Engine air ACURA CSX 2006 Service Manual Online

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ECM/PCM Inputs and Outputs at Connector C ( ) (44P)
Terminal
numberWire color Terminal name DescriptionSignal
11-31
NOTE: Standard battery voltage is about 12 V.
1 WHT IG1ETCS (IGNITION SIGNAL ETCS) Detects ignition signal With ignition switch ON (II): battery voltage
2 BLK PGMETCS (POWER GROUND ETCS) Ground circuit for ECM/
PCMLess than 1.0 V at all times
3 GRN/YEL ETCSM (THROTTLE ACTUATOR SIDE) Ground for throttle actuator With ignition switch ON (II): about 0 V
4 BLU/RED ETCSM (THROTTLE ACTUATOR SIDE) Drives throttle actuator With ignition switch ON (II): about 0 V
5 BRN INJ1 (No. 1 INJECTOR) Drives No. 1 injector At idle: duty controlled With ignition switch ON (II): battery voltage
6 RED INJ2 (No. 2 INJECTOR) Drives No. 2 injector
7 BLU INJ3 (No. 3 INJECTOR) Drives No. 3 injector
8 YEL INJ4 (No. 4 INJECTOR) Drives No. 4 injector
9 WHT/GRN AFSHTC (AIR FUEL RATIO
(A/F) SENSOR HEATER
CONTROL (SENSOR 1)) Drives A/F sensor heater
(sensor 1)
With ignition switch ON (II): battery voltage
With fully warmed up engine running: about 0 V
11 GRN/RED MAP (MANIFOLD ABSOLUTE PRESSURE
(MAP) SENSOR) Detects MAP sensor signal With ignition switch ON (II): about 3.0 V
At idle: about 1.0 V (depending on engine speed)
12 BLU VCC3 (SENSOR VOLTAGE) Provides sensor reference voltageWith ignition switch ON (II): about 5.0 V
13 YEL/RED VCC1 (SENSOR VOLTAGE) Provides sensor reference voltageWith ignition switch ON (II): about 5.0 V
14 GRN/WHT SG1 (SENSOR GROUND) Sensor ground Less than 1.0 V at all times
15 YEL/GRN IGPLS1 (No. 1 IGNITION COIL PULSE) Drives No. 1 ignition coil With ignition switch ON (II): about 0 V
With engine running: pulses
16 BLU/RED IGPLS2 (No. 2 IGNITION COIL PULSE) Drives No. 2 ignition coil
17 WHT/BLU IGPLS3 (No. 3 IGNITION COIL PULSE) Drives No. 3 ignition coil
18 BRN IGPLS4 (No. 4 IGNITION COIL PULSE) Drives No. 4 ignition coil
20 RED/BLK TPSA (THROTTLE POSITION (TP) SENSOR A) Detects TP sensor A signal With throttle fully open: about 3.9 V
With throttle fully closed: about 0.9 V
21 RED/BLU TPSB (THROTTLE POSITION (TP) SENSOR B) Detects TP sensor B signal With throttle fully open: about 4.1 V
With throttle fully closed: about 1.7 V
(cont’d)
Terminal side of female terminals
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ECM/PCM Inputs and Outputs at Connector C ( ) (44P)
Terminal
numberWire color Terminal name DescriptionSignal
11-32Fuel and Emissions Systems
System Description (cont’d)
NOTE: Standard battery voltage is about 12 V.
22 BLU/BLK VTPSW (ROCKER ARM OIL PRESSURE SWITCH) Detects rocker arm oil
pressure switch signalWith engine at low speed: about 0 V
With engine at high speed: battery voltage
23 BLU/WHT VTC (VTC OIL CONTROL SOLENOID VALVE) Drives VTC oil control
solenoid valvewith ignition switch ON (II): about 0 V
27 WHT/RED SHO2S (SECONDARY HEATED OXYGEN SENSOR
(SECONDARY HO2S)
(SENSOR 2)) Detects secondary HO2S
(sensor 2) signal
With throttle fully opened from idle and warmed up
engine: about 0.6 V
With throttle quickly closed: below 0.4 V
29 RED AFS (AIR FUEL RATIO (A/F) SENSOR (SENSOR 1)SIDE) Detects A/F sensor
(sensor 1) signal
30 RED/YEL AFS (AIR FUEL RATIO (A/F) SENSOR (SENSOR 1)SIDE) Detects A/F sensor
(sensor 1) signal
31 GRN CMPB (CAMSHAFT POSITION (CMP) SENSOR
B) Detects CMP sensor B
signal
With engine running: pulses
32 BLU/YEL CKP (CRANKSHAFT POSITION (CKP) SENSOR) Detects CKP sensor signal With engine running: pulses
36 BLK/GRN IG1 (IGNITION SIGNAL) Detects ignition signal With ignition switch ON (II): battery voltage
39 GRN SG3 (SENSOR GROUND) Sensor ground Less than 1.0 V at all times
40 BRN/YEL LG1 (LOGIC GROUND) Ground circuit for ECM/ PCMLess than 1.0 V at all times
41 BLU/WHT CMPA (CAMSHAFT POSITION (CMP) SENSOR
A) Detects CMP sensor A
signal
With engine running: pulses
42 RED/BLU KS (KNOCK SENSOR) Detects knock sensor signal With engine knocking: pulses
43 BLK/WHT NC (OUTPUT SHAFT (COUNTERSHAFT) SPEED
SENSOR) Detects output shaft
(countershaft) speed sensor
signalsWith ignition switch ON (II): pulses
With vehicle moving: about 5.0 V (pulses)
44 BRN/YEL LG2 (LOGIC GROUND) Ground circuit for ECM/ PCMLess than 1.0 V at all times
Terminal side of female terminals
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PGM-FI System
Air Conditioning (A/C) Compressor Clutch Relay
Air Fuel Ratio (A/F) Sensor
Barometric Pressure (BARO) Sensor
Camshaft Position (CMP) Sensor BCrankshaft Position (CKP) Sensor
Engine Coolant Temperature (ECT) Sensor 1 and 2
Ignition Timing Control
Injector Timing and Duration
11-33
ZIRCONIA
ELEMENT
SENSOR
TERMINALS
HEATER
TERMINALS
O-RING
MAGNET
TERMINAL TERMINAL
O-RING
MAGNET
THERMISTOR O-RING TERMINAL
The programmed fuel injection (PGM-FI) system is a
sequential multiport fuel injection system.
When the ECM/PCM receives a demand for cooling
from the A/C system, it delays the compressor from
being energized, and enriches the mixture to assure
smooth transition to the A/C mode.
The A/F sensor operates over a wide air/fuel range. The
A/F sensor is installed upstream of the TWC, and sends
signals to the ECM/PCM which varies the duration of
fuel injection accordingly.
The BARO sensor is inside the ECM/PCM. It converts
atmospheric pressure into a voltage signal that
modifies the basic duration of the fuel injection
discharge.
CMP sensor B detects the position of the No. 1 cylinder
as a reference for sequential fuel injection to each
cylinder. The CKP sensor detects crankshaft speed and is used by
the ECM/PCM to determine the ignition timing, timing
for the fuel injection of each cylinder, and engine
misfire detection.
ECT sensors 1 and 2 are temperature dependent
resistors (thermistors). The resistance decreases as the
engine coolant temperature increases.
The ECM/PCM contains the memory for basic ignition
timing at various engine speeds and manifold absolute
pressures. It also adjusts the timing according to engine
coolant temperature and intake air temperature.
The ECM/PCM contains the memory for basic discharge
duration at various engine speeds and manifold
pressures. The basic discharge duration, after being
read out from the memory, is further modified by
signals sent from various sensors to obtain the final
discharge duration.
By monitoring long term fuel trim, the ECM/PCM
detects long term malfunctions in the fuel system and
sets diagnostic trouble codes (DTCs) if needed.
(cont’d)
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Knock Sensor
Manifold Absolute Pressure (MAP) Sensor
Malfunction Indicator Lamp (MIL) Indication (In relation
to Readiness Codes) Mass Air Flow (MAF) Sensor/Intake Air Temperature
(IAT) Sensor
Output Shaft (Countershaft) Speed Sensor
A/T
11-34
Fuel and Emissions Systems
System Description (cont’d)
TERMINAL
PIEZO
CERAMIC
ELEMENT
DIAPHRAGM
O-RING TERMINAL HOT WIRE
SENSOR
O-RING
COLD WIRE
SENSOR IAT SENSOR
(THERMISTOR)
MAGNET O-RING
TERMINAL
The knock control system adjusts the ignition timing to
minimize knock.
The MAP sensor converts manifold absolute pressure
into electrical signals to the ECM/PCM.
The vehicle has certain readiness codes that are part of
the on-board diagnostics for the emissions systems. If
the vehicle’s battery has been disconnected or gone
dead, if the DTCs have been cleared, or if the ECM/PCM
has been reset, these codes are reset. In some states,
part of the emissions testing is to make sure these
codes are set to complete. If all of them are not set to
complete, the vehicle may fail the test, or the test
cannot be finished.
To check if the readiness codes are set to complete,
turn the ignition switch to ON (II), but do not start the
engine. The MIL will come on for 15 20 seconds. If it
then goes off, the readiness codes are complete. If it
flashes five times, one or more readiness codes are not
complete. To set each code, drive the vehicle or run the
engine as described in the procedures (see page 11-69). The mass air flow (MAF) sensor/intake air temperature
(IAT) sensor contains a hot wire sensor, a cold wire
sensor, and a thermistor. It is located in the intake air
passage. The resistance of the hot wire sensor, the cold
wire sensor, and the thermistor change due to intake air
temperature and air flow. The control circuit in the MAF
sensor controls the current to keep the hot wire at a set
temperature. The current is converted to voltage in the
control circuit, then output to the ECM/PCM.
This sensor detects countershaft speed.
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i-VTEC
11-37
LOW SPEED CAMHIGH SPEED CAM
HIGH
ENGINE SPEED HIGH
LOW
LOW
ENGINE
LOAD
TORQUE CURVE
 The i-VTEC system has a variable valve timing control (VTC) mechanism on the intake camshaft in addition to the
usual VTEC.
This system improves fuel efficiency and reduces exhaust emissions at all levels of engine speed, vehicle speed,
and engine load.
 The VTEC system changes the valve lift and timing by using more than one cam profile.
 The VTC system changes the phase of the intake camshaft via oil pressure. It changes the intake valve timing continuously.
Driving Condition VTC Control Description
Light-load Base Position For stable combustion, the cam angle is retarded, and reduces the entry of exhaust gas into the cylinder.
Medium/high-load Advance Control Cam phase angle is controlled to optimize valve timing, improving fuel efficiency and reducing
emissions.
High speed Advance-Base Position To reduce pumping loss, the intake valve is closed quickly. This gives the air/fuel mixture a charging
effect that helps to maximize engine power.
(cont’d)
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VTC System
VTEC System
K20Z2 engine
K20Z3 engine
11-38
Fuel and Emissions Systems
System Description (cont’d)
MAXIMUM VTC ADVANCE 25 °
TDC
EX IN 1IN 2
EX IN 2IN 1
MAXIMUM VTC ADVANCE 25 °
SHORT OVERLAP
LONG OVERLAP
LOW SPEED VALVE TIMING HIGH SPEED VALVE TIMING
EX IN EXIN
IN (LOW LIFT)
LOW SPEED VALVE TIMING HIGH SPEED VALVE TIMING
EX IN EX IN
 The VTC system makes continuous intake valve timing changes based on operating conditions.
 Intake valve timing is optimized to allow the engine to produce maximum power.
 Cam angle is advanced to obtain the EGR effect and reduce pumping loss. The intake valve is closed quickly to
reduce the entry of the air/fuel mixture into the intake port and improve the charging effect.
 The system reduces the cam advance at idle, stabilizes combustion, and reduces engine speed.
 If a malfunction occurs, the VTC system control is disabled and the valve timing is fixed at the fully retarded position.
 The VTEC system changes the cam profile to correspond to the engine speed. It maximizes torque at low engine speed and output at high engine speed.
 The low lift cam is used at low engine speeds, and the high lift cam is used at high engine speeds.
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Intake Air System
Catalytic Converter System
Positive Crankcase Ventilation (PCV) System
Intake Air Bypass Control Thermal Valve Three Way Catalytic Converter (TWC)
11-40Fuel and Emissions Systems
System Description (cont’d)
OUT
INVALVE
WAX
ELEMENT
INJECTOR INTAKE AIR
BYPASS CONTROL
THERMAL VALVE FRONT OF
VEHICLE
HOUSING
THREE WAY
CATALYST BREATHER PIPE
INTAKE
MANIFOLD
PCV HOSE PCV VALVE
:BLOW-BYVAPOR
:FRESHAIR
This system supplies air for engine needs.
When the engine is cold, the intake air bypass control
thermal valve sends air to the injector.
The amount of air is regulated by engine coolant
temperature. Once the engine is hot, the intake air
bypass control thermal valve closes, stopping air to the
injector. The TWC converts hydrocarbons (HC), carbon
monoxide (CO), and oxides of nitrogen (NOx) in the
exhaust gas to carbon dioxide (CO ), nitrogen (N ), and
water vapor.
The PCV valve prevents blow-by gasses from escaping
into the atmosphere by venting them into the intake
manifold.
22
* : This illustration shows K20Z2 engine
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Evaporative Emission (EVAP) Control Diagram
11-45
ATMOSPHERE
ATMOSPHERE
FUEL FILL
CAP FUEL TANK VAPOR
RECIRCULATION
TUBE
FUEL TANK VAPOR
CONTROL VALVE
VARIOUS
SENSORS
FUEL TANK FTP SENSOR
EVAP CANISTER
VENT SHUT VALVE
PUR
LT GRN
ECM/PCM BLK
YEL
YEL/BLU
BLK/YEL RED
BLU BLK
LT GRN
From
No. 3
ALTERNATOR
(10 A) FUSE
From
PGM-FI
SUBRELAY
EVAP
CANISTER
EVAP CANISTER
PURGE VALVE ATMOSPHERE
The EVAP controls minimize the amount of fuel vapor escaping into the atmosphere. Vapor from the fuel tank is
temporarily stored in the EVAP canister until it can be purged from the canister into the engine and burned.
The EVAP canister is purged by drawing fresh air through it and into a port on the intake manifold.
The purging vacuum is controlled by the EVAP canister purge valve, which operates whenever engine coolant
temperature is above 60 °C (140 °F).
(cont’d)
* : This illustration shows K20Z2 engine
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Evaporative Emission (EVAP) Control
System Monitor and Readiness CodeAir Fuel Ratio (A/F) Sensor Monitor and
Readiness Code
Enable Criteria
Procedure Enable Criteria
Procedure
11-70Fuel and Emissions Systems
How to Set Readiness Codes (cont’d)
NOTE: All readiness codes are cleared when the battery
is disconnected, if the DTCs have been cleared, or if the
ECM/PCM is reset with the HDS.
 Battery voltage is more than 10.5 V.
 Engine at idle.
 ECT SENSOR 1 and ECT SENSOR 2 between 80 °C (176 °F) and 100 °C (212 °F).
 MAP SENSOR less than 46.6 kPa (350 mmHg, 14 in.Hg).
 Vehicle speed (VSS) 0 km/h (0 mph).
 IAT SENSOR between 0 °C (32 °F) and 100 °C (212 °F).
1. Connect the HDS to the DLC.
2. Start the engine.
3. Select EVAP TEST in the INSPECTION MENU with the HDS, then select the FUNCTION TEST in the
EVAP TEST MENU.
 If the result is normal, readiness is complete.
 If the result is not normal, go to the next step.
4. Check for a Temporary DTC. If there is no DTC, one or more of the enable criteria were probably not
met; repeat the procedure. NOTE:
 Do not turn the ignition switch to LOCK (0) or ACC (I) during the procedure.
 All readiness codes are cleared when the battery is disconnected, if the DTCs have been cleared, or if the
ECM/PCM is reset with the HDS.
ECT SENSOR 1 at 60 °C (140 °F) or more. 1. Start the engine.
2. Test-drive the vehicle under stop-and-go conditions with short periods of steady cruise. During the
drive, decelerate (with the throttle fully closed) for
5 seconds. After about 5.6 km (3.5 miles), the
readiness code should switch from incomplete to
complete.
3. Check the readiness codes screen for the air fuel ratio (A/F) sensor in the DTCs MENU with the HDS.
 If the screen shows complete, readiness is complete.
 If the screen shows not complete, go to the next step.
4. Check for a Temporary DTC. If there is no DTC, the enable criteria was probably not met. Select the
DATA LIST MENU. Check the ECT SENSOR 1 in the
ALL DATA LIST with the HDS. If the ECT SENSOR 1
is less than 60 °C (140 °F), run the engine until it is
more than 60 °C (140 °F), then repeat the procedure.
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Air Fuel Ratio (A/F) Sensor Heater Monitor
Readiness Code
Misfire Monitor and Readiness Code
Fuel System Monitor and Readiness Code
Comprehensive Component Monitor and
Readiness CodeEGR Monitor and Readiness Code
Procedure
Enable Criteria
Procedure
11-71
NOTE: All readiness codes are cleared when the battery
is disconnected, if the DTCs have been cleared, or if the
ECM/PCM is reset with the HDS.
1. Start the engine, and let it idle for 1 minute. The readiness code should switch from incomplete to
complete.
2. If the readiness code is still not set to complete, check for a Temporary DTC. If there is no DTC,
repeat the procedure.
 This readiness code is always set to available because misfiring is continuously monitored.
 Monitoring pauses, and the misfire counter resets, if the vehicle is driven over a rough road.
 Monitoring also pauses, and the misfire counter holds at its current value, if the throttle position
changes more than a predetermined value, or if
driving conditions fall outside the range of any
related enable criteria.
 This readiness code is always set to available because the fuel system is continuously monitored
during closed loop operation.
 Monitoring pauses when the catalytic converter, EVAP control system, and A/F sensor monitors are
active.
 Monitoring also pauses when any related enable criteria are not being met. Monitoring resumes when
the enable criteria is again being met.
This readiness code is always set to available because
the comprehensive component monitor is continuously
running when ever the engine is cranking or running. NOTE:
 Do not turn the ignition switch to LOCK (0) or ACC (I) during the procedure.
 All readiness codes are cleared when the battery is disconnected, if the DTCs have been cleared, or if the
ECM/PCM is reset with the HDS.
ECT SENSOR 1 at 80 °C (176 °F) or more. 1. Connect the HDS to the DLC.
2. Start the engine.
3. Drive at a steady speed with the A/T in D position or M/T in 4th gear, at 80 100 km/h (50 62 mph) or
above for more than 10 seconds.
4. With the A/T in D position or M/T in 4th gear, decelerate from 100 km/h (62 mph) or above by
completely releasing the throttle for at least
5 seconds. If the engine is stopped during this
procedure, go to step 3 and do the procedure again.
5. Check the OBD status screen for DTC P0401 in the DTC’s MENU with the HDS.
 If it is PASSED, readiness is complete.
 If it is not PASSED, go to step 3 and retest.
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