service MITSUBISHI LANCER EVOLUTION IX 2005 Workshop Manual

SERVICE MANUAL
Supplement

Related materials

Title No. IssuedateTitle No. Issue
date
New model manuals Body edition service manual
• Lancer Sedia 1036K30 2000/5 • Lancer Sedia 1036K50 2000/5
• Lancer Sedia 1036K31 2000/7 • Lancer Sedia (supplement) 1036K51 2000/7
• Lancer Evolution VII 1036K32 2001/1 • Lancer Evolution VII 1036K52 2001/5
• Lancer Sedia 1036K33 2001/5 (supplement)
• Lancer Sedia 1036K34 2001/5 • Lancer Sedia (supplement) 1036K53 2001/10
• Lancer Evolution VII 1036K35 2002/1 • Lancer Evolution VII _MR 1036K54 2004/2
• Lancer Sedia 1036K36 2002/5 (supplement)
• Lancer Evolution VII 1036K37 2003/1
• Lancer 1036K38 2003/2
• Lancer 1036K39 2003/12 Electrical wiring service manual
• Lancer Evolution VII _MR 1036K40 2004/2 • Lancer Evolution IX 1036K82 2005/3
• Lancer* 1036K41 2004/3
• Lancer 1036K42 2005/1
• Lancer Evolution IX 1036K43 2005/3
Service manuals Engine service manual
• Lancer Sedia 1036K00 2000/5 • 4G6 engine 1039G46 2001/1
• Lancer Sedia
(supplement) 1036K01 2000/7 • 4G6 engine (supplement) 1039G63 2003/1
• Lancer Evolution VII 1036K02 2001/1 • 4G6 engine (supplement) 1039G71 2003/3
(supplement)
• Lancer Sedia
(supplement) 1036K03 2001/5
• Lancer Sedia
(supplement) 1036K04 2001/10
• Lancer Evolution VII 1036K05 2002/1 Transmission service manuals
(supplement) • W5M51 manual transmission 1039M17 2001/1
• Lancer Sedia
(supplement) 1036K06 2002/5 • W5M51 manual transmission 1039M22 2003/1
• Lancer Evolution VII 1036K07 2003/1 (supplement)
(supplement) • WGMAA manual transmission 1039M23 2003/1
• Lancer Sedia
(supplement) 1036K08 2003/2
• Lancer Sedia
(supplement) 1036K09 2003/12
• Lancer Evolution VII MR 1036K10 2004/2
• Lancer* 1036K41 2004/3
• Lancer 1036K11 2005/1
*Indicates where the new model manual was published with the service man\
ual in a single volume.
W
ARNING REGARDING THE SERVICING OF VEHICLES FITTED WITH SRS AIR BAGS AND SEATBELTS WITH PRE-
TENSIONERS
W arning
1. Improper servicing or maintenance of any SRS air bag or pre-tensioner fi\
tted seatbelt component, or related parts, could cause serious injury through the SRS air bag or pre-tensioner fitt\
ed seatbelt being activated unintentionally
or accidentally.
2. The SRS-ECU, the driver’s side air bag module, the passenger side air bag module, the pre-tensio\
ner fitted seatbelts and the clock spring, should be removed if there is a chance o\
f them being affected by heat during
painting work.
• 93ºC and above: the SRS-ECU, the driver’s air bag module, the passenger’s air bag module and the clock spring should be removed.
• 90ºC and above: the pre-tensioner fitted seatbelts should be rem\
oved.
3. Servicing and maintenance of any SRS air bag or pre-tensioner fitted sea\
tbelt components, or related parts, must be performed by an authorized Mitsubishi dealer.
4. Servicing and maintenance of any SRS air bag or pre-tensioner fitted sea\
tbelt components, or related parts, must only be undertaken after this service manual (specifically Section 52B-\
SRS air bags) has been carefully studied.

ENGINE – CAMSHAFT, VALVE STEM SEAL11-10



B 
Fitting the valve spring
Fit the valve spring so that the end of the valve spring which has
the smaller radius is on the rocker arm side.



C 
Fitting the valve spring retainer lock
In the same way as when the valve spring retainer lock was
removed, compress the valve spring using the special tool for
compressing valve springs (MD998772), and fit the valve spring
retainer lock.



D 
Fitting the rush adjuster
Caution
If a rush adjuster is being reused, it must be washed and
inspected before fitting.
(Ref: Engine Service Manual)



E 
Fitting the camshaft
1. Remove any sealant from the cylinder head.
2. Apply engine oil to the camshaft cams and journals.
3. Fit the camshaft to the cylinder head.
Caution
Ensure that the inlet and exhaust sides are not the wrong way
round.



F 
Fitting the camshaft bearing cap No.4, the camshaft
bearing cap No.3, the camshaft bearing cap No.5, the
camshaft bearing cap No.2, the rear camshaft bearing
cap, and the front camshaft bearing cap
1. Set the camshaft dowel pins in the position shown in the
diagram.Rocker arm side
Front of engine

slit
slit
Approx. 4°dowel pins
inlet sideexhaust side

13A-7MPI – TROUBLESHOOTING
3. INSPECTION PROCEDURES FOR EACH DIAGNOSIS CODE
MUT-II/III service data
•No.95 atmospheric pressure
sensor
(Ref: P13A-24)
Go on to the next page
Measurements taken at
C-50 engine ECU connector
•Measure engine ECU terminal
voltage
•Ignition switch: ON
•Voltage across earth at 42
OK:4.9~5.1V
Check connectorC-50
Inspect the harness between the
MAP sensor and the engine ECU.
•Check if the power supply has
short circuited.
MUT-II/III service data
• No.95: MAP sensor
(Ref: P13A-24)
Replace the engine ECU
Check connectorC-50
Inspect the harness between the
MAP sensor and the engine ECU.
•Check if earth wire is cut or
damaged.
MUT-II/III service data
•No.95: MAP sensor
(Ref: P13A-24)
Replace the engine ECU
Check connectorC50
Inspect the harness between the
MAP sensor and the engine ECU,
repair if necessary.
•Check if the power supply wire is
cut.
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
Measurements taken at the B-135
MAP sensor connector
•Undo the connector, and take
measurements using the
harness
(1) Voltage across earth at 3
(ignition switch: ON)
OK: 4.9~5.1V
(2) Resistance across earth at 2
OK: 2Ω or less
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
Check connectorB-135
NG
(2) NG (1) NGOK
NG
OK
OK
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
NG
OK
NG
OK
OK
NGOK
NG
OK
NG
Repair
NG
OK
OK
NG
NG
OK
Repair
Repair
Repair
Repair
Repair
Code No. P0105 MAP sensor systemProbable cause of the malfunction
Conditions for the inspection
• Ignition switch: ON
• Wait for 2 seconds after the ignition switch has been turned on or the
engine has started.
Evaluation conditions
• Sensor output voltage is 4.6V or more for 4 seconds (when atmospheric
pressure is more than 313 kPa)
• Sensor output voltage is 0.2V or less for 4 seconds (when atmospheric
pressure is more than 14 kPa)• MAP sensor malfunction
• Broken circuit or short circuit in the MAP
sensor circuit
• Poor connector contact
• Engine ECU malfunction

13A-8MPI – TROUBLESHOOTING
Continued from the previous page
Measurements taken at the B-135
MAP sensor connector
•Connect the test harness
(MB991348) to the connector
and measure at the pick-up
harness component.
•Ignition switch: ON
•Voltage across earth at 2
OK: 4.9~5.1V
Measurements taken at the B-135
MAP sensor connector
•Connect the test harness
(MB991348) to the connector
and measure at the pick-up
harness component.
•Ignition switch: ON
•Voltage across earth at 1
OK:altitude 0m 1.2~1.8V
altitude 600m 1.1~1.7V
altitude 1200m 1.0~1.6V
altitude 1800m 0.9~1.5V
Measurements taken at the C-50
engine ECU connector
•Measure engine ECU terminal
voltage
•Ignition switch: ON
•Voltage across earth at 92
OK:altitude 0m 1.2~1.8V
altitude 600m 1.1~1.7V
altitude 1200m 1.0~1.6V
altitude 1800m 0.9~1.5V
MUT-II/III service data
•No.95: MAP sensor
(Ref: P13A-24)
Replace the engine ECU
Check connectorC-50
Check connectorC-50
Inspect the harness between the
MAP sensor and the engine ECU,
repair if necessary.
•Check for damage to the power
supply wire.
Check connectorC-50
Inspect the harness between the
MAP sensor and the engine ECU.
•Check if the output wire has
short circuited.
Replace the MAP sensor
Check connectorC-50
Inspect the harness between the
MAP sensor and the engine ECU,
repair if necessary
•Check if the output wire has
been cut or damaged.
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
OK
OK
OK
OK
OK
NGRepair
OK
OK
OK
OK
NG
NGNG
NG
NG
OK
NG
Repair
NG
NG
Repair
Repair
Repair

13A-14MPI – TROUBLESHOOTING
MUT-II/III Service data
•No.25: atmospheric sensor
(Ref: P13A-83) *Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
Check connectorC-50
Check connectorC-50
Check connector C-49
Check connectorB-08
Go on to the next page
Inspect the harness between the
AFS and the engine ECU
•Check if the power supply wire
has short circuited
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
Temporary malfunction (Ref
Section 00: Dealing with
temporary malfunctions)
Inspect the harness between the
AFS and the engine ECU, repair
if necessary
•Check if the power supply wire
is cut
MUT-II/III Service data
•No.25: atmospheric sensor
(Ref: P13A-83) *
Inspect the harness between the
AFS and the engine ECU
•Check if the earth wire is cut or
damaged
MUT-II/III Service data
•No.25: atmospheric sensor
(Ref: P13A-83) *
Replace the engine ECU
Replace the engine ECU
Measurement at B-08 AFS
connector
•Undo the connector and
measure on the harness side.
(1) Voltage across earth at 1
(ignition switch: ON)
OK:4.9~5.1V
(2) Resistance across earth at 5
OK:Less than 2ΩMeasurement at C-50 engine
ECU connector
•Measure the voltage at the
engine ECU terminals
•Ignition switch: ON
•Voltage across earth at 42
OK:4.9~5.1V
*: Refer to the 03-1 Service Manual for the Lancer Evolution VIII (No.1036K07)
Code No.P2226 Atmospheric pressure sensor systemProbable cause of the malfunction
Conditions for inspection
•Ignition switch: ON
•Wait for 2 seconds after the ignition switch has been turned on or the
engine has started.
Evaluation conditions
•Output voltage from the sensor is more than 4.5V (when atmospheric
pressure is in excess of 114kPa) for 4 seconds.
Or,
•Output voltage from the sensor is more than 0.2V (when atmospheric
pressure is less than 5kPa) for 4 seconds.•Malfunction of the atmospheric pressure
sensor
•Broken circuit or short circuit in the
atmospheric pressure sensor circuit, or poor
connector contact
•Malfunction of engine ECU
NG
OK
OK
NG
(1) NG
(2) NG
OK
Repair
Repair
Repair
Repair
OK
NG
OK
OK
NG
OK
OK
NG
OK
OK
NG
NG
NG
NG
OKNGRepair
Repair

13A-15MPI – TROUBLESHOOTING
Continued from previous page
Measurements taken at B-08 AFS
connector
•Only connect the test harness
(MB991709) to terminals
No.1, No.2 and No.5 of the
connector and measure at the
pick up harness component.
•Ignition switch: ON
(1) Voltage across earth at 1
OK:4.9~5.1V
(2) Voltage across earth at 2
OK:altitude 0m 3.8~4.2V
altitude 600m 3.5~3.9V
altitude 1200m 3.3~3.7V
altitude 1800m 3.0~3.4V
*: Refer to the 03-1 Service Manual for the Lancer Evolution VIII (No.1036K07)
Replace the AFS
Check connectorC-50
Replace the engine ECU
Inspect the harness between AFS
and engine ECU, repair if
necessary
•Check if the output wire is cut or
damaged
Temporary malfunction (Refer to
Section 00: Dealing with
temporary malfunctions)
Check connectorsC-49 & C-50
Inspect the harness between AFS
and engine ECU
•Check if the output wire has
short circuited or is damaged
Inspect the harness between AFS
and engine ECU, repair if
necessary
•Check if the power supply wire
is damaged
MUT-II/III Service data
•No.25: atmospheric sensor
(Ref: P13A-83) *
Measurement at the C-50 engine
ECU connector
•Measurement of the terminal
voltage of the engine ECU
•Ignition switch: ON
•Voltage across earth at 51
OK:altitude 0m 3.8~4.2V
altitude 600m 3.5~3.9V
altitude 1200m 3.3~3.7V
altitude 1800m 3.0~3.4V
Check connectorC-50
Check connectorC-50
OK
OK
OK
OK
OK
NG
(1) NG
(2) NG
NG
NG
OK
NG
NG
NG
OK
OK
OK
NG
Repair
Repair
Repair
Repair
Repair

13A-16MPI – TROUBLESHOOTING
Check the purge control solenoid valve (Refer to Section
17: Checking the exhaust gas purification system)
MUT-II/III Service data
•No.11 O
2sensor (Ref: P13A-83)*
Refer to the diagnosis code classification table (P13A-6)MUT-II/III diagnosis code
•Is the diagnosis code displayed?
Check the timing of ignition (Ref Section 11, Engine
tuning)
Check the sound made by the injector (using a
soundscope)
Check the crank angle sensor and the fitting of the timing
belt cover
If there is abnormality in the exhaust gases and code
Nos. P0201~P0204 are recorded, check the injector
system
If abnormal sensor data is recorded, carry out inspections
for each diagnosis code in order (Ref: P13A-6)
Replace the purge control solenoid valve
Code No.P0130: O
2sensor system inspection (Ref:
P13A-16)*
Go on to next page.
MUT-II/III Service data
•No.13: Intake air temperature sensor
•No.14: TPS
•No.21: Water temperature sensor
•No.25: Atmospheric pressure sensor
•No.95: MAP sensor
(Ref: P13A-24)

Proceed to OK if all service data levels are normal.
Proceed via NG even if only one of the service data
levels is abnormal.
*: Refer to the 03-1 Service Manual for the Lancer Evolution VIII (No.1036K07)
NO
OK
OK
OK
OK
OK
YES
NG
NG
NG
NG
Inspection procedureFault to be checkedReference page
11
Engine seems hesitant
13A-16Acceleration malfunction
Engine seems to stumble
Engine has a power surge
15Mis-timed ignition13A-18
35Inter-cooler water spray circuit system13A-19
37No.2 waste gate solenoid valve system13A-21
38Air temperature sensor system13A-22
Engine seems hesitant, acceleration malfunction, engine
seems to stumble, engine has a power surgeProbable causes of the malfunction
Probable causes of the malfunction are noted in the right hand
column.•Malfunction of the air/fuel mixing control system
•Malfunction of the ignition system
•Malfunction of the fuel system
•Malfunction of the intake system
•Malfunction of the exhaust gas purification system
•Failure of compression pressure
•Malfunction of the turbocharger system
5. Inspection procedure for each type of fault
Inspection procedure 11
4. Checklist of faults

13A-17MPI – TROUBLESHOOTING
*: Refer to the 01-1 Service Manual for the Lancer Evolution VIII (No.1036K02)
*: Refer to the 03-1 Service Manual for the Lancer Evolution VIII (No.1036K07)
Repair
Repair
Repair
Repair
Repair
Repair
Continued from previous page
Replace the spark plug wire
Replace the spark plug
Replace the ignition coil
Inspection procedure 33: Inspection of the No.1 waste
gate solenoid valve (Ref: P13A-78) *2
Inspection procedure 37: Inspection of the No.2 waste
gate solenoid valve (Ref: P13A-21)
Inspection procedure 31: Inspection of the fuel control
solenoid valve (Ref: P13A-76) *2
Inspection procedure 38: Inspection of the air
temperature sensor (Ref: P13A-22)
Check the spark plug wire (Ref: Section 16: Ignition
apparatus)
Check the spark plug (Ref: Section 16: Ignition
apparatus)
Check connectors B-123 & B-119
Check the ignition coil (Ref: Section 16: Ignition
Apparatus)
Inspect the harness and the connectors between each
cylinder’s ignition coil and the body earth, and between
the engine ECU and the ignition coil. Check for cut or
short circuited wires, or other damage.
MUT-II/III Actuator test
•No.12: Waste gate solenoid valve (Ref: P13A-87)*2
Check the supercharge pressure of the turbo charger
(Ref: Section 15: Intake/Exhaust car servicing)
Check the supercharge pressure control system (Ref:
Section 15: Intake/Exhaust car servicing)
MUT-II/III Actuator test
•No.09: Fuel pressure control solenoid valve (Ref:
P13A-87)
Check the fuel pressure (Ref: P13D-109)
Check the compression pressure (Ref: Section 11:
Engine tuning)
If the intake hose and the inlet manifold are damaged
check the air intake and repair as necessary.
Measurements taken at B-108 air temperature sensor
connector
•Using the test harness (MB991658), connect it to only
connectors No.1 and No.2 and measure at the pick-
up harness component.
•Ignition switch: ON
•Voltage across earth at 1
OK:surrounding temperature -20ºC 3.8~4.4V
surrounding temperature 0ºC 3.2~3.8V
surrounding temperature 20ºC 2.3~2.9V
surrounding temperature 40ºC 1.5~2.1V
surrounding temperature 60ºC 0.8~1.4V
surrounding temperature 80ºC 0.4~1.0V
OK
OK
OK
OK
OK
OK
OK
OK
OK
OK
OK
OK
OK
NG
NG
NG
NG
NG
NG
NG
NG
NG
NG
NG

13A-24MPI – TROUBLESHOOTING
13A-23
6. Service data table
7. Engine ECU checks
7-1 Terminal voltage table