Iveco S30 Ent M23 Users Manual

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SOFIM
S30 ENT M23
4 CYLINDERS IN LINE
DIESEL CYCLE
FOR MARINE APPLICATIONS
INSTALLATION DIRECTIVE
MAY 2006 EDITION
TECHNOLOGICAL EXCELLENC E
INSTALLATION DIRECTIVE
2MAY 2006
S30 ENT M23
FOREWORD
We strongly recommend that you carefully read the indica-
tions contained in this document: compliance with them
protects the engine against irregular operation and assures
its reliability, safeguarding sea-going and maintenance person-
nel against accident hazards.
The indications contained in this directive pertain to the S30
ENT M23 engines and complement the IVECO MOTORS
publication “Guide to the Installation of Marine Engines” the
reader should refer to, for anything that is not explained
herein.
For more complete information about the engine, please
refer to the appropriate technical brochure.
Use of fuels and oils with different characteristics from
those set out in the operation and maintenance manual may
compromise the regular operation of the engine, limiting its
performance, reliability and working life.
Exclusive use of IVECO Original Parts is a necessary condi-
tion to maintain the engine in its original integrity.
Tampering, making modifications and using non original parts
can jeopardize the safety of boat engineers and users.
To obtain spare parts, you must indicate:
- Commercial code, serial number and indications shown
on the engine tag;
- Part number of the spare as per spare part catalog.
The information provided below refer to engine characteris-
tics that are current as of the publication date.
IVECO MOTORS reserves the right to make modifications
at any time and without advance notice, to meet technical or
commercial requirements or to comply with local legal and
regulatory requirements.
We refuse all liability
for any errors
and omissions.
The reader is reminded that the IVECO MOTORS Technical
Assistance Network is always at the Customer’s side with its
competence and professionalism.
Publication IVECO MOTORS edited by:
IVECO PowerTrain
Advertising & Promotion
Pregnana Milanese (MI)
www.ivecomotors.com
Printed P3D64S001 E - May 2006 Edition
INSTALLATION DIRECTIVE 3
MAY 2006 S30 ENT M23
CONTENTS
Page
1. WARNINGS AND CAUTIONS 4
2. ENGINE PARTS AND COMPONENTS 6
3. INSTALLATION OVERVIEW 8
4. GENERAL INSTALLATION CRITERIA 9
5. TECHNICAL DATA FOR INSTALLATION 10
6. IDENTIFICATION DATA 12
7. COMPONENTS SUPPLIED WITH THE ENGINE 13
8. FUEL LINE 14
9. ELECTRICAL EQUIPMENT 17
10. MAIN ANALOG INSTRUMENT PANEL 26
11. SECONDARY ANALOG INSTRUMENT PANEL 30
12. DRILLING PLANS FOR ANALOG PANELS 31
13. CUSTOMIZED INSTRUMENT PANEL 32
14. SENSORS FOR DETECTION
AND PANEL SIGNALING 34
15. PREPARING THE ENGINE
FOR FIRST START-UP 36
16. TESTS BEFORE THE FIRST START-UP 36
17. FIRST ENGINE START 37
18. EDC ANOMALIES INDICATION 38
19. BLINK CODE TABLE 39
20. UNDERWAY CHECKS 41
21. PREPARING THE ENGINE
FOR LONG IDLE PERIODS 42
22. WIRING DIAGRAMS 43
INSTALLATION DIRECTIVE
4MAY 2006
S30 ENT M23
To obtain the best engine performance, it is essential not to
deviate from the mission profile for which it was produced
and set up. The engine must not be used for purposes other
than those stated by the manufacturer. IVECO MOTORS
is willing to examine any need for particular installations
beforehand. Use of an electronically controlled injection
system, in providing the engine with performance benefits,
requires that the installer and maintenance specialist comply
with some fundamental rules, which will become more and
more commonplace as use of such equipment becomes
progressively more widespread. Boat outfitters and mainte-
nance specialists are invited to closely follow the instructions
contained herein. No modifications to the engine, its acces-
sories and components, are allowed.
Failure to comply with the instructions that follow shall
void the warranty and relieve IVECO MOTORS of all
liabilities.
For personnel safety
Specialists and installers are cautioned to comply with
workplace safety rules and to adopt prescribed individual
protection devices when working.
o Drain the cooling, lubrication and fuel lines only after
the fluids have duly cooled. The pressurized cap of the
water line may be opened only after the engine has duly
cooled.
o Batteries contain a highly corrosive sulfuric acid solution:
must never be upset and must be handled with the
utmost caution to prevent spillage. Ensure that the bat-
tery compartment is adequately ventilated.
Handling
The engine must be handled by experienced personnel,
using the prescribed tool or a rocker arm that keeps the
lifting lines parallel and with adequate equipment in terms
of capacity and size. The two eyebolts provided for lifting the
engine alone must always be used simultaneously.
Installation
o Knife switches or battery breakers may be used on the
power supply line of the engine electronic unit, provided
they are not used to shut the engine off.
o Do not modify the wiring harnesses; their length may
not be modified: use only available extensions.
o Do not use electronic device wiring harnesses not com-
pliant with the IVECO MOTORS directive, in terms of
length, type of conductor, location, clamping, connection
of the shielding and earth braids.
o To avoid any interference, the wiring harnesses of the
different on-board electronic devices must follow differ-
ent paths from those of the engine electronic systems.
o Do not connect any extraneous user device to the
engine electrical equipment.
o Do not place voltage across the boat’s on-board electri-
cal system without first verifying that there are no short
circuits.
o Do not branch pipes off to draw fuel from the engine
supply lines.
o Do not make any change to the engine’s hydraulic cir-
cuits and components.
o Do not execute arc welding operations before removing
the electronic units from their seating, placing them at an
adequate safety distance.
o Do not subject electronic units to temperatures exceed-
ing 80 °C.
o Do not paint electrical components and their connec-
tions.
o Do not alter the data contained in the engine control
electronic unit.
o Comply with prescribed procedures and torque values
when tightening threaded elements.
Start-up
o Ready the engine following the procedure set out in
Chapter 15.
o When starting the engine the first time, have suitable
means available to cut off air intake in case of a runaway
condition.
o Start the engine after ensuring that it is complete with
every part specified by the manufacturer and required
by the installation, without attempting to start it with
caps and occlusions to the lubrication, cooling and fuel
feed lines.
o Check that the fluid lines are perfectly sealed, especially
lines for fuels and lubricants, which may cause fires and
consequent harm to persons and equipment.
o Make sure that the various pipelines are not in contact
with warm surfaces or moving parts.
o The installing yard is required to carry out tests to verify
the functional compatibility between the electrical-elec-
tronic equipment of the engine and the other electronic
equipment present on the boat.
Tests and tuning up
o Never disconnect the batteries when the engine is
running.
o Remove the electrical connections from the batteries
before any operation on the electrical system.
o Ensure that the battery terminals comply with the exact
polarity, are properly tightened and protected against
accidental short circuits and corrosion phenomena.
o Do not connect or disconnect electrical connections
when electrical power supply is present.
1. WARNINGS AND CAUTIONS
INSTALLATION DIRECTIVE 5
MAY 2006 S30 ENT M23
o Do not cause sparks in the attempt to verify the pres-
ence of electrical voltage.
o Do not draw fuel through unfiltered lines.
o Do not clean the engine and its parts with corrosive or
abrasive detergent substances, to avoid compromising
the integrity of electrical connections.
o The engine fluids and air, water, and oil filters discarded
after use must be properly stored and delivered to
appropriate collection centers.
Long engine inactivity periods
Before long periods of inactivity, ready the engine following
the procedure set out in Chapter 21.
INSTALLATION DIRECTIVE
6MAY 2006
S30 ENT M23
2. ENGINE PARTS AND COMPONENTS
Figure 1
1. Engine coolant discharge cap - 2. Electric starter motor - 3. Tube bundle engine coolant/sea water heat exchanger - 4. Exhaust gas
and sea water discharge pipeline - 5. Engine coolant tank - 6. Coolant refill cap - 7. Lifting eyebolts - 8. Oil refill cap - 9. Sea water
pump actuation pulley - 10. Auxiliary belt automatic tensioner - 11. Alternator - 12. Location of sacrificial anode.
12
11
2
3
4
7 8 7
9
05_003_S
65
10
1
INSTALLATION DIRECTIVE 7
MAY 2006 S30 ENT M23
Figure 2
1. Engine coolant discharge cap location - 2. Combustion air filter - 3. Sacrificial anode - 4. Throttle potentiometer - 5. Combustion
air-sea water heat exchanger - 6. Oil dipstick - 7. Location of common rail high pressure injection pump - 8. Sea water pump - 9. Sea
water inlet - 10. Manual lubricating oil extraction pump - 11. Oil vapor separator - 12. Lubricating oil filters -
13. Common rail distributor - 14. Waste-gate actuator - 15. Cooled turbocharger - 16. Sea water junction pipe from after-cooler to
engine coolant/sea water heat exchanger.
6
12 13
17
05_002_S
23
16
17
15
4
8
7
9
11
5
10
1
14
INSTALLATION DIRECTIVE
8MAY 2006
S30 ENT M23
The figure shows the set of components of an installation,
including those supplied with the engine equipment, standard
or optional, and those supplied or produced by the yard.
It provides a comprehensive picture of the operations
required to install the engine.
Components arrangement and illustrations are not binding
but merely indicative, subject to the choices made by yard
engineers according to their skills, available spaces and the
prescriptions set out herein.
3. INSTALLATION OVERVIEW
1. Indicator and control panel - 2. Electrical panel with relay box and EDC electronic unit - 3. Exhaust gas and sea water discharge -
4. Filtered sea water intake - 5. Decanter filter - 6. Fuel feed pipe to the high pressure pump - 7. Fuel electric pump - 8. Fuel pre-
filter - 9. Fuel filter - 10. Fuel priming pipe - 11. Fuel return pipe to the tank - 12. Accelerator Bowden cable - 13. Accelerator lever.
Figure 3
1 2
45678
3
12
06_005_S
11
10
13
9
10
INSTALLATION DIRECTIVE 9
MAY 2006 S30 ENT M23
4. GENERAL INSTALLATION CRITERIA
Accessibility
The engine must be located in such a way as to allow filling
and draining engine liquids when doing servicing operations.
Anchoring
If anchoring is accomplished by interposing shock mounts,
they must be able to support the engine’s mass and the lon-
gitudinal thrust exerted by the propeller shaft in motion.
If rigid mounting is adopted, particular care must be given to
support alignment and co-planarity.
Information on dimensions and fastening values are provided
in the “Installation Diagram”.
Combustion and ventilation air
Compliance with prescriptions on the quantity of air
required for combustion and ventilation assures a regular
operation of the engine even in adverse conditions and it
enables to deliver its maximum design power (1).
Sea water line
It must be provided with an intake capable of preventing
the entry of foreign bodies into the suction pipes. Between
the intake and the pump, it is best to interpose a gate to be
closed in emergencies or for extended idle periods and a
filter to stop the smaller impurities; it is also recommended
to install a suitably dimensioned and easily replaced zinc
anode.
The engine sea water line was provided by the manufacturer
with protection anodes to be replaced periodically.
The rubber hoses positioned along the pipeline shall be suffi-
ciently rigid not to create choked areas caused by crushing (1).
Engine pre-heating
If the engine usage profile requires immediate delivery of
power at the highest rpm’s, it is recommended to install an
auxiliary pre-heater on the closed cooling loop.
Exhaust gas discharge
The exhaust gas discharge conduit shall be compliant with
the guidelines contained in the IVECO MOTORS publication
“Guide to the installation of marine engines”; it also provides
indications to compute the dimensions of the exhaust pipe-
lines, which is the Yard’s responsibility.
Electric - electronic equipment
Provide a suitable arrangement of the engine control elec-
tronic unit, of the relay box and of the possible optional
electronic units, referring to the dimensions and position of
the wire harnesses and their connectors.
Both units must be anchored in such a way as to dampen the
vibrations and stresses undergone by the hull while under-
way and/or induced by the engine’s operation.
(1) The EDC engine electronic control is programmed to
reduce maximum deliverable power if the operating
parameters measured by the sensors show that criti-
cal conditions have been reached, and if exceeded the
engine could be damaged.
INSTALLATION DIRECTIVE
10 MAY 2006
S30 ENT M23
5. TECHNICAL DATA FOR INSTALLATION
Combustion and ventilation air when underway
Static vacuum allowed downstream of the air filter kPa
mm H2O
3,5
350
Combustion air flow rate m3/h 710
Engine room ventilation air flow rate (excluding combustion air) m3/h 3590
Static vacuum allowed in the engine room kPa
mm H2O
0,1
10
Temperature allowed in the engine room °C 45
Temperature increase in the engine room to ext. temperature °C 15
Exhaust gas discharge
Allowed static back pressure kPa
mm H2O
10
1000
Exhaust gas temperature at maximum power (turbocharger inlet) °C 700
Flow rate at maximum power kg/h 875
Outer diameter of exhaust mixed with sea water mm
inches
100
4
Fuel supply
Transfer pump delivery at maximum rpm l/h 190
Flow rate return to tank l/h 185
Fuel temperature to allow maximum power °C 70
Inner diameter, intake pipe mm 8
Inner diameter, return pipe mm 8
Thread on pre-filter junctions M 14 x 1,5
Electric pump approved intake vacuum kPa
mmH2O
15
1500
Approved intake pressure at the low pressure mechanical pump kPa
mmH2O
20 to 120
2000 to 12000
Allowed on tank return pipe back pressure kPa
mm H2O
40
4000
Open sea water cooling line
Intake pipeline diameter mm
inches
32
1,26
Pump delivery at maximum rpm l/h 9000
Sea water pump height above sea level m 2
Allowed intake vacuum kPa
mm H2O
20
2000
Dry exhaust outer diameter mm
inches Not foreseen
Allowed engine inclination angles
Maximum longitudinal in continuous operation (static + dynamic) degrees/360 +20
Maximum transverse in continuous operation (static + dynamic) degrees/360 ± 22º30'
Longitudinal for oil level check with standard dipstick degrees/360 0 to +6
INSTALLATION DIRECTIVE 11
MAY 2006 S30 ENT M23
Figure 4
Dimensions
Measurements in: millimeters (inches).
Power takeoffs (optional)
1-race front pulley for “V” belts
Reference diameter mm 83
Race dimension mm 10
Power available at 1000 rpm (*) kW 1
Power available at 2000 rpm (*) kW 2
Radial force resulting from belt tension (*) N 400
(*) These values are valid for driving to the side opposite to that of the sea water pump
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06_001_S
INSTALLATION DIRECTIVE
12 MAY 2006
S30 ENT M23
6. IDENTIFICATION DATA
Figure 6
Figure 5
06_004_S
05_003_S
The engine identification data are stenciled on a tag positioned over the engine coolant tank
INSTALLATION DIRECTIVE 13
MAY 2006 S30 ENT M23
7. COMPONENTS SUPPLIED WITH THE ENGINE
Figure 7
06_019_S
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6 75
4
1. Connectors to be assembled - 2. Conductor terminals - 3. Gaskets to be fitted on individual wires - 4. PF connector rear cover -
5. Fuel electric pump - 6. Fuel pre-filter - 7. Fuel filter - 8. Components to replace fittings mounted on the fuel filter.
The engine is supplied with a box containing the parts
showed in the pictures, as well as spring supports to allow
keelson anchoring.
Electric connectors
As shown in pictures 1, 2, 3, 4, they must be used to set up
the cabling connecting them to the components located on
the fuel filter.
Individual electric connectors are each one sealed in see-
through bags, together with small parts required to com-
plete them. In order to avoid connection errors, connectors
are different from one another; each one of them must be
exclusively mounted by using the small parts contained in the
relevant plastic bag
Connection function
o A. Fuel temperature sensor for EDC
o M. Sensor designed to detect the presence of water in
the fuel pre-filter
o Z. Fuel filter clog sensor
o PF. Heating element on the fuel filter
o JFC. Connection to the JFC connector on the engine
harness
Chapter 9 shows the instructions to be followed to perform
connections.
Mechanical components
As shown in picture 8, they must be used to replace the fit-
tings mounted on the fuel filter support.
Chapter 8 shows the instructions to be followed in order to
carry out assembly operations.
Hydraulic components
Identified in the picture by numbers 5, 6, 7, hydraulic compo-
nents must be used to set up the fuel feeding system.
Chapter 8 shows the instructions to be followed in order to
perform connections.
INSTALLATION DIRECTIVE
14 MAY 2006
S30 ENT M23
8. FUEL LINE
For the installation, the following connections are required:
- from the tank to the pre-filter
- from the pre-filter to the pump inlet
- from the electric pump to the filter inlet
- from the filter outlet to the low pressure mechanical
feeding pump
- from the fuel discharge outlet to the tank.
Components
Pre-filter, electric pump and filter, supplied with the engine,
must be fitted in proximity of the tank, in a relatively low
point of the system. The filter must be prepared as indicated
here below and fastened in such a way to allow easy replace-
ment of the filtering cartridge.
Avoid the use of additional mesh or paper filters along the
feed lines between pre-filter and engine. To avoid introducing
impurities in the feeding lines inside the engine, do not place
filter cartridges pre-filled with fuel in the system.
Materials’ Characteristics
The fuel tank and the suction and return assembly must
withstand the continuous abrasion caused by a flow of fuel
oil of 200 l/h at a temperature of 120 °C without noticeable
1. Low pressure mechanical feeding pump and high pressure common rail injection pump - 2. Electro-injector - 3. Common rail -
4. Pre-filter - 5. Fuel electric pump - 6. Filter.
Figure 8
High pressure
Low pressure
1
4
06_006_S
2
3
6
5
deformation or wear or release of material. Use of metal
tanks, preferably made of iron alloys, is allowed, provided
they are connected to the negative terminal of the battery
to prevent the accumulation of electrostatic charges.
Tanks must be provided with vents to avoid exceeding an
internal pressure of ± 5kPa 0.5 m of H2O column); their
shape and the suction assembly must be such as to assure a
suction at the maximum longitudinal and transverse inclina-
tion allowed for the boat, with a residual quantity of fuel oil
considered “reserve”.
The suction inlet should be positioned in such a way as to
avoid taking in sludge. The return flow must be in such a way
as to facilitate the mixing of the returning fuel with the fuel
in the tank. If the tank is lower than the filter, then the return
pipe must always be submerged. The pipes and union fittings
of the fuel line must withstand a fuel oil flow rate of 200 l/h
at a temperature of 120 °C and a pressure of 3 bar (300
kPa) without noticeable deformation, wear or release of
material. Metal tubes, preferably made of iron alloys, are rec-
ommended, taking care to connect each individual segment
to engine ground to avoid the accumulation of electrostatic
charges and inserting a vibration damper elastic joint on each
segment. The pipes used must be certified according to the
relevant Countries’ rules or to the standards issued by clas-
sification Bodies.
INSTALLATION DIRECTIVE 15
MAY 2006 S30 ENT M23
Fuel supply system scheme
1. Low pressure limiter valve - 2. Pressure regulating electric valve - 3. High pressure radial pump - 4. Pressure sensor - 5. Common
rail - 6. Electro-injector - 7. Fuel tank - 8. Pre-filter - 9. Fuel electric pump - 10. Filter - 11. Vent fitting - 12. Low pressure mechanical
feed pump.
Figure 9
06_007_S
M
3
1
11 7
5 6
2
4
10 8
9
12
Hydraulic connections
Figure 10
1
2
06_020_S
1. Rubber holder fitting for fuel inflow into the low pressure mechanical feeding pump -
2. Rubber holder fitting to allow fuel outflow towards the tank.
INSTALLATION DIRECTIVE
16 MAY 2006
S30 ENT M23
Preparation of the fuel filter support
1. Screw - 2. Seal washers - 3. Rubber holder fitting.
The filter support must be prepared by replacing fuel inlet
and outlet fittings with the supplied ones.
Following the removal of the fittings on the support, Rubber
holder fitting must be mounted on the screws by fitting seal
washers as shown in the picture. Tighten the screws.
Figure 11
06_010_S
1 2 23
INSTALLATION DIRECTIVE 17
MAY 2006 S30 ENT M23
Figure 12
14
5
9
06_012_S
12
32
13
6
7
10
8
11
The electrical equipment of the engine comprises a series
of components provided separately from the engine to
enable an easy and diversified installation, according to the
Yard’s design choices. The need to make accessible, at sea or
underway, the controls to the electrical components and to
the connector for diagnostics contained in the relay box may
be met through different installation arrangements.
Along with the coupling of all connectors provided in the
wire harnesses, completing the installation also requires the
connecting wire harness to the connector JFC (11) for the
fuel filter, to complete the power line and to connect the
accumulator to the engine wire harness.
NOTE
The two general power supply terminals identified as
+BATT and −BATT must be connected to the accumula-
tor, while the terminal identified as +BATT/CC must be
connected to the +30 pole of the starter motor.
9. ELECTRICAL EQUIPMENT
1. Engine wiring - 2. +BATT/CC terminal - 3. Power line for electric starter motor and alternator - 4. Indicator and control panel - 5.
Extension harness - 6. Engine pre-heating glow plugs electronic control unit - 7. Fuse holder for the engine pre-heating glow plugs
electronic control unit - 8. ECU EDC connectors - 9. Relay box - 10. Diagnostic tool connector - 11. Harnessing to be made by
construction site personnel - 12. Fuel filter support - 13. Fuel electric pump
INSTALLATION DIRECTIVE
18 MAY 2006
S30 ENT M23
Synoptic
Figure 13
1. Connector for instrument panel connection wire harness - 2. Engine wire harness - 3. Connector for fuel filter wiring - 4. Power line.
Wires supplied with the engine include connectors for all
concerned components, connector JB to ensure connection
to the warning and control panel, and the JFC connector
to allow the connection to the components located on the
fuel filter.
06_030_S
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INDICATIONS AND
ALARMS SENSORS
ELECTRO-INJECTORS
EDC COMPONENTS
ALTERNATOR
ELECTRIC STARTER
MOTOR
THROTTLE POSITION
SENSOR
INSTALLATION DIRECTIVE 19
MAY 2006 S30 ENT M23
Wire harness
Engine wire harness Fuel filter interface wire harness
Figure 14
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A. Fuel temperature sensor for EDC - B. Drive shaft sensor for EDC - C. Camshaft sensor - F. Engine coolant temperature sensor for EDC - ECF. Connector for the engine
stopping functions if stressed - ECM. Connector for the engine stopping function if stressed - H. Combustion air pressure/temperature sensor for EDC - K. Air filter clogging sensor
(for alarm) - M. Sensor for detecting the presence of water in the fuel pre-filter (for alarm) - O. Exhaust gas temperature sensor (for gauge) - T. Coolant temperature sensor (for
gauge) - V. Oil pressure sensor (for gauge) - E1. Cylinders 1 and 2 electro-injectors - E2.-Cylinders 3 and 4 electro-injectors - E3. Cylinders 5 and 6 electro-injectors -
GG. Alternator - JB. Instrument panel connection wire harness - JF1,JF2. Relay box - MM.-Electric starter motor - PA.-Throttle position sensor - PF. Heating element on fuel filter
- PR. Rail pressure sensor - SI. Gear box oil temperature sensor - VE. Engine oil pressure/temperature sensor for EDC - VI. High gear box oil pressure sensor (25 bar) -
WI. Low gear box oil pressure sensor (7 bar) - ZH. Pressure control solenoid valve.
INSTALLATION DIRECTIVE
20 MAY 2006
S30 ENT M23
Power supply line
1.Alternator - 2. Electric starter motor - 3. Battery -
4. Engine wire harness.
The connection of terminal +B of the alternator to the
positive terminal +30 of the electric starter motor consists
of a 25 mm2 diameter conductor or bigger. The connection
of the positive +30 terminal of the electric starter motor to
the positive pole of the battery, achieved with a conductor
having a cross section of at least 70 mm2, allows to obtain,
as shown in the figure, the simultaneous connection of the
alternator to the battery. The simultaneous connection of the
alternator to the accumulator; on the same terminal, one will
have to connect the cable terminal to an eyelet marked as
+BATT/CC of the engine harness. The connection between
the engine ground and the negative pole of the battery must
be achieved according to the guidelines provided in the
Engine electrical ground paragraph.
CAUTION
If magneto-thermal protecting breakers are inserted, they
must not be used to stop the engine and in any case they
must be activated only a few seconds after shut-down.
Figure 15
M
50 D++B30
+BATT/CC
06_043_S
4
1
2
3
Equipment power supply
Supplementary services battery
To assure that the engine can be started with a sufficient
quantity of energy, it is advisable to provide for the instal-
lation of a supplementary battery, dedicated to supplying
power to the on-board electrical services. The power line to
recharge it may be constructed according to the indications
provided in Chapter 22.
If one engine is installed
The battery used for services may be recharged interposing
on the power supply line a relay actuated by the recharge
signal of the alternator’s electronic regulator (D+).
If two engines are installed
The presence of two generators allows to keep the recharg-
ing functions separated: the generator (G1) recharges the
battery (AC1) dedicated to starting both engines and pow-
ering both electrical/electronic control circuits, whilst the
generator (G2) recharges the battery (AC2) used to power
the services. In two-engine applications, it is essential to con-
nect the engine grounds to a common potential; the solution
proposed in Chapter 22 fully complies with this need, assuring
the full functionality and independence of the two circuits.
INSTALLATION DIRECTIVE 21
MAY 2006 S30 ENT M23
Battery recharging
B+. Connected to the +30 of the electric starter motor - D+.
Excitation - N. Not connected.
This is accomplished through the power supply line of the
electric starter motor and connection to the +B of the
alternator. The electronic regulator of the alternator that
equips the engine allows an effective control over the bat-
tery recharging operation.
If, due to installation requirements, the batteries need to be
positioned at a distance from the engine, we recommend
increasing the cross section of the power line conductors
and verifying recharging effectiveness by measuring voltage
across the battery poles.
Engine electrical ground
The connection of the engine electrical ground is achieved
by connecting with a cable of at least 70 mm2 cross section
to the negative pole of the battery to the tightening point of
the electric starter motor as shown in the following figure.
1. Point of connection of the engine electrical ground.
To anchor the grounding terminal to the engine, proceed as
follows:
o Completely remove the conducting paint from both
parts constituting the connection, using mechanical
means or suitable chemical product; if the anchoring
operation is to take place on superficially treated parts,
completely remove the anaphoretic paint with mechani-
cal means, obtaining a smooth support surface.
o Apply a uniform layer of BH44D paint (IVECO standard
18-1705) with a brush or spray gun.
o Join the parts constituting the grounding note within 5
minutes from the time the paint was applied.
Figure 16
04_078_N
Figure 17
1
06_020_N
INSTALLATION DIRECTIVE
22 MAY 2006
S30 ENT M23
Figure 18
Wiring to the JFC connector
By stabilizing the fuel filter assembly position, it will be possi-
ble to set up the wiring to connect the components located
on the fuel filter.
The diagram in the picture shows the connections to be
performed on connectors.
Connection function
o A. Fuel temperature sensor for EDC
o M. Sensor designed to detect the presence of water in
the fuel pre-filter
o Z. Fuel filter clog sensor
o PF. Heating element on the fuel filter
o JFC. Connection to the JFC connector on the engine
harness
NOTE
Comply with conductors’ minimum diameters indicated in
the diagram in order to avoid voltage drops which would
endanger the system operation.
06_041_S
Minimum cable
cross section in mm2
Connector code
Component
terminal
Minimum cable
cross section in mm2
Connector code
Component
terminal
INSTALLATION DIRECTIVE 23
MAY 2006 S30 ENT M23
0&
:
-
*&#
!
!
&
+
%
"
!
"
!
06_031_S
1
Figure 19
1. Fuel filter
The picture shows 5 connectors and the position that con-
ductors must have in order to ensure correct connections.
Wiring must be performed to ensure minimum diameters of
conductors, as indicated in the electric diagram.
CAUTION
Wrong connections of conductors can generate malfunc-
tions and damage electric components.
The wiring must be made with the JFC connector, not
connected to the engine harness. Coupling of the two JFC
connectors will have to be done with the power supply
switched off.
INSTALLATION DIRECTIVE
24 MAY 2006
S30 ENT M23
Relay box
It represents the main interconnection point and it performs
multiple interfacing functions between the various system
components.
It is the seat of remote control switches and fuses; compo-
nents are mounted on a base and thus it is possible to extract
them to set up verification or replacement operations.
Remote control switches (relays) depend upon the following
components:
K1 key switch electric discharge
K2 emergency engine shut-down provision
K3 EDC main (power supply
K4 power supply to terminal 50 of the electric
starter motor
K5 Electric fuel pump power supply
K6 fuel filter heater element power supply
The components to which fuses depend upon are as follows:
F1 electric fuel pump
F2 heating element on fuel filter
F3 power supply to the heater plug control unit (15 A)
F4 EDC (10 A)
F5 EDC (25 A)
Figure 23
&¬
&¬
&¬
&¬
&¬
+
+
+
+
+
+
06_024_S
Connections of the central electronic unit
(ECU) EDC 16C8
A. 60 pole connector - B. 94 pole connector.
The connection of the central electronic unit, ECU, to the
components of the EDC system is achieved by means of
three connectors to subdivide the wiring harnesses, thereby
favoring a quicker identification of the lines during testing
operations.
o B for engine mounted components
o A for boat side connections
The different connectors are polarized and provided with
levers to favor the connection and disconnection operations
and assure proper coupling.
The sequence of operations allowing the removal of connec-
tors from their housing is as follows:
A) Extract the extraction lever retaining device;
B) Lift the extraction lever, make sure the anchoring slide is
extracted from its housing;
C) Lift the connector without causing any fluctuation which
would jeopardize the integrity of electric terminals.
Figure 20
Figure 21
Figure 22
B
A
06_029_S
06_060_S
A
06_061_S
C
B
INSTALLATION DIRECTIVE 25
MAY 2006 S30 ENT M23
Water presence in the filter sensor
1. filter - 2. Conductor to be connected
with the negative battery terminal.
CAUTION
In order to enable the proper working of the sensor to
detect water in the fuel, it is necessary that the filter
support is connected electrically to the negative battery
terminal.
In the engine models which use parts with insulated poles it
is necessary to electrically insulate the filter support from the
boat mass and then connect the support with the negative
battery terminal.
Figure 27
Heater plug fuse
A maxi 60 A fuse is located in serial connection with the
electric network of heater plugs.
Diagnostic connector
A multipolar plug is located in proximity of the relay box,
to which an IVECO MOTORS diagnostic tool can be con-
nected to.
The diagnostic tool allows the processing of data recorded
during the engine operation phase and memorized in the
ECU; data interpretation will provide useful indications to
better schedule maintenance interventions.
Throttle lever position sensor
After testing the working condition of the linkage, adjust the
run of the servo components (see Chapter 18).
o With the throttle at idle setting, the potentiometer rod
has to be in the resting position.
o With the throttle at the stop, the potentiometer rod has
to be in the position of maximum run out.
06_050_S
06_048_S
Figure 24
Figure 25
Figure 26
2
1
06_040_S
80856
INSTALLATION DIRECTIVE
26 MAY 2006
S30 ENT M23
10. MAIN ANALOG INSTRUMENT PANEL
Installation of the IVECO MOTORS onboard panel with
analog indicators entails connecting the panel’s JC connec-
tor to the JB connector on engine wire harness, interposing
the appropriate extension wire harness available in 3, 5 and
7 meter-long versions. The JC-JB wire harness comprises 47
lines, each connected to the terminal identified on both con-
nectors by the same number.
To the main panel is connected the JE connector, provided
for connection to the secondary panel; in installations with
no secondary panel, do not remove the cap of the JE con-
nector to avoid compromising the electrical continuity of the
systems’ power supply circuit.
To allow the work of the fuel filter clogging alarm (SIFC), in
the indication alarm module, it has to disconnect the connec-
tor (12) fitted close to JC.
Figure 28
1. Coolant temperature gauge (TA) - 2. Revolution counter and hour counter (CG) - 3.Voltmeter (V) - 4. Buzzer (SA) - 5. Indication
and alarm module (MS) - 6. Engine oil pressure gauge (MO) - 7. Connector for secondary instrument panel (JE)- 8. On board panel
instrument light switch (L) - 9. Engine start/stop key switch (CA) -10. Engine stop push-button (usable only with electric harness
versions with excitation engine stop) - 11. Sound alarm inhibition push-button (P1) -12. SIFC Alarm abilitation connector -
13. Connector for main panel wiring (JC) - 14. Cap with electrical continuity connection.

oF
oC
V
bar



 


 



06_002_S
1
13
2
3 4 5
6
7
11 10 98
14
12
INSTALLATION DIRECTIVE 27
MAY 2006 S30 ENT M23
CONNECTORS OF THE JB - JC EXTENSION WIRE HARNESS, SEEN FROM THE COUPLING SIDE
To identify the functions served by the individual lines, refer to the electrical diagrams in Chapter 22.
1. JB-JC extension wire harness - 2. JE-JH extension wire harness.
Figure 30
Synoptic of the connections of the analog panels
JB JA
JF1 JF2
A2
A1
A
JHJH
JE JE
JC
JC
04_254_N
1
2
MAIN
INSTRUMENT
PANEL
RELAY
BOX
EDC
SECONDARY
INSTRUMENT
PANEL
BATTERY
ENGINE
EQUIPMENT
JC JB
32
47
18
28
45 17
29
44 16
42
43
31
46
30
711
12
24
38
1
5
6
13
14
15
4
40
2627
41
25 39
21
22
36
34
8
9
19
20
33
35
23
37
2
3
10
24
12
40
39
22
38
37
23
36
44
16
13
14
41
26
25
27
15
28
42
43
1
11 4
10 2
3
7
5
17
6
18
35
21
9
20
19
33
832
34 47
29
45
30
31
46
04_250_N
Figure 29
INSTALLATION DIRECTIVE
28 MAY 2006
S30 ENT M23
Indications and alarms module
1. Runaway engine (SSV) - 2. Presence of water in fuel pre-
filter (SAC) - *3. Low coolant level (SBLA) - 4. Alternator fault
(SS) - *5. Clogged oil filter (SIFO) - *6. Clogged oil vapor filter
(SIFB) - *7. Pre-lubrication (SP) - 8. Clogged air filter (SIFA)
- 9. Clogged fuel filter (SIFC) - 10. High coolant temperature
(SATA) - 11. Low oil pressure (SBPO) - 12. Pre-post heating
(SCP) - 13. EDC malfunction (EDC).
* Unavailable functions on S30 ENT M23 engines.
The indications and alarms module comprises the indicator
lights and the electronic alarm interface, timing and stor-
age circuit. It is programmed in such a way that when it is
powered, all indicator lights are lighted, with the exception
of those for “pre-lubrication”, “pre-post heating” and “EDC”
failure and a sound signal is emitted by the buzzer.
The sound alarm may be silenced before the end of the test,
acting on the appropriate control.
During the starting phase and for the subsequent 15 sec-
onds, needed to stabilize the low oil pressure signal, all the
module’s functions are inhibited; once this time interval has
elapsed, every alarm state detected by the sensors will cause
the associated indicator to be lighted and the buzzer to be
powered; the exceptions are the “pre-lubrication” and “pre-
post heating” indicators, given only visually.
When a new alarm state is detected, the indicator light will
flash to highlight the occurrence with respect to any others
which may be ongoing at the time. When the sound alarm is
shut off, the light indicator will remain lighted and the alarm
will be stored until the engine is stopped.
The standard set-up of the S30 ENT M23 provides for use
of the indicators SAC, SS, SIFA, SATA, SBPO, EDC.
Installation
In order to drill holes on the area where the panel is to be
mounted, refer to the dimensions indicated in Chapter 12.
Operation of the panel
After completing the electrical connections and engine
preparation, perform the tests required for the first start, as
described in Chapter 17.
Verify the proper operation of the panel, proceeding as
follows:
o Make sure that the “ENGINE ROOM / BRIDGE” switch
of the Relay Box is in the “BRIDGE” position, then turn
the key switch to the first position and verify that the
instruments are powered and the indications and alarms
module runs the alarm test for about 5 seconds accord-
ing to the procedures set out below.
o Once the test is complete, only the indications pre-
scribed for the engine not running must remain lighted:
e.g. “alternator charge” and “low oil pressure”; the analog
instruments must provide values consistent with the
relevant physical parameters.
Testing the engine start function
Turn the key switch to the second position and keep it in it
until the engine has started, then release the switch, which
will stably return to the first position; after releasing the key,
the switch may be brought back to the starting position only
after the switch is returned to the resting or zero position.
Checking indications
After starting the engine, verify whether the operating
modes of the indications and alarms module are similar to
those set out below.
Using appropriate measuring instruments, verify the consist-
ency of the indications provided by the analog instruments.
Verify the indication of the panel revolution counter, compar-
ing it with the one measured by a reference instrument; if the
indication is different, proceed as described below.
Testing the engine stop function
The engine is stopped and the panel is disabled by returning
the key switch to the resting or zero position.
If the engine stopping function if stressed is present, press the
stopping button situated on the board.
Figure 31
04_234_N
2
4
8
13
1
3
5
6
9
12
10
11
7
INSTALLATION DIRECTIVE 29
MAY 2006 S30 ENT M23
Revolution-counter calibration
1. Adjustment screw -
2. Panel lighting lamp.
Verify the indication of the panel revolution counter by com-
paring it with the one measured with a reference instrument;
if it differs, operate the adjustment screw (1), located in the
rear part of the instrument, until consistency is achieved;
repeat the operation for different engine rpms.
Maintenance
Should it become necessary to replace a panel light, remove
the lamp holder from the rear part of the instrument (see
Figure 32A).
04_255_N
1
2
Revolution-counter calibration
1. Calibration increasing button -
2.Calibration decreasing button.
Verify the indication of the panel revolution counter by com-
paring it with the one measured with a reference instrument;
if it differs, press the button 1 and 2 situated on the rear
of the tachometer, until consistency is achieved; repeat the
operation for different engine rpms.
Maintenance
The board is illuminated by not-replaceable internal LEDs.
Figure 32B
06_113_V
1 2
Figure 32A
INSTALLATION DIRECTIVE
30 MAY 2006
S30 ENT M23
11. SECONDARY ANALOG INSTRUMENT PANEL
electronic
RPMx100
04_240_N
1
3
2
5
4
6
7
1.Connector for secondary panel wire harness (JH) - 2. Engine start push-button (CS) - 3. Revolution counter (CG) -
4. Buzzer (SA) - 5. Indications and alarms module (MS) - 6. Engine stop push-button (AS) -
7. Sound alarm inhibition push-button (P1).
Figure 33
The connection is achieved by removing the cap on the JE
connector of the main panel, and connecting the JE connec-
tor to the JH connector on the secondary panel, interposing
the extension wire harness, available in 3, 5 and 7 meter-long
versions (see Figure 29). The JE-JH wire harness comprises
12 lines, each connected to the terminal identified on both
connectors by the same number (see Figure 34).
CONNECTORS OF THE JE-JH EXTENSION WIRE
HARNESS, SEEN FROM THE COUPLING SIDE
Installation
In order to drill holes on the area where the panel is to be
mounted, refer to the dimensions indicated in Chapter 12.
Operation of the secondary panel
After completing the electrical connection to the main panel
and engine preparation, and performing the tests required
for the first start (as described in Chapter 17), verify the
proper operation of the panel, proceeding as follows:
o Make sure that the “ENGINE ROOM / BRIDGE” switch
of the Relay Box is in the “BRIDGE” position, then turn
the key switch to the first position, thus enabling the
operation of both panels.
o Carry out the same tests for the secondary panel as
were carried out for the main panel.
o Disable the secondary panel by bringing the key switch
on the main panel to the resting or zero position.
Testing the engine start and stop function.
With the panel enabled, press the green push-button until
the engine starts, then release it; wait for engine rpm to sta-
bilize before stopping it by pressing the red push-button.
The starting and stopping operations can be performed sev-
eral times and consecutively from the secondary panel
Checking indications
Proceed in the same way as for the main panel.
Figure 34
*% *(
1 6 6 1
7 12 12 7
04_251_N
INSTALLATION DIRECTIVE 31
MAY 2006 S30 ENT M23
12. DRILLING PLANS FOR ANALOG PANELS
Measurements in: millimeters.
= =
225
285
264
Ø4
Ø4
Ø4
Ø4
==
140
200
26264 4
26 4
MAIN PANEL
= =
180
240
282
==
80
140
2828
28
Ø4
Ø4
Ø4
Ø4
22
SECONDARY PANEL
Figure 35
Figure 36
INSTALLATION DIRECTIVE
32 MAY 2006
S30 ENT M23
13. CUSTOMIZED INSTRUMENT PANEL
Using only the components of the panel that are not wired
to allow for panel customization, they will have to be wired
using the 10 meter long wire harness, set up at one end for
coupling to the JB connector and at the opposite end with
conductors with free terminals with identifying numbering
on each wire. The conductors will have to be connected to
the individual components as indicated in the electrical and
wiring diagrams in Chapter 22.
CAUTION
To assure the functionality of the safeties pertaining to the
engine start/stop commands from the instrument panel or
engine room, it is mandatory to wire the key switch strictly
as shown in the electrical diagrams in Chapter 22.
The wiring details of the indications and alarms module
alone are provided below; indications for IVECO MOTORS
indicator instruments, are shown in the related wiring dia-
grams in Chapter 22.
JD Connector for indications and alarms module
VIEW FROM THE INTEGRATED SIDE
IN THE REAR PART OF THE MODULE
VIEW FROM THE TERMINAL SIDE
OF THE COUPLING SIDE WIRING
Connector TRIDENT - ITT Cannon
part # TST 24PA00
terminal female part # 192990-0050
lid rear part # TST24AH00
JD connects the indications and alarms module to the elec-
trical system of the engine (sensors, power supply, etc.).
The terminal part of the wire harness, supplied with the
module, must be completed using female terminals, as
described in the electrical diagram of Chapter 24.
For standard-equipped engines, to have the essential indica-
tions available, the following ways must be wired: 1, 2, 3, 7, 8,
9, 10, 13, 14, 15, 17, 18, 19 with the female terminals supplied
as standard equipment.
Figure 37
Figure 38
13
9
5
1
14 15 16
10 11 12
6
24
7 8
3
21 22 23 24
17 18 19 20
04_241_N
123
4
568 7
10 912 11
1314
16 15
171820 19
212224 23
05_034_C
INSTALLATION DIRECTIVE 33
MAY 2006 S30 ENT M23
CAUTION
To assure the utmost reliability and safety while underway, all installations must be provided with the following alarm indica-
tions:
(EDC) EDC failure
(SATA) high coolant temperature
(SBPO) low oil pressure
It is also recommended that the following indications be present:
(SAC) presence of water in the fuel pre-filter
(SIFA) clogged air filter
(SIFC) fuel filter indication
(SS) alternator fault
Functions of the JD terminals
PIN Description Electric level
OFF Indication ON Indication
1 Module power supply Positive (+B)
2 Not connected -
3 EDC Fault indication High (+B) Low (ground)
4 Not connected -
5 Pre-heating indication High (+B) Low (ground)
6 Pre-lubrication indication Open circuit High (+B)
7 Engine start Power supply positive (+B) while starting
8 Sound alarm inhibition Negative (ground) during the request
9 Module power supply Negative (ground)
10 Buzzer power supply Negative (ground) during the emission of sound
11 Clogged oil filter indication Open circuit Low (ground)
12 Clogged oil vapor filter indication Open circuit Low (ground)
13 Clogged air filter indication Open circuit Low (ground)
14 Clogged fuel filter indication Low (ground) Open circuit
15 Alternator fault indication High (+B) Low (1 to 3 V)
16 Low engine coolant level indication Open circuit Low (ground)
17 High coolant temperature indication Open circuit Low (ground)
18 Low engine oil pressure indication Open circuit Low (ground)
19 Presence of water in fuel indication Open circuit Low (ground)
20 Overloaded or runaway engine indication Open circuit High (+B)
21 Not connected -
22 Not connected -
23 Reception of data from main panel NMEA communication protocol (0 to 5 V)
24 Transmission of data to secondary panel NMEA communication protocol (0 to 5 V)
INSTALLATION DIRECTIVE
34 MAY 2006
S30 ENT M23
14. SENSORS FOR DETECTION AND PANEL SIGNALING
Coolant temperature sensor
Resistor with negative temperature coefficient, providing the
signal for analog temperature indication.
Operating voltage: from 6V to 24 V
Calibration range from 0 °C to 120 °C
Resistance value at 90 °C 51,2 ± 4,3 Ω
Electrical poles isolated
High coolant temperature sensor
Switching coolant temperature sensor, providing the signal
for the related indicator.
Operating voltage: from 6 to 24 V
Condition at ambient temperature normally open
Closing temperature: 100 ± 3 °C
Electrical poles isolated
Oil pressure sensor
Rheostat component providing the signal for the analog
indication of pressure.
Operating voltage from 6V to 24 V
Calibration range from 0 bar to 10 bar
Resistance value at 0 bar 10 Ω +3/-5 Ω
Resistance value at 2 bar 52 ± 4 Ω
Resistance value at 4 bar 88 ± 4 Ω
Resistance value at 6 bar 124 ± 5 Ω
Maximum value of resistance 184 Ω
Operating temperature from - 25°C to 100°C
Electrical poles isolated
Figure 39
Figure 40
Figure 41
04_027_C
04_237_N
04_236_N
INSTALLATION DIRECTIVE 35
MAY 2006 S30 ENT M23
Figure 42
Low oil pressure sensor
Pressure switch, providing the signal for the related indicator.
Operating voltage: from 6 to 24 V
Condition at ambient pressure normally closed
Calibration range 0.5 - 0.8 bar
Closing pressure: 0.5 bar
Opening pressure: 0.8 bar
Maximum current 15 A (not inductive)
Electrical poles isolated
Air filter clogging sensor
Vacuum switch, providing the signal for the clogged air filter
alarm indicator.
Operating voltage from 6V to 24 V
Condition at ambient pressure normally open
Closing vacuum 52 mbar
Operating temperature from -20 °C to +80 °C
Maximum current 0,1 A (not inductive)
Electrical poles isolated
Figure 43
04_028_C
04_238_N
Fuel filter clogging sensor
Figure 44
Pressure switch, providing the signal for the related indica-
tor.
Operating voltage: from 6 to 24 V
Condition at ambient pressure normally closed
Opening pressure: 1.5 ± 0.1 bar
Maximum current 0,1 A (not inductive)
Electrical poles isolated
Exhaust gas temperature sensor
NiCr-Ni thermocouple sensor with insulated poles, pro-
viding the signal for the analog indication of exhaust gas
temperature.
Temperature Voltage
°C mV
100 4.10
200 8.13
300 12.21
400 16.40
500 20.65
600 24.91
700 29.14
800 33.30
900 37.36
Figure 45
04_030_C
04_260_N
INSTALLATION DIRECTIVE
36 MAY 2006
S30 ENT M23
15. PREPARING THE ENGINE
FOR FIRST START-UP
1. Drain the residual 30/M protective oil from the sump.
2. Pour into the lubricating loop only lubricating oil of the
type and in the quantities set out in the Refilling Table.
3. Drain the CFB protective liquid from the fuel loop,
completing the operations as indicated under item 3. of
Chapter 21.
4. Remove the caps and/or seals from the engine intake,
exhaust, aeration and venting ports, restoring normal
conditions of use. Connect the inlet of the turbocharger
to the air filter.
5. Connect the fuel loops to the boat tank, completing
the operations set out in item 4. of Chapter 21. During
filling operations, connect the pipe returning fuel to the
tank to a collecting container, to prevent residues of CFB
protective liquid from ending up into the boat tank.
6. Verify and refill engine coolant as prescribed.
7. Remove from the engine the labels with the inscription
“ENGINE WITHOUT OIL”.
Although they are extremely important, “common sense”
checks such as the exposure of sensitive parts (plastics, wire
harness, electronic units, etc...) to heat, and those that for
years have characterized the quality of the work performed
in the yard, are not mentioned herein.
Tests of the proper operation of the engine and the com-
ponents of the electronic control system may be performed
rapidly and with the utmost reliability using specific diagnostic
tools, available from IVECO MOTORS Technical Assistance
Centers.
Fuel tank suction
Verify the fuel suction at the maximum allowed longitudinal
and transverse inclination, with the residual quantity of fuel
considered “RESERVE”, such as to cause the reserve indica-
tor light to be permanently lighted.
Throttle lever position sensor
In the positions of minimum and maximum travel, verify the
correlation between the position of the throttle control valve
on the bridge and the position of the sensor rod, checking:
Instrument panel
Verify the efficiency of all light indicators, as described in the
related Chapters.
16. TESTS BEFORE
THE FIRST START-UP
INSTALLATION DIRECTIVE 37
MAY 2006 S30 ENT M23
17. FIRST ENGINE START
Before starting the engine, please make sure the sea water
gate valve is open, check the levels of the lubricating oil and
of the engine coolant, and complete venting the air from the
fuel feed loop:
o Turn the key on “ON”; so that the ECU EDC feeds the
fuel electric pump for a few seconds, thus pressurizing
the low pressure feeding circuit.
o Loosen the vent fitting on the pre-filter.
o Newly turn the key on “ON” to feed the electric pump
until air-free fuel flows out of it.
o Tighten the vent fitting.
Make sure that the fuel that flows out of the fitting is not
dispersed in the environment.
CAUTION
Never attempt to vent the high pressure system, as this is
useless and extremely dangerous.
NOTE
A few moments after engine start, make sure sea water is
correctly expelled out of the system.
Once the first start-up phase is complete, verify that:
o There are no liquid leaks from the coolant loop pipeline
junction hoses.
o There are no exhaust gas leaks into the hull.
o Complete the instrument panel operation tests as
described in the related Chapters.
o Verify that the power supply voltage across the battery,
after about 15 minutes with the engine running, is no
less than about 13 V.
o Stop the engine and delete any “errors” which may have
been stored in the injection system ECU during the
stabilization phases. For the deletion procedure, refer to
Chapter 20.
INSTALLATION DIRECTIVE
38 MAY 2006
S30 ENT M23
18. EDC ANOMALIES INDICATION
Anomalies indicator light
The ECU continuously monitors, with complex self-testing
routines, its own operating conditions as well as those of the
components connected to it and of the engine.
When anomalies are detected, the alarm indicator light on
the indicator and control panel is lighted in manners that
provide a first indication on the severity of the problem.
Light off: no anomaly detected or slight anomaly
that does not compromise operating
safety
Light on: significant anomaly, allowing to proceed to
a service center
Blinking light: severe anomaly requiring immediate
repairs. If possible, shut the engine down.
Recovery
The recognition of significant or severe anomalies causes
the adoption of strategies that allow to use the engine with
complete safety, guaranteed by limiting performance within
pre-set thresholds according to the severity of the case.
These strategies cause the reduction of the maximum values
of torque and power delivered by the engine.
In the case of intermittent anomalies, i.e. recognized by the
ECU and subsequently no longer present, performance
reduction will continue until the engine is shut down.
Normal operation will be restored only the next time the
engine is started, while the anomaly data will be “saved” in
the failure memory.
NOTE
Identification of severe anomalies of the accelerator posi-
tion sensor, causes the ECU to increase the engine rpm
from about 800 rpm to about 1050 rpm, in order to
achieve a minimum engine thrust and allow manoeuvers.
Error deletion procedure
It will be possible through the IVECO PT01 device con-
nected to the dedicated J1 diagnostic connector.
CAUTION
The mistake deleting procedure is intended to eliminate
the information relating to the mistakes from the ECU
memory, which happened during previous working periods.
The mistakes will not be deleted unless the relating cause
has been removed. Please remember that some anomalies
can be detected by the ECU self-diagnosis only during a
complete engine working cycle.
Figure 46
06_048_S
INSTALLATION DIRECTIVE 39
MAY 2006 S30 ENT M23
19. BLINK CODE TABLE (software version P315 V4.B)
Blinking
code
EDC indicator
light
Indicated fault Max power
reduction
DTC code
Control area
11 (on) not significant in marine applications -117 - 119
13 (off) not significant in marine applications -78
14 blinking throttle position sensor (line 1 o line 2) x8 - 9
17 off not plausible accelerator position sensor signals -11
18 off EDC anomalies warning light control -108
Engine Area 1
21 blinking water temperature sensor x20 - 21
22 off air temperature sensor -57
23 on fuel temperature sensor -40
24 blinking supercharge air pressure sensor x17 - 131
25 off ambient pressure sensor (inside the unit) -10
27 on electric fuel pump control relay exication circuit -94
28 off coil relay fuel heater -42
Engine Area 2
35 off battery voltage value -18
36 off pre-heating warning light control circuit -48
37 off engine heater plugs feeding relay -47
38 off not plausible signal "15", power supply from key -109
39 off engine heater plugs control unit -49
Injectors
51 blinking cylinder 1 electro-injector x66 - 67
52 blinking cylinder 2 electro-injector x68 - 69
53 blinking cylinder 3 electro-injector x70 - 71
54 blinking cylinder 4 electro-injector x72 - 73
57 blinking electro-injector cylinder 1-2-3 power driver 1-4 x60 - 61
58 blinking electro-injector cylinder 4-5-6 power driver 1-4 x62 - 63
59 blinking cylinder electroinjector unit power stage (A o B chip internal
error) x64 - 65
Engine RPM sensor
61 blinking driving shaft sensor signal x37
62 blinking timing shaft sensor signal x36
63 blinking not plausible driving and timing shifts sensors signals x38
(continue to next page)
INSTALLATION DIRECTIVE
40 MAY 2006
S30 ENT M23
Blinking
code
EDC indicator light Indicated fault Max power
reduction
Code DTC
Interface
72 on CAN lines error -87 - 88- 45
73 on CAN lines error -43 - 44 - 46
74 off CAN lines error -29 - 126 - 128
129 - 130
75 off CAN lines error -125 - 127
Fuel pressure
81 blinking fuel pressure control deviation STOP 98 - 99
81 blinking rail pressure too low value STOP 100
81 blinking rail pressure too high value STOP 101
81 blinking fuel pressure control management - 102 - 103
82 blinking fuel pressure sensor signal STOP 95
82 on fuel pressure sensor signal deviation x96
83 blinking pressure adjustment solenoid valve STOP 82 - 83 - 84
Electronic unit
91 blinking internal errors -50 - 52 - 54 - 55
56 - 86 - 121
92 blinking EEPROM memory error -51
93 (on) not relevant for marine applications -58
94 on main relay -80
96 blinking initialization error (inside control unit) x104
97 blinking analogical-digital converter -3
97 blinking control unit/sensors feeding x105
97 blinking control unit/sensors feeding STOP 106
98 blinking internal errors -90 - 91
99 on internal errors -110
INSTALLATION DIRECTIVE 41
MAY 2006 S30 ENT M23
20. UNDERWAY CHECKS
ECU Temperature
Verify that the temperature of the surface of the electronic
engine control unit, after 30 minutes underway at full engine
power, is less than +70 °C.
Engine compartment vacuum
Verify that value of ambient air pressure in the engine room
with the engine(s) at full load and maximum power output
complies with the value specified herein.
Combustion air temperature
Verify that the temperature in the engine room, after 30 min-
utes underway at full engine power, does not exceed 45 °C
and, in any case, does not exceed the value of external tem-
perature by more than 15°C.
Exhaust back-pressure
Verify that the value of back-pressure present at the inlet of
the exhaust gas conduit, with the engine(s) at full load and
maximum power output, complies with the value specified
herein.
Exhaust temperature
Verify that the temperature of the exhaust gases under
maximum engine power output conditions is close to the
prescribed value. To determine the propeller power absorp-
tion curve, it will also be possible to obtain the fuel injec-
tion values from the ECU parameters by using the IVECO
MOTORS tool.
Fuel temperature
Verify that the temperature of the fuel in the low pressure
line, while underway at full power and with a stable quantity
of fuel in reserve, does not exceed 70 °C. A higher value
would entail a reduction in engine performance. If the ten-
dency to reach the maximum allowed temperature is noted,
install a heat exchanger for the fuel.
Pressure in the fuel supply line
To assure the regular operation of the engine and the reli-
ability of the components of the fuel supply and injection
system, you need to verify that:
o Diesel feeding pipe pressure to low pressure mechanical
pump should range between 0.2 and 1.2 bar (2000 to
12000 mm H2O);
o pressure in the fuel oil return line to the tank is less than
0.4 bar relative (4000 mm H2O).
Measures are carried out inserting a “T” junction near the
fuel inlet and outlet, taking care to avoid any air suction. Val-
ues are read at variable rpm, from idle to maximum, at 200
rpm intervals.
If there are any symptoms indicating the possible presence of
air in the fuel supply line, a check may be made by inserting
a clear tube, arranged as an inverted U, before the engine
inlet junction.
INSTALLATION DIRECTIVE
42 MAY 2006
S30 ENT M23
21. PREPARING THE ENGINE FOR LONG IDLE PERIODS
To prevent oxidation to the internal parts of the engine and
to some components of the injection system, if idle periods
exceeding two months are expected, the engine needs to
be prepared with six-months periodicity, proceeding as
follows:
1. Drain the lubricating oil from the sump, after heating the
engine.
2. Pour 30/M protective oil (alternatively, oil conforming
with MIL 2160B Type 2 specifications) into the engine to
the “minimum” level marked on the dipstick.
Start the engine and let it run for about 5 minutes.
3. Drain the fuel from the injection line and from the filter,
taking care to avoid letting the fuel come in contact with
the auxiliaries belt.
4. Connect the fuel line to a tank containing CFB protec-
tive liquid (ISO 4113) and assist the inflow of the liquid
by pressurizing the line and turning the engine over for
about 2 minutes, after excluding the operation of the
injection system. The required operation may be carried
out by directly polarizing the terminal 50 of the electric
starter motor with positive voltage 12 V, using a conduc-
tor prepared for the occasion.
5. Nebulize 30/M protective oil at the rate of about 70 g
(30 g per liter of displacement) into the turbocharger
intake, while the engine is turning over as described
above.
6. Close with suitable stoppers or seal with adhesive tape
all engine intake, exhaust, aeration and venting ports.
7. Drain the residual 30/M protective oil from the sump; it
may be re-used for 2 more engine preparation opera-
tions.
8. Apply tags with the inscription “ENGINE WITHOUT
OIL on the engine and onboard panel.
9. Drain the coolant, if it has not been mixed with anti-
freeze and corrosion inhibiting agents, affixing tags to
indicate that the operation has been carried out.
If external parts of the engine are to be protected, spray
protective liquid OVER 19 AR onto unpainted metal parts,
such as flywheel, pulleys and others; avoid spraying belts, con-
nector cables and electrical equipment.
INSTALLATION DIRECTIVE 43
MAY 2006 S30 ENT M23
Wiring diagram key
Figure 47
General conditions for the preparation and interpretation of wiring diagrams
o Key switch open
o Engine not running
o Liquids at efficient levels and pressures
22. WIRING DIAGRAMS
B62 4
85150
28 72 5 1 68 61 62 25 48 52 93 71 92
JB
13
JB
10
JB
11
6
BAT
6
+
6
+
BAT
50
25
AC
70
GG
B+
2
5030
MM
PE
A
B
PF
A
B
30
50 15
JB
7
M
EJFC
5JB
1
R2
D1
VU
J1
R1 SS EDC SCP
CA
QP
JC
18 12 17
JC
7
T C D B E
K4
87 30
85 86
30 87
86 85
K1
30
87a
86 85
K2 JC
9
JB
9
F3F4
F5
87 30
85 86
K3
30 87
86 85
K6
30 87
86 85
K5
F1 F6
F2
MPO
M
91 31 30 45
6 3 2
PA
46 8 9
1 5 4
JB
18 12 17
ST30 86 D G4 31G1 G2 G3
G4G1 G2 G3
CC
JC
2
JB
2
AS
JE
10
JH
10
JH
4
JE
4
JB
8
JC
8
JFC
A B
JFC C D
Terminal
connections
Minimum cable
cross section in mm2
Component code
or connector code
Component
terminal
Connection
JC: connector
8: terminal
Component
code
Fuse code
Sk Connett_B S30
INSTALLATION DIRECTIVE
44 MAY 2006
S30 ENT M23
Electrical equipment component code
A fuel temperature sensor for EDC
B drive shaft sensor
C camshaft sensor
F engine coolant temperature sensor for EDC
H combustion air pressure/temperature sensor for
EDC
I coolant high temperature sensor
K air filter clogging sensor (for alarm)
L instrument panel light switch
M sensor for detecting the presence of water in
the fuel pre-filter (for alarm)
O exhaust gas temperature sensor
T coolant temperature sensor (for gauge)
V oil pressure sensor (for gauge)
W engine oil low pressure sensor
Z fuel filter clogging sensor
P1 sound alarm inhibition push-button
R1 120 Ω resistor for CAN line balancing
R2 alternator pre-excitation resistor
AC battery
AQ engine shut-off push-button on main panel
AS engine shut-off push-button on secondary panel
CA key switch
CC engine pre-heating glow plugs electronic control
unit
CS engine start push-button on secondary panel
E1, E2, E3, E4
electro-injector
G1, G2, G3, G4
engine pre-heating glow plugs
GG alternator
MM electric starter motor
MS IVECO MOTORS indications and alarms module
PA throttle position sensor
PE fuel electric pump
PF heating element on fuel filter
PR rail pressure sensor
QP main analog instrument panel
QS secondary analog instrument panel
SA buzzer
WI low gear box oil pressure sensor (7 bar)
ZH pressure control solenoid valve
85150 ECU of the EDC system
(continues on next page)
INSTALLATION DIRECTIVE 45
MAY 2006 S30 ENT M23
Electrical equipment component code (follows)
Connectors
A 60 pole EDC engine components
B 94 pole EDC electro-injectors
J1 external diagnostic tool (on the relay box panel)
JB on engine wire harness
set for connection to the main analog
instrument-panel or to the interface wire
harness for converter module
JC on main analog instrument panel
set for connection to the engine wire harness
JD IVECO MOTORS indications and alarms module
Je on main analog instrument panel
set for connection to the secondary analog
instrument panel
Jh on seCondary analog instrument panel
set for connection to the main analog
instrument-panel
vIndicator lights
EDC EDC malfunction
SAC presence of water in fuel pre-filter
SATA high coolant temperature
SBLA low coolant level
SBPO low oil pressure
SCP pre-post heating
SIFA clogged air filter
SIFB clogged oil vapor filter
SIFC clogged fuel filter
SIFO clogged oil filter
SP pre-lubrication
SS alternator fault
SSV runaway engine
Gauges
CG revolution-counter
MI gear box oil pressure gauge
MO engine oil pressure gauge
TA engine temperature
TI gear box oil temperature
TS exhaust gas temperature
V voltmeter
Remote control switches mounted on the relay box
K1 key switch electric discharge
K2 emergency engine shut-down provision
K3 EDC main (power supply
K4 power supply to terminal 50 of the electric
starter motor
K5 fuel electric pump power supply
K6 fuel filter heater element power supply
Fuses mounted on the relay box
F1 fuel electric pump
F2 heating element on fuel filter
F3 power supply to the heater plug control unit (15 A)
F4 EDC (10 A)
F5 EDC (25 A)
Maxi fuse
F6 heater plug power circuit
INSTALLATION DIRECTIVE
46 MAY 2006
S30 ENT M23
EDC connector B
B62 4
85150
28 72 5 1 68 61 62 25 48 52 93 71 92
JB
13
JB
10
JB
11
6
BAT
6
+
6
+
BAT
50
25
AC
70
GG
B+
2
5030
MM
PE
A
B
PF
A
B
30
50 15
JB
7
M
EJFC
5JB
1
R2
D1
VU
J1
R1 SS EDC SCP
CA
QP
JC
18 12 17
JC
7
T C D B E
K4
87 30
85 86
30 87
86 85
K1
30
87a
86 85
K2 JC
9
JB
9
F3F4
F5
87 30
85 86
K3
30 87
86 85
K6
30 87
86 85
K5
F1 F6
F2
MPO
M
91 31 30 45
6 3 2
PA
46 8 9
1 5 4
JB
18 12 17
ST30 86 D G4 31G1 G2 G3
G4G1 G2 G3
CC
JC
2
JB
2
AS
JE
10
JH
10
JH
4
JE
4
JB
8
JC
8
JFC
A B
JFC C D
Sk Connett_B S30
INSTALLATION DIRECTIVE 47
MAY 2006 S30 ENT M23
EDC connector A
15
8
U
P
123
43 28
PR
50 11 20
2 1 3
F3F4
6
BAT
6
+
BAT
A
B
1
2
ZH
19 23
U
P
R
t
1342
13 40 53 52 58 41 51 12 27
B C
1
2
E1
47 16 33 17
1
2
E4
46 311
1
2
E3
2
1
2
E2
85150
F5
AC
K3
49
H
2
11
2
A F
2 1 3
4 72642
K5 85
K6 85
CC 86
3087
8685
JFC H
JFC I
Sk Connett_A S30
INSTALLATION DIRECTIVE
48 MAY 2006
S30 ENT M23
Main analog instrument panel
C C
CG
50
15
30
CA
SA
TA MO V
JB 41
T
1
1
V
1
1
33
JB 32
34 40
85150
K I
1
1
48642 7128
45
O
422526 21 4322 23 19194746 3018 1238
92 726162 15
3135 17 20 2928 JB
1037 11
1
JC 41
L
P1
82 7146 15 39271636 13 5
4 3 2 1
33
JC 32
34 40
MS
1245422526 21 4322 23
199
194746 3018 38
1987 10 1315 2 3
3135 173 24
3 24
20 2928
17 18 54 1216 1411
JC
1037 11
6 20
44
44
SAC
SS
SI FA
EDC
S ATA
SBPO
B
AQ
1 32
M
QP
4JE
4JH
AS
10 JH
10 JE
JD
1
1
SCP
SBLA
SIFB
SIFO
SIFC
SP
SSV
49
1 82 7146 15 39271636 13 5
49
W
1
1
Z
A
B
6
BAT
6
+
BAT
50
25
AC
70
GG
B+
2
5030
MM
R2
D1
K4
87 30
85 86
30 87
86 85
K1
30
87a
86 85
K2
F4
F5
87 30
85 86
K3
M
40
500
10
20 30
F
E
JFC
C D
JFC
G
JFC
Sk Quadro principale S30
INSTALLATION DIRECTIVE 49
MAY 2006 S30 ENT M23
Secondary analog instrument panel
CG
SA
2
3
4 1
CS
MS
1
9 198
710 13
15 2317 18 5
412
16 1411 623
JD
AS
346
58
7109 11 12
12 11 10 9 7
85
63
4
P1
JE
JH
QS
2
1
21
40
500
10
20 30
C C
CG
50
15
30
CA
SA
TA MO V
JB
1
JC
L
P1
82 7146 15 39271636 13 5
4 3 2 1
MS
SAC
SS
SI FA
EDC
S ATA
SBPO
AQ
QP
JD
SCP
SBLA
SIFB
SIFO
SIFC
SP
SSV
49
1 82 7146 15 39271636 13 5
49
6
BAT
6
+
BAT
50
25
AC
70
GG
B+
2
5030
MM
R2
D1
K4
87 30
85 86
30 87
86 85
K1
F4
F5
87 30
85 86
K3
M
40
500
10
20 30
* * 72 5 1 B EDC
1
99 198
710 13
15 2317 18 5
412
16 1411 624
2
34
34
Sk Quadro secondario S30
* See main instrument panel
wiring diagram
INSTALLATION DIRECTIVE
50 MAY 2006
S30 ENT M23
Wiring of a specific personalised instrument board
123
4
56
10 912 11
1314
16 15
171820 19
212224 23
JB
1234
5678
bar
psi
0
246810
0
29 58 87
116
145
G
250
oF
oC
210175
105
120
100
40
80
VOLT
8
12 14
16
G
35 29 30 17 1278232335 3413 19 18 31
OFF ON
START 7
8



 
min
X100
Connections
to be carried out
Identifying numbering
on each wire
10 meter long
wire harness
JD Connector integrated in the rear part
of the indications and alarms module
Sk Quadri VDO S30
INSTALLATION DIRECTIVE 51
MAY 2006 S30 ENT M23
Wiring of the double personalised instrument board (main and secondary board)
MAIN PANEL SECONDARY PANEL
123
4
56
10 912 11
1314
16 15
171820 19
212224 23
JBJB
1234
5678
bar
psi
0
246810
0
29 58 87
116
145
G
250
oF
oC
210175
105
120
100
40
80
VOLT
G
19 18 317232335 3413
123
4
56
10 912 11
1314
16 15
171820 19
212224 23
1234
5678
bar
psi
0
246810
0
29 58 87
116
145
G
250
oF
oC
210175
105
120
100
40
80
VOLT
G
8
OFF ON
START
8
12 14
16
8
12 14
16
7
8
7
8



 
min
X100



 
min
X100
35 29 30 17 12
Sk Quadri VDO 1°+2° S30
INSTALLATION DIRECTIVE
52 MAY 2006
S30 ENT M23
-

 
-




!#
"!4 "!4
"!4 nn "!4
--
''
"
!#
n


''
"
-- *!


*"
)% )%
n
-
 

"!4
n
!# --
"!4

''
"


*"





n
!#


2,
n

& &
Sk Accum_Servizi S30
Supplementary services battery recharge
Single engine
installation
Two-engines
installation
Key:
- AC1: Main Battery
- AC2: Battery for auxiliary services
- IE1: Engine 1 electrical system
- IE2: Engine 2 electrical system
- RL: Relay 50A max.
- *: Electrical power supply for services
IVECO S.p.A.
PowerTrain
Viale Dell’Industria, 15/17
20010 Pregnana Milanese - MI - (Italy)
Tel. +39 02 93.51.01 - Fax +39 02 93.59.00.29
www.ivecomotors.com

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