the new filtering cartdrige until when the
gasket is completely on its seat.
-Tigthen through the 99360076-tool at 10-15 Nm torque.
!
During this operation don’t smoke and don’t use free
flames.
Avoid to breathe the vapors coming from filter.
Alternator belt replacement
Due to several applications the belt run can change very much.
!
Warning: with switched off motor (but still hot) the
belt can operate without advance notice.
Wait for the motor temperature lowering to avoid
very serious accidents.
For applications with automatic belt stretcher, the procedure
is the following:
Figure 122
-Operate on the tightener (1) and withdraw the belt (2)
from the alternator and water pumps from pulleys and
from the returns pumps.
-Replace the worn belt with a new one.
-Place the belt on the pulleys and the guide rollers.
-Place the automatic tightener in order to key the belt in
the functioning position.
-Further adjustments are not required.
108545
62 SECTION 3 - DUTY-INDUSTRIAL APPLICATION F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 1
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
SECTION 4
Overhaul and technical specifications
Page
GENERAL SPECIFICATIONS 3...............
CLEARANCE DATA 4.....................
4AND6ENGINEOVERHAUL 11.............
ENGINE REMOVAL AT THE BENCH 11........
REPAIR OPERATIONS 12....................
CYLINDER UNIT 12........................
-Checks and measurements 12...............
-Checking head supporting surface
on cylinder unit 13........................
TIMING SYSTEM 14........................
-Camshaft 14.............................
-Checking cam lift and pin alignment 15........
BUSHES 15...............................
-Bush replacement 16......................
-Tappets 16..............................
-Fitting tappets — camshaft 17................
OUTPUT SHAFT 18........................
-Measuring journals and crankpins 18..........
-Measuring journals and crankpins (6 cyl.) 20....
-Replacing oil pump control gear 22...........
-Fitting main bearings 22....................
-Finding journal clearance 22.................
-Checking crankshaft shoulder clearance 23.....
CONNECTING ROD — PISTON ASSEMBLY 23..
-Pistons 24...............................
2SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Page
-Measuring piston diameter 24................
-Piston pins 25............................
-Conditions for proper pin-piston coupling 25....
-Connecting rods 26.......................
-Bushes 27...............................
-Checking connecting rods 28................
-Checking bending 28.......................
-Checking torsion 28.......................
-Fitting connecting rod-piston assembly 28......
-Connecting rod-piston coupling 28............
-Fitting split rings 29........................
-Fitting connecting rod-piston assembly
into cylinder barrels 29.....................
-Finding crankpin clearance 30................
-Checking piston protrusion 31...............
Page
CYLINDER HEAD 32........................
-Removing the valves 32....................
-Checking cylinder head wet seal 33...........
-Checking cylinder head supporting surface 33...
VALVES 34................................
-Removing carbon deposits, checking and
grinding valves 34.........................
-Checking clearance between valve stem and valve
guide and valve centering 34.................
VALVE GUIDE 35..........................
VALVE SEATS 35...........................
-Regrinding — replacing the valve seats 35.......
CYLINDER HEAD VALVE SEATS (6 CYL.) 36....
FITTING CYLINDER HEAD 38................
-Refitting the cylinder head 39................
TIGHTENING TORQUE 40..................
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 3
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
GENERAL SPECIFICATIONS
Type 4CYLINDERS 6CYLINDERS
Cycle Four-stroke diesel engine
Power Turbocharged with intercooler
Injection Direct
Number of cylinders 4 6
Bore mm 104
Stroke mm 132
+++..=
Total displacement cm34485 6728
TIMING
start before T.D.C. A
end after B.D.C. B
18.5º
29.5º
start before B.D.C. D
end after T.D.C. C
67º
35º
X
Checking timing
mm
X
mm
Checking operation
mm
X
mm
-
-
0.20 to 0.30
0.45 to 0.55
FUEL FEED
Injection
Type: Bosch
high pressure common rail
EDC7 ECU
Injector CRIU 2
Nozzle type DSLA and DLLA
Injection sequence 1-3-4-2 1-5-3-6-2 -4
bar
Injection pressure bar 250 - 1450 250 - 1600
4SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
CLEARANCE DATA
Type 4CYLINDERS 6CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
1
X
Cylinder barrels 1102.009 to 102.031
L
Cylinder barrels:
outside diameter 2
length L
-
-
Cylinder barrels — housings on
engine block (interference) -
Outside diameter 20,5
3
XCylinder barrels:
inside diameter 2-
1
X
2
Spare pistons
type:
Size X
Outside diameter 1
Pin housing 2
61
103.730 to 103.748
38.010 to 38.016
Piston — cylinder barrels 0.252 to 0.294
Piston diameter 10.5
X
Piston protrusion X 0.28 to 0.52
3
Piston pin 337.994 to 38.000
Piston pin — pin housing 0.01 to 0.022
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 5
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Type 4CYLINDERS 6CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
X
1
3
2
X
X
X1*
Split ring slots X 2
X3
2.705 to 2.735
2.440 to 2.460
4.030 to 4.050
1
3
2
S
S
S
S1*
Split rings S 2
S3
*measuredon98mm4cyl.
*measuredon99mm6cyl.
* measured on 101 mm
F4HE
2.560 to 2.605
2.350 to 2.380
3.977 to 3.990
1
Split rings - slots 2
3
0.100 to 0.175
0.060 to 0.110
0.040 to 0.083
Split rings 0.5
X1
3
2
X
X
Split ring end opening
in cylinder barrel:
X1
X2
X3
0.30 to 0.40
0.60 to 0.80
0.30 to 0.55
1
2
Small end bush
housing 1
Big end bearing
housing 2
40.987 to 41.013
72.987 to 73.013
S
4
3Small end bush diameter
Outside 4
Inside 3
Spare big end half
bearings S
41.279 to 41.553
38.019 to 38.033
1.955 to 1.968
Small end bush — housing 0.266 to 0.566
Piston pin — bush 0.019 to 0.039
Big end half bearings 0.250 to 0.500
6SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Type 4CYLINDERS 6CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
X
Size X
Max. tolerance
on connecting rod
axis alignment
-
-
12
S1S2
Journals 1
Crankpins 2
Main half bearings S 1
Big end half bearings S 2
*provided as spare part
82.99 to 83.01
68.987 to 69.013
2.456 to 2.464
1.955 to 1.968
3
Main bearings
No. 1 — 5 / 1- 7 3
No.2—3—4 3
87.982 to 88.008
87.977 to 88.013
Half bearings — Journals
No. 1—5 / 1-7
No. 2—3—4 / 2-3-4-5-6
0.041 to 0.119
0.041 to 0.103
Half bearings - Crankpins 0.033 to 0.041
Main half bearings
Big end half bearings 0.250 to 0.500
1
X
Shoulder journal X 1 37.475 to 37.545
X 2
Shoulder main bearing X 2 25.98 to 26.48
X3 Shoulder half-rings X 3 37.28 to 37.38
Output shaft shoulder 0.068 to 0.41
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 7
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Type 4CYLINDERS 6CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
1
Valve guide seats on
cylinder head 17.042 to 7.062
2
3
2
Valve guides
3
-
-
Valveguidesandseatsonhead -
Valve guides -
α
4Valves:
4
α
4
α
6.970 to 6.999
60o±0.25o
6.970 to 6.999
45o±0.25o
Valve stem and guide 0.052 to 0.092
0.052 to 0.092
1
Housing on head for
valve seat:
1
1
34.837 to 34.863
34.837 to 34.863
α
2
Val
v
esea
t
ou
t
side diame
t
e
r
;
valve seat angle on cylinder
head:
2
α
2
α
34.917 to 34.931
60o
34.917 to 34.931
45o
X
X
Sinking X
0.59 to 1.11
0.96 to 1.48
Between valve seat
and head
0.054 to 0.094
0.054 to 0.094
Valve seats -
8SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Type 4CYLINDERS 6CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
HH1 H2
Valve spring height:
free spring H
under a load equal to:
339.8 ±9N H1
741 ±39 N H2
47.75
35.33
25.2
X
Injector protrusion X -
123 4 5
Camshaft bush
housings No. 1-5/1-7
Camshaft housings
No. 2-3-4/2-3-4-5-6
59.222 to 59.248
54.089 to 54.139
1
2
3
Camshaft journals:
15
1753.995 to 54.045 53.995 to 54.045
Camshaft bush outside
diameter: -
Bush inside
diameter 54.083 to 54.147
Bushes and housings
on block -
Bushes and journals 0.038 to 0.162
H
Cam lift:
H
H
6.045
7.582
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 9
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Type 4CYLINDERS 6CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
1
Tappet cap housing
on block 116.000 to 16.030
2
3
2
Tappet cap outside
diameter: 2
3
15.924 to 15.954
15.960 to 15.975
Between tappets and housings 0.025 to 0.070
Tappets -
1
Rocker shaft 121.965 to 21.977
2
Rockers 222.001 to 22.027
Between rockers and shaft 0.024 to 0.162
10 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70159
70158
70160
70161
70162
Figure 1
Figure 2
Figure 3
Figure 4
Loosen the fixing screws (1) and remove the rod caps (2).
Withdraw the pistons including the connecting rods from the
top of the engine block.
Remove the screws (1) and the main bearing caps (2).
The second last main bearing cap (1) and the relevant support
are fitted with shoulder half-bearing (2).
Use tool 99360500 (1) and hoist to remove the crankshaft (2)
from the block.
Remove the main half-bearings (1).
Remove the screws (2) and remove the oil nozzles (3).
!
Keep the half-bearings into their housings since in case
of use they shall be fitted in the same position found
at removal.
!
Take note of lower and upper half-bearing assembling
positions since in case of reuse they shall be fitted in
the same position found at removal.
Figure 5
4AND6ENGINEOVERHAUL
ENGINE REMOVAL AT THE BENCH
The following instructions assume that the engine has
previously been placed on the rotating bench and that
removal of all specific components of the Iveco Motors
equipment have been already removed as well. (See Section
3 of the manual herein).
The section illustrates therefore all the most important engine
overhaul procedures.
The following operations are relating to the 4 cylinder engine
but are similar and applicable for the 6 cylinder.
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 11
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70163
70165
70164
70166
70167
Figure 6
Figure 7
Figure 8
Figure 9
Figure 10
Remove the screws (1) and disconnect camshaft (3) retaining
plate (2).
Withdraw carefully the camshaft (1) from the engine block.
Withdraw the tappets (1) from the engine block.
Once engine is disassembled, clean accurately the
cylinder-block assembly.
Use the proper rings to handle the cylinder unit.
The engine block shall not show cracks.
Check operating plug conditions and replace them in case of
uncertain seal or if rusted.
Inspect cylinder barrel surfaces; they shall be free from seizing,
scores, ovalisation, taper or excessive wear.
Inspection of cylinder barrel bore to check ovalisation, taper
and wear shall be performed using the bore dial gauge (1)
fitted with the dial gauge previously set to zero on the ring
gauge (2) of the cylinder barrel diameter.
Measurements shall be performed on each cylinder, at three
different heights in the barrel and on two planes perpendicular
with each other: one parallel to the longitudinal axis of the
engine (A), and the other perpendicular (B). Maximum wear
is usually found on plane (B) in correspondence with the first
measurement.
Should ovalisation, taper or wear be found, bore and grind the
cylinder barrels. Cylinder barrel regrinding shall be performed
according to the spare piston diameter oversized by 0.5 mm
and to the specified assembling clearance.
!
Take note of plate (2) assembling position.
REPAIR OPERATIONS
CYLINDER UNIT
Checks and measurements
!
Should the ring gauge be not available, use a
micrometer for zero-setting.
s
12 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
zs
Figure 11
!
In case of regrinding, all barrels shall have the same
oversize (0.5 mm).
Checking head supporting surface on cylinder
unit
When finding the distortion areas, replace the cylinder unit.
Planarity error shall not exceed 0.075 mm.
Check cylinder unit operating plug conditions, replace them
in case of uncertain seal or if rusted.
α
Check main bearing housings as follows:
-fit the main bearings caps on the supports without
bearings;
-tighten the fastening screws to the specified torque;
-use the proper internal gauge to check whether the
housing diameter is falling within the specified value.
Replace if higher value is found.
107267
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 13
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70169
Figure 12
TIMING SYSTEM
Camshaft
CAMSHAFT MAIN DATA (4 cyl.)
Specified data refer to pin standard diameter
Figure 13
MAIN DATA ABOUT CAMSHAFT PINS (6 F4HE684 engine cylinders)
Specified data refer to pin standard diameter
Camshaft pin and cam surfaces shall be absolutely smooth;
if they show any traces of seizing or scoring replace the
camshaft and the bushes.
84089
14 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70171
70172
Figure 14
Figure 15
Check camshaft (2) pin diameter using micrometer (1) on
two perpendicular axes.
Camshaft bushes (2) shall be pressed into their housings.
Internal surfaces must not show seizing or wear.
Use bore dial gauge (3) to measure camshaft front and rear
bush (2) and intermediate housing (1) diameter.
Measurements shall be performed on two perpendicular
axes.
BUSHESChecking cam lift and pin alignment
Set the camshaft on the tailstock and using a 1/100 gauge set
on the central support, check whether the alignment error
is not exceeding 0.04 mm, otherwise replace the camshaft.
Check cam lift; found values shall be: 6.045 mm for exhaust
cams and 7.582 mm for intake cams, in case of different values
replace the camshaft.
Figure 16
CAMSHAFT BUSH AND HOUSING MAIN DATA (4 cyl.)
* Value to be obtained after driving the bushes.
107399
Sec. A-A
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 15
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Figure 17
Figure 18
MAIN DATA ABOUT CAMSHAFT BUSHES AND RELATED HOUSINGS
*Height to be obtained after driving the bushes.
70174
To replace front and rear bushes (1), remove and refit them
using the beater 99360362 (2) and the handgrip 99370006
(3).
Bush replacement
!
When refitting the bushes (1), direct them to make
the lubricating holes (2) coincide with the holes on
the block housings.
70175
MAIN DATA CONCERNING THE TAPPETS AND THE
RELEVANT HOUSINGS ON THE ENGINE BLOCK
Tappets
Figure 19
107268
sec. A-A
16 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70176
70164
70238
Lubricate the tappets (1) and fit them into the relevant
housings on the engine block.
Lubricate the camshaft bushes and fit the camshaft (1) taking
care not to damage the bushes or the housings.
Set camshaft (3) retaining plate (1) with the slot facing the
top of the engine block and the marking facing the operator,
then tighten the screws (2) to the specified torque.
Fitting tappets — camshaft
Figure 20
Figure 21
Figure 22
Figure 23
70179
70180
Check camshaft end float (1).
It shall be 0.23 ±0.13 mm.
Fit nozzles (2) and tighten the fastening screws (1) to the
specified torque.
Figure 24
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 17
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70182
70181
Figure 25
Figure 26
Grind journals and crankpins if seizing, scoring or excessive
ovalisation are found. Before grinding the pins (2) measure
them with a micrometer (1) to decide the final diameter to
which the pins are to be ground.
!
It is recommended to insert the found values in the
proper table.
SeeFigure26.
Undersize classes are:
!
Journals and crankpins shall always be ground to the
same undersize class.
Journals and crankpins undersize shall be marked on
thesideofthecrankarmNo.1.
For undersized crankpins: letter M
For undersized journals: letter B
For undersized crankpins and journals: letters MB.
FILL THIS TABLE WITH OUTPUT SHAFT JOURNAL AND CRANKPIN MEASURED VALUES (4 CYL.)
*Rated value
OUTPUT SHAFT
Measuring journals and crankpins
18 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70183
Figure 27
OUTPUT SHAFT MAIN TOLERANCES
70237
MAIN BEARING ON TIMING
SYSTEM CONTROL SIDE
INTERMEDIATE MAIN
BEARINGS
FIRST MAIN BEARING
ON FRONT SIDE
measured on > 45.5 mm radius
between adjacent journals
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 19
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOLERANCES TOLERANCE CHARACTERISTIC GRAPHIC SYMBOL
S
H
A
P
E
Roundness
S
H
A
P
E
Cilindricity //
Parallelism //
DIRECTION Verticality
Straightness
POSITION Concentricity or coaxiality
Circular oscillation
OSCILLATION Total oscillation
Taper
LEVELS OF IMPORTANCE FOR PRODUCT CHARACTERISTICS GRAPHIC SYMBOL
CRITICAL ©
IMPORTANT
SECONDARY
Figure 28
FILL THIS TABLE WITH OUTPUT SHAFT JOURNAL AND CRANKPIN MEASURED VALUES
*Rated value
Figure 29
MAIN OUTPUT SHAFT TOLERANCES
* Measured on a radius greater than 45.5 mm
** 0.500 between adjacent main journals 70577
Measuring journals and crankpins (6 cyl.)
107269
20 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70237
MAIN BEARING ON TIMING
SYSTEM CONTROL SIDE
INTERMEDIATE MAIN
BEARINGS FIRST MAIN BEARING ON
FRONT SIDE
Figure 30
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 21
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOLERANCES TOLERANCE CHARACTERISTIC GRAPHIC SYMBOL
S
H
A
P
E
Roundness
S
H
A
P
E
Cilindricity //
Parallelism //
DIRECTION Verticality
Straightness
POSITION Concentricity or coaxiality
Circular oscillation
OSCILLATION Total oscillation
Taper
LEVELS OF IMPORTANCE FOR PRODUCT CHARACTERISTICS GRAPHIC SYMBOL
CRITICAL ©
IMPORTANT
SECONDARY
70184
70185
70187
Figure 31
Figure 32
Figure 33
Figure 34
Refit the crankshaft (2).
Check the backlash between crankshaf main journals and the
relevant bearings as follows:
Tighten the pre-lubricated screws (1) in the following three
successive stages:
-1st stage,withtorquewrenchto50±6 Nm.
-2nd stage,withtorquewrenchto80±6 Nm.
!
Refit the main bearings that have not been replaced,
in the same position found at removal.
Fitting main bearings
!
Do not try to adapt the bearings.
Main bearings (1) are supplied spare with 0.250 — 0.500 mm
undersize on the internal diameter.
Clean accurately the main half bearings (1) having the
lubricating hole and fit them into their housings.
The second last main half bearing (1) is fitted with shoulder
half rings.
Check that gear toothing (1) is not damaged or worn,
otherwiseremoveitusingtheproperpuller(3).
When fitting the new gear, heat it to 180°C for 10 minutes
in an oven and then key it to the crankshaft.
Figure 35
-clean accurately the parts and remove any trace of oil;
-position a piece of calibrated wire (3) on the crankshaft
pins (4) so that it is parallel to the longitudinal axis;
-fit caps (1), including the half bearings (2) on the relevant
supports.
70186
70161
Replacing oil pump control gear Finding journal clearance
22 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
This check is performed by setting a magnetic-base dial gauge
(2) on the crankshaft (3) as shown in the figure, standard
value is 0.068 to 0.41.
If higher value is found, replace main thrust half bearings of
the second last rear support (1) and repeat the clearance
check between crankshaft pins and main half bearings.
70188
70189
70190
70191
Figure 36
Figure 37
Figure 38
Figure 39
-3rd stage, with tool 99395216 (1) set as shown in the
figure, tighten the screws (2) with 90 ±5°angle.
-Remove caps from supports.
The backlash between the main bearings and the pins is
found by comparing the width of the calibrated wire (2) at
the narrowest point with the scale on the envelope (1)
containing the calibrated wire.
The numbers on the scale indicate the backlash in mm.
Replace the half bearings and repeat the check if a different
backlash value is found. Once the specified backlash is
obtained, lubricate the main bearings and fit the supports by
tightening the fastening screws as previously described.
CONNECTING ROD — PISTON ASSEMBLY
COMPONENTS
1. Stop rings - 2. Pin - 3. Piston - 4. Split rings - 5. Screws -
6. Half bearings - 7. Connecting rod - 8. Bush.
α
Checking crankshaft shoulder clearance
!
Pistons are supplied from parts with 0.5 mm oversize.
CONNECTING ROD PISTON ASSEMBLY
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 23
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
32615
32614
32613
70192
Figure 40
Figure 41
Figure 42
Figure 43
Figure 44
Remove split rings (1) from piston (2) using pliers 99360183
(3).
Piston pin (1) split rings (2) are removed using a scriber (3).
Using a micrometer (2), measure the diameter of the piston
(1) to determine the assembly clearance.
The clearance between the piston and the cylinder barrel can
be checked also with a feeler gauge (1) as shown in the figure.
!
The diameter shall be measured at 12 mm from the
piston skirt.
MAIN DATA CONCERNING KS. PISTON, PINS AND SPLIT RINGS
* Value measured on 99 mm diameter
Pistons
Measuring piston diameter
107270
24 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
32620
16552
32619
18857
Figure 45
Figure 46
Figure 47
Figure 48
To measure the piston pin (1) diameter use the micrometer
(2).
Lubricate the pin (1) and its seat on piston hubs with engine
oil; the pin shall be fitted into the piston with a slight finger
pressure and shall not be withdrawn by gravity.
Use a micrometer (1) to check split ring (2) thickness.
Check the clearance between the sealing rings (3) of the 2nd
and 3rd slot and the relevant housings on the piston (2), using
a feeler gauge (1).
Piston pins
Figure 49
86497
MAIN DATA CONCERNING MONDIAL MAHLE PISTON, PINS AND SPLIT RINGS
* Value measured on 101 mm diameter
Conditions for proper pin-piston coupling
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 25
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
41104
Figure 50
Figure 51
Figure 52
Use a micrometer (1) to check split ring (2) thickness.
DIAGRAM FOR MEASURING THE CLEARANCE X
BETWEEN THE FIRST PISTON SLOT AND THE
TRAPEZOIDAL RING
Since the first sealing ring section is trapezoidal, the clearance
between the slot and the ring shall be measured as follows:
make the piston (1) protrude from the engine block so that
the ring (2) protrudes half-way from the cylinder barrel (3).
In this position, use a feeler gauge to check the clearance (X)
between ring and slot: found value shall be the specified one.
70194
Use feeler gauge (1) to measure the clearance between the
ends of the split rings (2) fitted into the cylinder barrel (3).
MAIN DATA FOR CONNECTING ROD, BUSH, PISTON
PIN AND HALF BEARINGS
Connecting rods
* Value for inside diameter to be obtained after driving in
connecting rod small end and grinding.
** Value not measurable in released condition
!
The surface of connecting rod and rod cap are
knurled to ensure better coupling.
Therefore, it is recommended not to smooth the
knurls.
107271
26 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70196
Figure 53
Bushes
Check that the bush in the connecting rod small end is free
from scoring or seizing and that it is not loosen. Otherwise
replace.
Removal and refitting shall be performed using the proper
beater.
When refitting take care to make coincide the oil holes set
on the bush with those set on the connecting rod small end.
Grind the bush to obtain the specified diameter.
!
Every connecting rod is marked as follows:
-On body and cap with a number showing their
coupling and the corresponding cylinder.
In case of replacement it is therefore necessary
to mark the new connecting rod with the same
numbers of the replaced one.
-On body with a letter showing the weight of the
connecting rod assembled at production:
SV, 1820 to 1860 (yellow marking);
SW, 1861 to 1900 (green marking);
SX, 1901 to 1940 (blue marking);
Spare connecting rods are of the W class with green
marking *.
Material removal is not allowed.
*
CONNECTING ROD BODY
CONNECT-
ING ROD
BODY
CONNECT-
ING ROD
BODY
CONNECT-
ING ROD
BODY
CONNECT-
ING ROD
BODY
CONNECTING ROD
BODY
CONNECTING ROD BODY
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 27
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
61696
61694
61695
70198
Figure 54
Figure 55
Figure 56
Figure 57
Check that the axis of the connecting rods (1) are parallel
using tool 99395363 (5) as follows:
-fit the connecting rod (1) on tool 99395363 (5) spindle
and lock it with screw (4);
-set the spindle (3) on V-blocks by resting the connecting
rod (1) on the stop bar (2).
Check connecting rod (5) torsion by comparing two points
(A and B) of pin (3) on the horizontal plane of the connecting
rod axis.
Position the dial gauge (2) support (1) to obtain a preload of
approx. 0.5 mm on the pin (3) in point A and then set the
dial gauge (2) to zero. Move the spindle (4) with the
connecting rod (5) and compare any deviation on the
opposite side (B) of the pin (3): the difference between A and
B shall not exceed 0.08 mm.
Checkconnectingrod(5)bendingbycomparingtwopoints
C and D of the pin (3) on the vertical plane of the connecting
rod axis.
Position the vertical support (1) of the dial gauge (2) to rest
the latter on pin (3), point C.
Move the connecting rod forwards and backwards to find pin
top position, then in this condition reset the dial gauge (2).
Move the spindle with the connecting rod (5) and repeat the
check of the top point on the opposite side D of the pin (3).
The difference between point C and point D shall not exceed
0.08 mm.
Fitting connecting rod-piston assembly
Connecting rod-piston coupling
The piston crown is marked as follows:
1. Part number and design modification number;
2. Arrow showing piston assembling direction into cylinder
barrel, this arrow shall face the front key of the engine
block;
3. Marking showing 1st slot insert testing;
4. Manufacturing date.
Checking connecting rods Checking bending
Checking torsion
28 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
72705
32613
70200
70201
Figure 58
Figure 59
Figure 60
Figure 61
Figure 62
Connect piston (2) to connecting rod (4) with pin (3) so that
the reference arrow (1) for fitting the piston (2) into the
cylinder barrel and the numbers (5) marked on the
connecting rod (5) are read as shown in the figure.
Position the piston (1) on the connecting rod according to
the diagram shown in the figure, fit the pin (3) and stop it by
the split rings (2).
Fitting split rings
Use pliers 99360183 (3) to fit the split rings (1) on the piston
(2).
Split rings shall be fitted with the marking “TOP” facing
upwards and their openings shall be displaced with each
other by 120°.
Fit half bearings (1) on connecting rod and cap.
Lubricate accurately the pistons, including the split rings and
the cylinder barrel inside.
Use band 99360605 (2) to fit the connecting rod-piston
assembly (1) into the cylinder barrels and check the following:
-the number of each connecting rod shall correspond to
the cap coupling number.
!
Split rings are supplied spare with the following sizes:
- standard, yellow marking;
- 0.5 mm oversize, yellow/green marking;
Fitting connecting rod-piston assembly into
cylinder barrels
!
Refit the main bearings that have not been replaced,
in the same position found at removal.
Do not try to adapt the half bearings.
108597
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 29
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70203
70204
70205
70206
Figure 63
Figure 64
Figure 65
Figure 66
Figure 67
DIAGRAM FOR CONNECTING ROD-PISTON
ASSEMBLY FITTING INTO BARREL
-Split ring openings shall be displaced with each other by
120°;
-connecting rod-piston assemblies shall have the same
weight;
-the arrow marked on the piston crown shall be facing the
front side of the engine block or the slot obtained on the
piston skirt shall be corresponding to the oil nozzle
position.
Finding crankpin clearance
To measure the clearance proceed as follows:
-clean the parts accurately and remove any trace of oil;
-set a piece of calibrated wire (2) on the output shaft pins
(1);
-fit the connecting rod caps (3) with the relevant half
bearings (4).
-Lubricate the screws (1) with engine oil and then tighten
them to the specified torque using the torque wrench
(2).
-Apply tool 99395216 (1) to the socket wrench and
tighten screws (2) of 60°.
-Remove the cap and find the existing clearance by
comparing the calibrated wire width (1) with the scale
onthewireenvelope(2).
α
α
108596
30 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70207
70208
Figure 68
If a different clearance value is found, replace the half bearings
and repeat the check.
Once the specified clearance has been obtained, lubricate
the main half bearings and fit them by tightening the
connecting rod cap fastening screws to the specified torque.
Once connecting rod-piston assemblies refitting is over, use
dial gauge 39395603 (1) fitted with base 99370415 (2) to
check piston (3) protrusion at T.D.C. with respect to the top
oftheengineblock.
Protrusion shall be 0.28 to 0.52 mm.
!
Before the final fitting of the connecting rod cap
fastening screws, check that their diameter
measured at the centre of the thread length is not
< 0.1 mm than the diameter measured at approx. 10
mm from screw end.
Check manually that the connecting rods (1) are sliding
axially on the output shaft pins and that their end float,
measured with feeler gauge (2) is 0.10 to 0.33 mm.
Checking piston protrusion
Figure 69
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 31
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70319
Figure 70
Intake (1) and exhaust (2) valves have heads with the same
diameter.
The central notch () of the exhaust valve (2) head
distinguishes it from the intake valve.
!
Should cylinder head valves be not replaced, number
them before removing in order to refit them in the
same position.
A = intake side — S = exhaust side
CYLINDER HEAD
Removing the valves
Valve removal shall be performed using tool 99360268 (1)
and pressing the cap (3) so that when compressing the
springs (4) the cotters (2) can be removed. Then remove the
cap (3) and the springs (4).
Repeat this operation for all the valves.
Overturn the cylinder head and withdraw the valves (5).
70321
70322
Figure 71
Figure 72
Remove sealing rings (1 and 2) from the valve guide.
!
Sealing rings (1) for intake valves are yellow.
Sealing rings (2) for exhaust valves are green.
32 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70323
Figure 73
Figure 74
This check shall be performed using the proper tools.
Use a pump to fill with water heated to approx. 90°Cand2
to 3 bar pressure.
Replace the core plugs (1) if leaks are found, use the proper
punch for their removal/refitting.
Replace the cylinder head if leaks are found.
Distortion found along the whole cylinder head shall not
exceed 0.20 mm.
If higher values are found grind the cylinder head according
to values and indications shown in the following figure.
Checking cylinder head wet seal
!
Before refitting, smear the plug surfaces with
water-repellent sealant.
Checking cylinder head supporting surface
70325
The rated thickness A for the cylinder head is 105 ±0.25 mm,
max. metal removal shall not exceed thickness B by 1 mm.
!
After grinding, check valve sinking. Regrind the valve
seats, if required, to obtain the specified value.
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 33
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70326
18625
18882
70327
Figure 75
Figure 76
Figure 77
Figure 78
VALVES
INTAKE AND EXHAUST VALVE MAIN DATA
Remove carbon deposits from valves using the proper metal
brush.
Check that the valves show no signs of seizing, scoring or
cracking.
Regrind the valve seats, if required, using tool 99305018 and
removing as less material as possible.
Check the valve stem (1) using a micrometer (2), it shall be
6.970 ÷6.999.
Use a magnetic base dial gauge (1) set as shown in the figure,
the assembling clearance shall be 0.052 ÷0.092 mm.
Turn the valve (2) and check that the centering error is not
exceeding 0.03 mm.
Removing carbon deposits, checking and
grinding valves Checking clearance between valve stem and
valve guide and valve centering
INTAKE
VALVE
EXHAUST
VALVE
34 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
EXHAUST
70328
70330
70331
Figure 79
Figure 80
Use a bore dial gauge to measure the inside diameter of the
valve guides, the read value shall comply with the value
showninthefigure.
Check the valve seats (2). If slight scoring or burnout is found,
regrind seats using tool 99305018 (1) according to the angle
values shown in Figure 81.
VALVE SEATS
Regrinding — replacing the valve seats
VALVE SEAT MAIN DATA (4 CYL.)
INTAKE EXHAUST
INTAKE
Figure 81
VALVE GUIDE
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 35
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
70332
Figure 82
Should valve seats be not reset just by regrinding, replace
them with the spare ones. Use tool 99305018 (Figure 80) to
remove as much material as possible from the valve seats
(take care not to damage the cylinder head) until they can
be extracted from the cylinder head using a punch.
Heat the cylinder head to 80°- 100°C and using the proper
punch, fit the new valve seats, previously cooled, into the
cylinder head.
Use tool 99305018 to regrind the valve seats according to
the values shown in Figure 81.
MAIN DATA CONCERNING THE SEATS ON THE CYLINDER HEAD (4 CYL.)
EXHAUST INTAKE
Figure 83
MAIN DATA ABOUT ENGINE VALVE SEATS
Valve seats are installed by cooling onto the cylinder head
and machining to the correct dimension.
CYLINDER HEAD VALVE SEATS (6 CYL.)
70515
EXHAUST INTAKE
36 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
70332
70331
Figure 84
Figure 85
If valve seats cannot be restored just by regrinding, it is
possible to assemble the spare inserts provided.
In this case, it is necessary to install seats into the cylinder
head sized as shown in the figure and to assemble the valve
seats.
VALVE SEAT MAIN DATA (6 CYL.)
In order to assemble the valve seats into the cylinder head,
it is necessary to heat the cylinder head to 80 to 100°Cand,
through a suitable punch, to assemble the new, previously
cooled valve seats (2) into the head.
Then, with tool 99305018, adjust valve seats according to the
values shown in Figure 85.
EXHAUST INTAKE
EXHAUSTINTAKE
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 37
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
50676
70334
770321
Figure 86
Figure 87
Figure 88
MAIN DATA TO CHECK INTAKE AND EXHAUST
VALVE SPRINGS
Before refitting use tool 99305047 to check spring flexibility.
Compare load and elastic deformation data with those of the
new springs shown in the following table.
FITTING CYLINDER HEAD
Lubricate the valve stems (1) and fit them into the relevant
valve guides according to the position marked at removal.
Fit the sealing rings (2 and 3) on the valve guide.
Position on the cylinder head: the spring (4), the upper cap
(3); use tool 99360268 (1) to compress the spring (4) and
lock the parts to the valve (5) by the cotters (2).
!
Sealing rings (2) for intake valves are yellow and
sealing rings (3) for exhaust valves are green.
VALVE SPRINGS
70333
Figure 89
After regrinding, check that valve (3) sinking value is the
specified one by using the base 99370415 (2) and the dial
gauge 99395603 (1).
38 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Height Under a load of
mm kg
H 47.75 Free
H135.33 P 339.8 ±19 N
H225.2 P1 741 ±39 N
Check cleanness of cylinder head and engine block coupling
surface.
Take care not to foul the cylinder head gasket.
Set the cylinder head gasket (1) with the marking “TOP” (1)
facing the head.
The arrow shows the point where the gasket thickness is
given.
70335
Figure 90
Refitting the cylinder head
!
Before re-utilising the fixing screws for the cylinder
head, verify there is no evidence of wear or
deformation and in that case replace them.
88775
Figure 91
There are two types of head seals for F4AE04.., F4AE06.. and
F4HE06.. engines, for the thickness (1.25 mm Type A and
1.15 mm Type B) take the following measures:
-for each piston detect, as indicated on NO TAG, at a
distance of 45 mm from the centre of the piston
overhandings S1 and S2 in relation to the engine base
upper plane then calculate the average:
For4cylinderversions:
Repeat the operation for pistons 2, 3 and 4 and calculate the
average value.
For6cylinderversions:
Repeat the operation for pistons 2, 3, 4, 5 and 6 and calculate
the average value.
If S is > 0,40 mm use seal type A.
If S is < 0,40 mm use seal type B.
S=Scil1 +Scil2 +Scil3 +Scil4 +Scil5 +Scil6
6
Scil1 =S1 +S2
2
S=Scil1 +Scil2 +Scil3 +Scil4
4
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 39
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
40 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
TIGHTENING TORQUE
C
O
M
P
O
N
E
N
T
TORQUE
C
O
M
P
O
N
E
N
T
Nm kgm
Studs M6 for camshaft sensors 8±2 0.8 ±0.2
Studs M8 for feed pump 12 ±2 1.2 ±0.2
Screw M12 for fastening rear gear case
Screw M10 for fastening rear gear case
Screw M8 for fastening rear gear case
77 ±12
47 ±5
24 ±4
7.7 ±1.2
4.7 ±0.5
2.4 ±0.4
Nut M6 for fastening camshaft sensor 10 ±2 1 ±0.2
Screw M8 for fastening oil pump 1st stage
2nd stage
8±1
24 ±4
0.8 ±0.1
2.4 ±0.4
Screw M8 for fastening front cover 24 ±4 2.4 ±0.4
Screw M8 for fastening camshaft longitudinal retaining plate 24 ±4 2.4 ±0.4
Screw M8 for fastening camshaft gear 36 ±4 3.6 ±0.4
Screw M10 for fastening crankcase plate 43 ±5 4.3 ±0.4
Nut M18 for fastening high pressure pump gear 105 ±5 10.5 ±0.5
Nuts M8 for fastening fuel pump 24 ±4 2.4 ±0.4
½inch plug on cylinder head
¼inch plug on cylinder head
¾inch plug on cylinder head
24 ±4
36 ±5
12 ±2
2.4 ±0.4
3.6 ±0.5
1.2 ±0.2
S
c
r
e
w
M
6
f
o
r
f
s
t
e
n
i
n
i
n
j
e
c
t
o
r
s
1st s
t
a
e
d
8.5 ±0.35 0.85 ±0.035
S
crew
M
6
f
or
f
as
t
en
i
ng
i
n
j
ec
t
ors
1
s
t
e
2nd stage 75º ±
Nut fastening for injector feed connector 50 ±5 5 ±0.5
Nut M6 for flame start grille on intake manifold 8±2 0.8 ±0.2
Screw M8 for fastening intake manifold 24 ±4 2.4 ±0.4
Screw M12 for fastening rear brackets for engine lifting 77 ±12 7.7 ±1.2
Screws M8 for fastening Common Rail 24 ±4 2.4 ±0.4
Connectors M14 for high pressure fuel pipes 20 ±2 2 ±0.2
Screw M12 (12 x 1.75 x 130) for fastening cylinder head
1
s
t
s
t
e
}
35 ±5 3.5 ±0.5
Screw M12 (12 x 1.75 x 150) for fastening cylinder head 1s
t
s
t
age
}
55 ±55.5±0.5
2nd stage 90º ±
3rd stage 90º ±
Screw for fastening rocker bracket 36 ±5 3.6 ±0.5
Valve clearance adjusting nuts 24 ±4 2.4 ±0.4
Nuts M14 for fastening fuel pipes from high pressure pump to Common Rail 20 ±2 2 ±0.2
Screw M8 for fastening high pressure pipe connector 24 ±4 2.4 ±0.4
Screw M6 for fastening wiring bulkhead 10 ±2 1 ±0.2
Screw M8 for fastening electric wiring support for injector feed 24 ±4 2.4 ±0.4
Nuts for fastening wiring on each injector 1.5 ±0.25 0.15 ±0.025
Screw M12 for fastening fuel filter bracket 77 ±8 7.7 ±0.8
Screw M8 for fastening fuel filter holder 24 ±4 2.4 ±0.4
Fuel filter contact + ¾turn
Screw M22 for fastening oil pressure relief valve on oil filter support 80 ±8 8 ±0.8
Screw M8 for radiator seal and oil filter support 24 ±4 2.4 ±0.4
Oil filter contact + ¾turn
11/8inchconnectiononfiltersupport for turbine lubrication 24 ±4 2.4 ±0.4
Nut M12 for fastening turbine lubrication pipe 10 ±2 1 ±0.2
Screw M10 for fastening engine coolant inlet connection 43 ±6 4.3 ±0.6
90°elbow fastening (if required) to engine coolant inlet connection 24 ±4 2.4 ±0.4
Pipe on cylinder head for compressor cooling 22 ±2 2.2 ±0.2
SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS 41
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
C
O
M
P
O
N
E
N
T
TORQUE
C
O
M
P
O
N
E
N
T
Nm kgm
Screw M6 for fastening engine coolant drain connector 10 ±2 1 ±0.2
Pin fastening on engine block for exhaust manifold 10 ±2 1 ±0.2
Screw M10 for fastening exhaust manifold on cylinder head 53 ±5 5.3 ±0.5
Screw M12
f
or
f
as
t
enin
dam
p
er ada
p
t
er 1st s
t
a
e50 ±5 5 ±0.5
S
c
r
e
w
M
1
2
f
o
r
f
s
t
e
n
i
n
d
m
p
e
r
d
p
t
e
r
1
s
t
e
and damper on output shaft 2nd stage 90º
Screw M10 for fastening pulley on output shaft 68 ±7 6.8 ±0.7
Screw M8 for fastening water pump 24 ±4 2.4 ±0.4
Screw M10 for fastening auxiliary component control belt tensioners 43 ±6 4.3 ±0.6
Screw M10 for fastening fixed pulleys for auxiliary component control belt 43 ±6 4.3 ±0.6
Screw M10 for fastening flywheel housing
Screw M12 for fastening flywheel housing
85 ±10
49 ±5
8.5 ±1
4.9 ±0.5
Screw M6 for fastening heat exchanger for control unit
Screw M8 for fastening heat exchanger for control unit
10 ±2
24 ±4
1±0.2
2.4 ±0.4
Connection M12 for fuel inlet-outlet on heat exchanger 12 ±2 1.2 ±0.2
Nut M8 for fastening valve cover 24 ±4 2.4 ±0.4
Screw M6 for fastening camshaft sensor 8±2 0.8 ±0.2
Screw M6 for fastening output shaft sensor 8±2 0.8 ±0.2
Screw M14 for fastening coolant temperature sensor 20 ±3 2 ±0.3
Screw M5 for fastening oil pressure/temperature sensor 6±1 0.6 ±0.1
Screw for fastening fuel pressure sensor 35 ±5 3.5 ±0.5
Screw M14 for fastening fuel temperature sensor 20 ±3 2 ±0.3
Screw for fastening air temperature/pressure sensor on intake manifold 6±1 0.6 ±0.1
Screw M12 for fastening engine oil level sensor 12 ±2 1.2 ±0.2
{
pins M8
t
M
8
6
-
c
y
l
.
7±1
4
3
±
6
0.7 ±0.1
4
3
±
0
6
Turbine fixing to exhaust manifold
{
nu
t
sM8
6
-
c
y
l
.
{
p
in
s
M
8
4
3
±
6
7
±
1
4
.
3
±
0
.
6
0
7
±
0
1
u
b
e
t
o
e
u
s
t
o
d
4-cyl.
{
p
i
n
s
M
8
nuts M8
7
±
1
24 ±4
0
.
7
±
0
.
1
2.4 ±0.4
Adapter M12 on turbine for lubricant oil pipes (inlet) 35 ±5 3.5 ±0.5
Pipe fixing on adapter M10 for turbine lubrication 35 ±5 3.5 ±0.5
Oil pipe fixing on adapter M10 for turbine lubrication to block 43 ±6 4.3 ±0.6
Oil drain pipe fixing M8 on turbine 24 ±4 2.4 ±0.4
Connector fixing M6 for oil return from cylinder head to flywheel housing 10 ±2 1 ±0.2
Screw M12 for fastening engine flywheel 1st stage
d
30 ±4 3 ±0.4
S
c
r
e
w
M
1
2
f
o
r
f
s
t
e
n
i
n
e
n
i
n
e
f
l
y
w
h
e
e
l
1
s
t
e
2nd stage 60º ±
Screw M8 for fastening front bracket for engine lifting 24 ±4 2.4 ±0.4
Screw for fastening engine oil sump 24 ±4 2.4 ±0.4
Screw M8 for fastening cylinder barrel lubricating nozzles 15 ±3 1.5 ±0.3
Screw M12 for fastening output shaft caps 1st stage
2nd stage
d
50 ±6
80 ±6
5±0.6
8±0.6
2
s
t
e
3rd stage 90º ±
Screw M8 for fastening camshaft longitudinal retaining plate 24 ±4 2.4 ±0.4
Screw M8 for fastening camshaft gear 36 ±4 3.6 ±0.4
Screw M11 for fastening connecting rod caps 1st stage
d
60 ±5 6 ±0.5
S
c
r
e
w
M
1
1
f
o
r
f
s
t
e
n
i
n
c
o
n
n
e
c
t
i
n
r
o
d
c
p
s
1
s
t
e
2nd stage 60º ±
Alternator
M10 Screw, Bracket fixing on water feed pipefitting 43 ±6 4.3 ±0.6
M10 Screw, alternator locking 43 ±6 4.3 ±0.6
Starter
Starter fixing screw 43 ±6 4.3 ±0.6
42 SECTION 4 - OVERHAUL AND TECHNICAL SPECIFICATIONS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
SECTION 5 - TOOLS 1
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
SECTION 5
Tools
Page
TOOLS 3................................
2SECTION 5 - TOOLS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
SECTION 5 - TOOLS 3
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99305018 Kit for valve seat regrinding
99305047 Spring load tester
99305453 Tool to check the diesel supply circuit and the common-rail injection
system
99317915 Set of 3 pin wrenches (14 - 17 - 19 mm)
99322205 Revolving stand for overhauling units (700 daN/m capacity, 120
daN/m torque)
99331052 Adapter for measures on engine injectors (use with 99395872)
4SECTION 5 - TOOLS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99340055 Tool to remove output shaft front gasket
99340056 Tool to remove output shaft rear gasket
99341001 Double acting puller
99341009 Pair of brackets
99341015 Press
99342101 Tool to remove injectors
SECTION 5 - TOOLS 5
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99346252 Tool for fitting output shaft front gasket
99346253 Tool for fitting output shaft rear gasket
99360076 Tool to remove oil filter (engine)
99360183 Pliers for removing/refitting piston rings (65 — 110 mm)
99360268 Tool for removing/refitting engine valves
99360292 Keying device for seal assembly on the valve guide
6SECTION 5 - TOOLS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99360339 Tool for rotating/stopping the engine flywheel
99360351 Equipment for flywheel holding
99360362 Beater for removing/refitting camshaft bushes (to be used with
993700069)
99360500 Tool for lifting the output shaft
99360595 Lifting rig for engine removal/refitting
99360605 Band for fitting piston into cylinder barrel (60 — 125 mm)
SECTION 5 - TOOLS 7
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99361037 Brackets for fastening engine to revolving stand 99322205
99363204 Tool to remove gaskets
99367121 Manual pump for pressure and depression measures
99370006 Handgrip for interchangeable beaters
99370415 Gauge base for different measurements (to be used with 99395603)
99389829 Dog type dynamometric wrench 9x12 (5-60 Nm)
8SECTION 5 - TOOLS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99389834 Torque screwdriver for injector solenoid valve connector stop nut
setting
99395216 Pair of gauges with ½”and¾” square head for angle tightening
99395220 Universal goniometer/inclinometer
99395363 Complete bush testing square
99395603 Dial gauge (0 — 5 mm)
99395872
Analog to digital multimeter for voltage, current intensity, resistance,
diodes, frequencies, capacity and registration of the minimum, average
and maximum values
SECTION 5 - TOOLS 9
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
8093731 Tester PT01
10 SECTION 5 - TOOLS F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
APPENDIX 1
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
Appendix
Page
SAFETY PRESCRIPTIONS 3..................
-Standard safety prescriptions 3..............
-Prevention of injury 3.....................
-During maintenance 3.....................
-Respect of the Environment 4...............
2APPENDIX F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
Particular attention shall be drawn on some precautions that
must be followed absolutely in a standard working area and
whose non fulfillment will make any other measure useless
or not sufficient to ensure safety to the personnel in-charge
of maintenance.
Be informed and inform personnel as well of the laws in force
regulating safety, providing information documentation
available for consultation.
-Keep working areas as clean as possible, ensuring
adequate aeration.
-Ensure that working areas are provided with emergency
boxes, that must be clearly visible and always provided
with adequate sanitary equipment.
-Provide for adequate fire extinguishing means, properly
indicated and always having free access. Their efficiency
must be checked on regular basis and the personnel
must be trained on intervention methods and priorities.
-Organize and displace specific exit points to evacuate
the areas in case of emergency, providing for adequate
indications of the emergency exit lines.
-Smoking in working areas subject to fire danger must be
strictly prohibited.
-Provide Warnings throughout adequate boards signaling
danger, prohibitions and indications to ensure easy
comprehension of the instructions even in case of
emergency.
-Do no
t
execu
t
ean
y
in
t
erven
t
ion i
f
no
t
pro
ided
w
i
t
h
necessary instructions.
-Do not use any tool or equipment for any different
operation from the ones they’ve been designed and
provided for: serious injury may occur.
-In case of test or calibration operations requiring engine
running, ensure that the area is sufficiently aerated or
utilize specific vacuum equipment to eliminate exhaust
gas. Danger: poisoning and death.
SAFET
Y
PRESCRIPTIONS
Standard safety prescriptions
Prevention of injury
-Do not wear unsuitable cloths for work, with fluttering
ends, nor jewels such as rings and chains when working
close to engines and equipment in motion.
-Wear safety gloves and goggles when performing the
following operations:
- filling inhibitors or anti-frost
- lubrication oil topping or replacement
- utilization of compressed air or liquids under pressure
(pressure allowed: 2 bar).
-Wear safety helmet when working close to hanging
loads or equipment working at head height level.
-Always wear safety shoes when and cloths adhering to
the body, better if provided with elastics at the ends.
-Use protection cream for hands.
-Change wet cloths as soon as possible
-In presence of current tension exceeding 48-60 V verify
efficiency of earth and mass electrical connections.
Ensure that hands and feet are dry and execute working
operations utilizing isolating foot-boards. Do not carry
out working operations if not trained for.
-Do not smoke nor light up flames close to batteries and
to any fuel material.
-Put the dirty rags with oil, diesel fuel or solvents in
anti-fire specially provided containers.
During maintenance
-Never open filler cap of cooling circuit when the engine
is hot. Operating pressure would provoke high
temperature with serious danger and risk of burn. Wait
unit the temperature decreases under 50 °C.
-Never top up an overheated engine with cooler and
utilize only appropriate liquids.
-Always operate when the engine is turned off: whether
particular circumstances require maintenance
intervention on running engine, be aware of all risks
involved with such operation.
-Be equipped with adequate and safe containers for
drainage operation of engine liquids and exhaust oil.
-Keep the engine clean from oil tangles, diesel fuel and or
chemical solvents.
-Use of solvents or detergents during maintenance may
originate toxic vapors. Always keep working areas
aerated. Whenever necessary wear safety mask.
-Do not leave rags impregnated with flammable
substances close to the engine.
-Upon engine start after maintenance, undertake proper
preventing actions to stop air suction in case of runaway
speed rate.
-Do not utilize fast screw-tightening tools.
-Never disconnect batteries when the engine is running.
-Disconnect batteries before any intervention on the
electrical system.
-Disconnect batteries from system aboard to load them
with the battery loader.
-After every intervention, verify that battery clamp
polarity is correct and that the clamps are tight and safe
from accidental short circuit and oxidation.
-Do not disconnect and connect electrical connections
in presence of electrical feed.
-Before proceeding with pipelines disassembly
(pneumatic, hydraulic, fuel pipes) verify presence of liquid
or air under pressure. Take all necessary precautions
bleeding and draining residual pressure or closing dump
valves. Always wear adequate safety mask or goggles.
Non fulfillment of these prescriptions may cause serious
injury and poisoning.
APPENDIX 3
F4HE NEF ENGINES
Print P2D32N003GB Base - February 2006
-Avoid incorrec
t
t
igh
t
ening or ou
t
o
f
couple. Danger:
incorrect tightening may seriously damage engine’s
components, affecting engine’s duration.
-Avoid priming from fuel tanks made out of copper alloys
and/or with ducts not being provided with filters.
-Do not modify cable wires: their length shall not be
changed.
-Do not connect any user to the engine electrical
equipment unless specifically approved by Iveco.
-Do not modify fuel systems or hydraulic system unless
Iveco specific approval has been released. Any
unauthorized modification will compromise warranty
assistance and furthermore may affect engine correct
working and duration.
For engines equipped with electronic gearbox:
-Do not execute electric arc welding without having
priory removed electronic gearbox.
-Remove electronic gearbox in case of any intervention
requiring heating over 80 °C temperature.
-Do not paint the components and the electronic
connections.
-Do not vary or alter any data filed in the electronic
gearbox driving the engine. Any manipulation or
alteration of electronic components shall totally
compromise engine assistance warranty and
furthermore may affect engine correct working and
duration.
-Respect of the Environment shall be of primary
importance: all necessary precautions to ensure
personnel’s safety and health shall be adopted.
-Be informed and inform the personnel as well of laws in
force regulating use and exhaust of liquids and engine
exhaust oil. Provide for adequate board indications and
organize specific training courses to ensure that
personnel is fully aware of such law prescriptions and of
basic preventive safety measures.
-Collect exhaust oils in adequate specially provided
containers with hermetic sealing ensuring that storage is
made in specific, properly identified areas that shall be
aerated, far from heat sources and not exposed to fire
danger.
-Handle the batteries with care, storing them in aerated
environment and within anti-acid containers. Warning:
battery exhalation represent serious danger of
intoxication and environment contamination.
Res
p
ect of the Envi
r
onment
4APPENDIX F4HE NEF ENGINES
Base - February 2006 Print P2D32N00GB
1
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
Part 2
G-DRIVE APPLICATION ENGINES
Section 1 - General specifications
Page
CORRESPONDENCE BETWEEN TECHNICAL CODE
AND COMMERCIAL CODE 7.............
COOLING SYSTEM 8......................
AIR INDUCTION - BOOST DIAGRAM 9.......
-Description 9............................
OIL VAPOUR RECYCLING 10................
Section 2 - G-Drive application
GENERAL SPECIFICATIONS 11...............
CLEARANCE DATA 13......................
REMOVING AND REFITTING ENGINE
FROM RADIATOR 19.....................
-Removal 19..............................
-Refitting 19..............................
TOOLS 20................................
!
Part 2 describes a specific industrial application: G-Drive engines.
These engines are marketed as an assembly that is also equipped with the air/coolant and possibly air/air (intercooler)
cooling device.
The description of this application gives the differences with the industrial application (given in the preceding Parts) and
reference must be made to it for all repair and maintenance work.
2G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Diagrams and symbols have been widely used to give a clearer and more immediate illustration of the subject being dealt with, (see
next page) instead of giving descriptions of some operations or procedures.
Example
Ø 1 = housing for connecting rod small end bush
Ø 2 = housing for connecting rod bearings
α
Tighten to torque
Tighten to torque + angular value
1
2
3
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
SPECIAL REMARKS
4G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
SYMBOLS - ASSISTANCE OPERATIONS
Removal
Disconnection Intake
Refitting
Connection Exhaust
Removal
Disassembly Operation
Fitting in place
Assembly ρCompression ratio
Tighten to torque Tolerance
Weight difference
α
Tighten to torque + angle value Rolling torque
Press or caulk Rotation
Regulation
Adjustment
Angle
Angular value
Visual inspection
Fitting position check Preload
Measurement
Value to find
Check
Number of revolutions
Equipment Temperature
Surface for machining
Machine finish bar Pressure
Interference
Strained assembly
Oversized
Higher than.
Maximum, peak
Thickness
Clearance
Undersized
Less than.
Minimum
Lubrication
Damp
Grease
Selection
Classes
Oversizing
Sealant
Adhesive
Temperature < 0 °C
Cold
Winter
Air bleeding
Temperature > 0 °C
Hot
Summer
Replacement
Original spare parts
5
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
UPDATING
Section Description Page Date of revision
6G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
CORRESPONDENCE BETWEEN TECHNICAL CODE AND COMMERCIAL CODE
SECTION 1 - GENERAL SPECIFICATIONS 7
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
Technical Code Commercial Code
F4HE9685A*J100 -
Figure 1
106529
Water leaving the thermostat
Coolant recirculating in the engine
Water entering the pump
DIAGRAM OF THE COOLING SYSTEM
COOLING SYSTEM
The engine cooling system, closed circuit forced circulation
type, generally incorporates the following components:
-Expansion tank; placement, shape and dimensions are
subject to change according to the engine’s equipment.
-Radiator, which has the duty to dissipate the heat
subtracted to the engine by the cooling liquid. Also this
component will have specific peculiarities based on the
equipment developed, both for what concerns the
placement and the dimensions.
-Viscous pusher fan, having the duty to increase the heat
dissipating power of the radiator. This component as well
will be specifically equipped based on the engine’s
development.
-Heat exchanger to cool the lubrication oil: even this
component is part of the engine’s specific equipment.
-Centrifugal water pump, placed in the front part of the
engine block.
-Thermostat regulating the circulation of the cooling liquid.
-The circuit may eventually be extended to the
compressor,ifthisisincludedintheequipment.
8SECTION 1 - GENERAL SPECIFICATIONS G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Figure 2
AIR INDUCTION - BOOST DIAGRAM
Description
The turbocharger is composed by the following main parts:
one turbine, one transforming valve to regulate the boost
feeding pressure , one main body and one compressor.
During engine working process, the exhaust emissions flow
through the body of the turbine, causing the turbine disk
wheel’s rotation.
The compressor rotor, being connected by shaft to the
turbine disk wheel, rotates as long as this last one rotates,
compressing the drawn air through the air filter.
The above mentioned air is then cooled by the radiator and
flown through the piston induction collector.
The turbocharger is equipped with a transforming valve to
regulate the pressure , that is located on the exhaust collector
before the turbine and connected by piping to the induction
collector.
It’s funchon is to restrict the exhaust of the emissions , releasing
part of them directly to the exhaust tube when the boost
feeding pressure, over the compressor, reaches the
prescribed bar value.
The cooling process and the lubrication of the turbocharger
and of the bearings is made by the oil of the engine.
106548
Compressed air to the heat exchanger
Refrigerated compressed air to the pistons
Exhaust gas
Intake air
TURBOCHARGING DIAGRAM
SECTION 1 - GENERAL SPECIFICATIONS 9
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
Figure 3
1. Pre-separator - 2. Exhaust to the outside (temporary) - 3. Filter - 4. Return to engine.
The tappet cover houses the pre-separator (1), whose shape and position determines an increase in oil vapour outlet speed and
condenses a part of vapours at the same time.
Condensate oil returns to the oil sump whereas the residual vapours are ducted, collected and filtered in the blow-by (3).
In the blow-by (3), part of the vapours condense and return to the oil sump whereas the remaining part is put into cycle again
through pipe (2).
Oil condensate
Oil vapours
OIL VAPOUR RECYCLING
108729
10 SECTION 1 - GENERAL SPECIFICATIONS G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
SECTION 2 - G-DRIVE APPLICATION 11
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
GENERAL SPECIFICATIONS
Type FAHE9685A
Cycle Four-stroke diesel engine
Power Supercharged with intercooler
Injection Direct
Number of cylinders 6
Bore mm 104
Stroke mm 132
+++..=
Total displacement cm36728
TIMING
start before T.D.C. A
end after B.D.C. B
18.5º
29.5º
start before B.D.C. D
end after T.D.C. C
67º
35º
X
Checking timing
mm
X
mm
Checking operation
mm
X
mm
-
-
0.20 to 0.30
0.45 to 0.55
FUEL FEED
Injection
Type: Bosch
high pressure common rail
EDC7 ECU
Nozzle type Injectors
Injection sequence 1-5-3-6-2 -4
bar
Injection pressure bar 250 ÷1450
!
Data, features and performances are valid only if the technician fully complies with all the installation requirements provided
by Iveco Motors.
Furthermore, the use of the unit after overhaul showd conform to the original specified power and engine rev/min for
which the engine has been designed.
12 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Clearance data - 6 cyl.
F
A
H
E
9
6
8
5
A
Type
F
A
H
E
9
6
8
5
A
ρCompression ratio 17 : 1
Max. output kW
(HP)
rpm
215
292
1800
Max. torque Nm
(kgm)
rpm
-
-
-
Loadless en
g
ine
idling rpm -
Loadless engine
peak rpm rpm -
Bo
r
e
x
s
t
r
oke
Displacement
104 x 132
6728
TURBOCHARGING
Turbocharger type
with intercooler
HOLSET HX35W
bar
LUBRICATION
Oil pressure (warm engine)
- idling bar
Forced by gear pump, relief valve single action
oil filter
-peakrpm bar 2
4
COOLING
Water pump control
Thermostat
-startofopening ºC
By liquid
Through belt
81 ±2
15W40 ACEA E3
FILLING
engine sump liters
engine sump + filter liters
15
15 + 1
SECTION 2 - G-DRIVE APPLICATION 13
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
CLEARANCE DATA
Type 6 CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
1
X
Cylinder barrels 1103.99 to 104.010
L
Cylinder barrels:
outside diameter 2
length L
-
-
Cylinder barrels — housings on
engine block (interference) -
Outside diameter 20.5
3
XCylinder barrels:
inside diameter 2-
1
X
2
Spare pistons
type:
Size X
Outside diameter 1
Pin housing 2
12
103.851 to 103.865
40.00 to 40.25
Piston — cylinder barrels 0.113 to 0.147
Piston diameter 10.5
X
Piston protrusion X 0.28 to 0.52
3
Piston pin 337.994 to 38
Piston pin — pin housing 0.0006 to 0.0202
14 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Type 6 CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
X
1
3
2
X
X
X1*
Split ring slots X 2
X3
*measuredon99mm
3
2.42 to 2.44
4.03 to 4.05
1
3
2
S
S
S
S1*
Split rings S 2
S3
3
2.350 to 2.380
4.030 to 4.050
1
Split rings - slots 2
3
0.100 to 0.175
0.040 to 0.90
0.020 to 0.065
Split rings 0.5
X1
3
2
X
X
Split ring end opening
in cylinder barrel:
X1
X2
X3
0.30 to 0.40
0.60 to 0.80
0.3 to 0.55
1
2
Small end bush
housing 1
Big end bearing
housing 2
42.987 to 43.013
72.987 to 73.013
S
4
3Small end bush diameter
Outside 4
Inside 3
Spare big end half
bearings S
40.987 to 41.013
38.019 to 38.033
1.955 to 1.968
Small end bush — housing 0.266 to 0.566
Piston pin — bush 0.0188 to 0.0372
Big end half bearings 0.250; 0.500; 0.750; 1.000
SECTION 2 - G-DRIVE APPLICATION 15
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
Type 6 CYLINDERS
CYLINDER UNIT AND CRANKSHAFT COMPONENTS mm
X
Size X
Max. tolerance
on connecting rod
axis alignment
-
-
12
S1S2
Journals 1
Crankpins 2
Main half bearings S 1
Big end half bearings S 2
*provided as spare part
82.99 to 83.01
73.533 to 74.513
2.456 to 2.464
1.955 to 1.968
3
Main bearings
No. 1—7 3
No. 2—3—4—5—6 3
87.982 to 88.008
87.977 to 88.013
Half bearings — Journals
No. 1—7
No. 2—3—4—5—6
0.044 to 0.106
0.039 to 0.111
Half bearings - Crankpins 0.038 to 0.116
Main half bearings
Big end half bearings +0.250; +0.500; +0.750; +1.000
1
X
Shoulder journal X 1 37.28 to 37.38
X 2
Shoulder main bearing X 2 28.77 to 29.03
X3 Shoulder half-rings X 3 37.28 to 37.38
Output shaft shoulder 0.095 to 0.265
16 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Type 6 CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
1
Valve guide seats on
cylinder head 17.042 to 7.062
2
3
2
Valve guides
3
-
-
Valveguidesandseatsonhead -
Valve guides -
α
4Valves:
4
α
4
α
6.970 to 6.999
60 ±0.25°
6.970 to 6.999
45 ±0.25°
Valve stem and guide 0.043 to 0.092
1
Housing on head for
valve seat:
1
1
34.837 to 34.863
34.837 to 34.863
α
2
Val
v
esea
t
ou
t
side diame
t
e
r
;
valve seat angle on cylinder
head:
2
α
2
α
34.917 to 34.931
60°
34.917 to 34.931
45°
X
X
Sinking X
0.59 to 1.11
0.96 to 1.48
Between valve seat
and head
0.054 to 0.094
0.054 to 0.094
Valve seats -
SECTION 2 - G-DRIVE APPLICATION 17
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
Type 6 CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
HH1 H2
Valve spring height:
free spring H
under a load equal to:
339.8 ±9N H1
741 ±39 N H2
47.75
35.33
25.2
X
Injector protrusion X -
123 4 5
Camshaft bush
housings No. 1
Camshaft housings
No. 2-3-4-5-6-7
59.222 to 59.248
54.089 to 54.139
1
2
3
Camshaft journals:
1754.005 to 54.035
Camshaft bush outside
diameter: -
Bush inside
diameter 54.083 to 54.147
Bushes and housings
on block -
Bushes and journals 0.038 to 0.162
H
Cam lift:
H
H
6.045
7.582
18 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
Type 6 CYLINDERS
CYLINDER HEAD — TIMING SYSTEM mm
1
Tappet cap housing
on block 116.000 to 16.030
2
3
2
Tappet cap outside
diameter: 2
3
15.924 to 15.954
15.960 to 15.975
Between tappets and housings 0.025 to 0.070
Tappets -
1
Rocker shaft 121.965 to 21.977
2
Rockers 222.001 to 22.027
Between rockers and shaft 0.024 to 0.162
Figure 4
Removal
Remove the fan safety grilles (5) by undoing the relevant
fasteners.
Placeacontainerunderthepipe(12)tocollectthecoolant.
Disconnect and remove the pipe (12) together with the
sleeves by undoing the clamps.
Disconnect the air pipes (4) and (15) from the air exchanger
and from the engine, then remove it from its seat. Disconnect
the exhaust pipe (14) from the system.
Disconnect and remove the coolant pipes (1) and (2).
Block the radiator assembly (3) appropriately, then detach it
from the crankcase by undoing the fasteners (6) on both
sides.
Remove the radiator assembly from its seat, taking care over
any interference with the fan.
108598
Check the state of wear of the rubber couplings.
REMOVING AND REFITTING ENGINE FROM RADIATOR
Disconnect the air hose (9) from air filter (10) to the turbine
(8).
Remove the air cleaner (10) by undoing the fasteners (7) and
remove it from its seat together with the support (11).
Refitting
Proceed by reversing the operations described for removal;
restore the coolant system.
NOTE
SECTION 2 - G-DRIVE APPLICATION 19
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
20 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99305018 Kit for valve seat regrinding
99305047 Spring load tester
99305453 Tool to check the diesel supply circuit and the common-rail injection
system
99317915 Set of 3 pin wrenches (14 - 17 - 19 mm)
99322205 Revolving stand for overhauling units (700 daN/m capacity, 120
daN/m torque)
99331052 Adapter for measures on engine injectors (use with 99395872)
SECTION 2 - G-DRIVE APPLICATION 21
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99340055 Tool to remove output shaft front gasket
99340056 Tool to remove output shaft rear gasket
99341001 Double acting puller
99341009 Pair of brackets
99341015 Press
99342101 Tool to remove injectors
22 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99346252 Tool for fitting output shaft front gasket
99346253 Tool for fitting output shaft rear gasket
99360076 Tool to remove oil filter (engine)
99360183 Pliers for removing/refitting piston rings (65 — 110 mm)
99360268 Tool for removing/refitting engine valves
99360292 Keying device for seal assembly on the valve guide
SECTION 2 - G-DRIVE APPLICATION 23
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99360339 Tool for rotating/stopping the engine flywheel
99360351 Equipment for flywheel holding
99360362 Beater for removing/refitting camshaft bushes (to be used with
993700069)
99360500 Tool for lifting the output shaft
99360595 Lifting rig for engine removal/refitting
99360605 Band for fitting piston into cylinder barrel (60 — 125 mm)
24 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
99361037 Brackets for fastening engine to revolving stand 99322205
99363204 Tool to remove gaskets
99367121 Manual pump for pressure and depression measures
99370006 Handgrip for interchangeable beaters
99370415 Gauge base for different measurements (to be used with 99395603)
99389829 Dog type dynamometric wrench 9x12 (5-60 Nm)
SECTION 2 - G-DRIVE APPLICATION 25
G-DRIVE ENGINES
Print P2D32N003GB Base - February 2006
TOOLS
TOOL NO. DESCRIPTION
99389834 Torque screwdriver for injector solenoid valve connector stop nut
setting
99395216 Pair of gauges with ½”and¾” square head for angle tightening
99395220 Universal goniometer/inclinometer
99395363 Complete bush testing square
99395603 Dial gauge (0 — 5 mm)
99395872
Analog to digital multimeter for voltage, current intensity, resistance,
diodes, frequencies, capacity and registration of the minimum,
average and maximum values
26 SECTION 2 - G-DRIVE APPLICATION G-DRIVE ENGINES
Base - February 2006 Print P2D32N00GB
TOOLS
TOOL NO. DESCRIPTION
8093731 Tester PT01

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